Sample records for usaf reconnaissance purposes

  1. USAF Support to Low Intensity Conflict: Three Case Studies From the 1980s

    DTIC Science & Technology

    1994-06-01

    included armed reconnaissance provided by AC- 130H gunships, and an airdrop of USAF Combat Control Teams and Army Rangers . The main body for the...performance of elite units such as Delta Force, SEALS, Rangers , etc. did not justify the money spent or their claims of eliteness. AU Library Document M-43828...48Adkin, 132. 23 Figure 1 Task Organization for Joint Task Force 120. CJTF 120 Carribean Peacekeeping Force CTF 121 Airborne CTF 123 Rangers

  2. Microprocessor Front-End Terminal Study.

    DTIC Science & Technology

    1981-06-01

    Engineer APPROVED: .HN MARCINIAK, Colonel, USAF hief, Information Sciences Division FOR THE COMANDER: JOHN P. HUSS Acting Chief, Plans Office If your...friendly forces. The files are maintained by this branch acting independently or in coordination with lateral services or national agencies. 24 MFT Final...and reconnaissance mission results are analyzed to determine the degree of success of the attack. Target damage assessments are made, and targets are

  3. Evolving Intelligence, Surveillance & Reconnaissance (ISR) for Air Force Cyber Defense

    DTIC Science & Technology

    2013-02-14

    Telecommunications and Assessment Program ( TMAP ) notes in Air Force Instruction (AFI) 10-712 that “adversaries can easily monitor (unclassified) systems to...Instruction (AFI) 10-712, Telecommunications Monitoring And Assessment Program ( TMAP ), 2011, 4. 23. Lt Col Hugh M. Ragland., interview with author...Monitoring And Assessment Program ( TMAP ), 8 June 2011. Brenner, Carl N. Col, USAF. NASIC Air & Cyber Analysis Group/CC. Interview by the author. 29

  4. National Reconnaissance Almanac

    DTIC Science & Technology

    2011-01-01

    Germany. 1945 Mar. 19: The German V-2 program was abandoned, leaving rocket technology for capture by Allied forces. 1946 Apr. 16: The U.S. Army...first launched captured German V-2 rocket at White Sands, New Mexico during missile testing. May 2: RAND report, “Preliminary Design of Experimental...first human in space. May 5: LCDR Alan Shepard became first American in space during a brief sub-orbital flight. Aug. 30: USAF launched Corona

  5. Angle of Arrival Detection Through Artificial Neural Network Analysis of Optical Fiber Intensity Patterns

    DTIC Science & Technology

    1990-12-01

    ARTIFICIAL NEURAL NETWORK ANALYSIS OF OPTICAL FIBER INTENSITY PATTERNS THESIS Scott Thomas Captain, USAF AFIT/GE/ENG/90D-62 DTIC...ELECTE ao • JAN08 1991 Approved for public release; distribution unlimited. AFIT/GE/ENG/90D-62 ANGLE OF ARRIVAL DETECTION THROUGH ARTIFICIAL NEURAL NETWORK ANALYSIS... ARTIFICIAL NEURAL NETWORK ANALYSIS OF OPTICAL FIBER INTENSITY PATTERNS L Introduction The optical sensors of United States Air Force reconnaissance

  6. Air Sea Battle Intelligence, Surveillance, and Reconnaissance Concept of Operations: Getting Back to Fundamentals

    DTIC Science & Technology

    2012-05-08

    Assessment” phase. This phase will be constant throughout the AirSea Battle. A subset of this phase includes battle damage assessment ( BDA ). BDA ...taskings for assessment. There may be situations where operations will cease until the proper BDA is desired. This possibility directly... BDA assessments. It is paramount to task fifth generation fighter with this mission set due to their advanced capabilities. 15 The USAF and USN

  7. The United States Air Force in Southeast Asia: The War in Northern Laos, 1954-1973

    DTIC Science & Technology

    1993-01-01

    Simultaneously, all 315th Air Division courier flights were canceled; all training was scrubbed ; 0=0 (l) and certain division troop carriers stood alert...Force and scrub it of its national markings. With Defense and State approval, he manned the plane with experienced USAF reconnaissance pilots from...the aegis of Cambodian Prince Norodom Sihanouk. On June 22 they agreed in principle to a tripartite government that would rule Laos until new general

  8. Reassessment of psychological distress and post-traumatic stress disorder in United States Air Force Distributed Common Ground System operators.

    PubMed

    Prince, Lillian; Chappelle, Wayne L; McDonald, Kent D; Goodman, Tanya; Cowper, Sara; Thompson, William

    2015-03-01

    The goal of this study was to assess for the main sources of occupational stress, as well as self-reported symptoms of distress and post-traumatic stress disorder among U.S. Air Force (USAF) Distributed Common Ground System (DCGS) intelligence exploitation and support personnel. DCGS intelligence operators (n=1091) and nonintelligence personnel (n = 447) assigned to a USAF Intelligence, Surveillance, and Reconnaissance Wing responded to the web-based survey. The overall survey response rate was 31%. Study results revealed the most problematic stressors among DCGS intelligence personnel included high workload, low manning, as well as organizational leadership and shift work issues. Results also revealed 14.35% of DCGS intelligence operators' self-reported high levels of psychological distress (twice the rate of DCGS nonintelligence support personnel). Furthermore, 2.0% to 2.5% self-reported high levels of post-traumatic stress disorder symptoms, with no significant difference between groups. The implications of these findings are discussed along with recommendations for USAF medical and mental health providers, as well as operational leadership. Reprint & Copyright © 2015 Association of Military Surgeons of the U.S.

  9. Command History, 1971. Volume 1. Sanitized

    DTIC Science & Technology

    1971-01-01

    of 1971. During this period USAF A-lEs, F-4s, B-52s, and AC-ll9Gs provided interdiction, armed reconnaissance, and ground support to MAJ GEN Vang Pao’s...tribesmen. The ground situation was critical as GEN Pao was swept off the Plain of Jars and back almost to Luang Prabang, the royal capital of Laos...friendly forces. The seriousness of the situation in northern Zaos had subsided and GEN Pao’s forces were retaking ground lost earlier in a repeat of

  10. SR-71A - in Flight View from Tanker during an Airborne Refueling

    NASA Technical Reports Server (NTRS)

    1997-01-01

    This photo shows a USAF tanker aircraft Boom Operator's or 'Boomer's' view of NASA Dryden Flight Research Center's SR-71A, tail number 844, following air refueling during a 1997 flight. Two SR-71 aircraft have been used by NASA as testbeds for high-speed and high-altitude aeronautical research. The aircraft, an SR-71A and an SR-71B pilot trainer aircraft, have been based here at NASA's Dryden Flight Research Center, Edwards, California. They were transferred to NASA after the U.S. Air Force program was cancelled. As research platforms, the aircraft can cruise at Mach 3 for more than one hour. For thermal experiments, this can produce heat soak temperatures of over 600 degrees Fahrenheit (F). This operating environment makes these aircraft excellent platforms to carry out research and experiments in a variety of areas -- aerodynamics, propulsion, structures, thermal protection materials, high-speed and high-temperature instrumentation, atmospheric studies, and sonic boom characterization. The SR-71 was used in a program to study ways of reducing sonic booms or over pressures that are heard on the ground, much like sharp thunderclaps, when an aircraft exceeds the speed of sound. Data from this Sonic Boom Mitigation Study could eventually lead to aircraft designs that would reduce the 'peak' overpressures of sonic booms and minimize the startling affect they produce on the ground. One of the first major experiments to be flown in the NASA SR-71 program was a laser air data collection system. It used laser light instead of air pressure to produce airspeed and attitude reference data, such as angle of attack and sideslip, which are normally obtained with small tubes and vanes extending into the airstream. One of Dryden's SR-71s was used for the Linear Aerospike Rocket Engine, or LASRE Experiment. Another earlier project consisted of a series of flights using the SR-71 as a science camera platform for NASA's Jet Propulsion Laboratory in Pasadena, California. An upward-looking ultraviolet video camera placed in the SR-71's nosebay studied a variety of celestial objects in wavelengths that are blocked to ground-based astronomers. Earlier in its history, Dryden had a decade of past experience at sustained speeds above Mach 3. Two YF-12A aircraft and an SR-71 designated as a YF-12C were flown at the center between December 1969 and November 1979 in a joint NASA/USAF program to learn more about the capabilities and limitations of high-speed, high-altitude flight. The YF-12As were prototypes of a planned interceptor aircraft based on a design that later evolved into the SR-71 reconnaissance aircraft. Dave Lux was the NASA SR-71 project manger for much of the decade of the 1990s, followed by Steve Schmidt. Developed for the USAF as reconnaissance aircraft more than 30 years ago, SR-71s are still the world's fastest and highest-flying production aircraft. The aircraft can fly at speeds of more than 2,200 miles per hour (Mach 3+, or more than three times the speed of sound) and at altitudes of over 85,000 feet. The Lockheed Skunk Works (now Lockheed Martin) built the original SR-71 aircraft. Each aircraft is 107.4 feet long, has a wingspan of 55.6 feet, and is 18.5 feet high (from the ground to the top of the rudders, when parked). Gross takeoff weight is about 140,000 pounds, including a possible fuel weight of 80,280 pounds. The airframes are built almost entirely of titanium and titanium alloys to withstand heat generated by sustained Mach 3 flight. Aerodynamic control surfaces consist of all-moving vertical tail surfaces, ailerons on the outer wings, and elevators on the trailing edges between the engine exhaust nozzles. The two SR-71s at Dryden have been assigned the following NASA tail numbers: NASA 844 (A model), military serial 61-7980 and NASA 831 (B model), military serial 61-7956. From 1990 through 1994, Dryden also had another 'A' model, NASA 832, military serial 61-7971. This aircraft was returned to the USAF inventory and was the first aircraft reactivated for USAF reconnaissance purposes in 1995. It has since returned to Dryden along with SR-71A 61-7967.

  11. SR-71A - in Flight over Southern Sierra Nevada Mountains

    NASA Technical Reports Server (NTRS)

    1997-01-01

    NASA Dryden Flight Research Center's SR-71A, tail number 844, banks away over the Sierra Nevada mountains after air refueling from a USAF tanker during a 1997 flight. Two SR-71 aircraft have been used by NASA as testbeds for high-speed and high-altitude aeronautical research. The aircraft, an SR-71A and an SR-71B pilot trainer aircraft, have been based here at NASA's Dryden Flight Research Center, Edwards, California. They were transferred to NASA after the U.S. Air Force program was cancelled. As research platforms, the aircraft can cruise at Mach 3 for more than one hour. For thermal experiments, this can produce heat soak temperatures of over 600 degrees Fahrenheit (F). This operating environment makes these aircraft excellent platforms to carry out research and experiments in a variety of areas -- aerodynamics, propulsion, structures, thermal protection materials, high-speed and high-temperature instrumentation, atmospheric studies, and sonic boom characterization. The SR-71 was used in a program to study ways of reducing sonic booms or over pressures that are heard on the ground, much like sharp thunderclaps, when an aircraft exceeds the speed of sound. Data from this Sonic Boom Mitigation Study could eventually lead to aircraft designs that would reduce the 'peak' overpressures of sonic booms and minimize the startling affect they produce on the ground. One of the first major experiments to be flown in the NASA SR-71 program was a laser air data collection system. It used laser light instead of air pressure to produce airspeed and attitude reference data, such as angle of attack and sideslip, which are normally obtained with small tubes and vanes extending into the airstream. One of Dryden's SR-71s was used for the Linear Aerospike Rocket Engine, or LASRE Experiment. Another earlier project consisted of a series of flights using the SR-71 as a science camera platform for NASA's Jet Propulsion Laboratory in Pasadena, California. An upward-looking ultraviolet video camera placed in the SR-71's nosebay studied a variety of celestial objects in wavelengths that are blocked to ground-based astronomers. Earlier in its history, Dryden had a decade of past experience at sustained speeds above Mach 3. Two YF-12A aircraft and an SR-71 designated as a YF-12C were flown at the center between December 1969 and November 1979 in a joint NASA/USAF program to learn more about the capabilities and limitations of high-speed, high-altitude flight. The YF-12As were prototypes of a planned interceptor aircraft based on a design that later evolved into the SR-71 reconnaissance aircraft. Dave Lux was the NASA SR-71 project manger for much of the decade of the 1990s, followed by Steve Schmidt. Developed for the USAF as reconnaissance aircraft more than 30 years ago, SR-71s are still the world's fastest and highest-flying production aircraft. The aircraft can fly at speeds of more than 2,200 miles per hour (Mach 3+, or more than three times the speed of sound) and at altitudes of over 85,000 feet. The Lockheed Skunk Works (now Lockheed Martin) built the original SR-71 aircraft. Each aircraft is 107.4 feet long, has a wingspan of 55.6 feet, and is 18.5 feet high (from the ground to the top of the rudders, when parked). Gross takeoff weight is about 140,000 pounds, including a possible fuel weight of 80,280 pounds. The airframes are built almost entirely of titanium and titanium alloys to withstand heat generated by sustained Mach 3 flight. Aerodynamic control surfaces consist of all-moving vertical tail surfaces, ailerons on the outer wings, and elevators on the trailing edges between the engine exhaust nozzles. The two SR-71s at Dryden have been assigned the following NASA tail numbers: NASA 844 (A model), military serial 61-7980 and NASA 831 (B model), military serial 61-7956. From 1990 through 1994, Dryden also had another 'A' model, NASA 832, military serial 61-7971. This aircraft was returned to the USAF inventory and was the first aircraft reactivated for USAF reconnaissance purposes in 1995. It has since returned to Dryden along with SR-71A 61-7967.

  12. SR-71 Mid-air Refueling with KC-135 Tanker

    NASA Technical Reports Server (NTRS)

    1995-01-01

    NASA Dryden Flight Research Center's SR-71B, tail number 831, is seen here receiving air refueling from a USAF tanker during a July, 1995 flight. Two SR-71 aircraft have been used by NASA as testbeds for high-speed and high-altitude aeronautical research. The aircraft, an SR-71A and an SR-71B pilot trainer aircraft, have been based here at NASA's Dryden Flight Research Center, Edwards, California. They were transferred to NASA after the U.S. Air Force program was cancelled. As research platforms, the aircraft can cruise at Mach 3 for more than one hour. For thermal experiments, this can produce heat soak temperatures of over 600 degrees Fahrenheit (F). This operating environment makes these aircraft excellent platforms to carry out research and experiments in a variety of areas -- aerodynamics, propulsion, structures, thermal protection materials, high-speed and high-temperature instrumentation, atmospheric studies, and sonic boom characterization. The SR-71 was used in a program to study ways of reducing sonic booms or over pressures that are heard on the ground, much like sharp thunderclaps, when an aircraft exceeds the speed of sound. Data from this Sonic Boom Mitigation Study could eventually lead to aircraft designs that would reduce the 'peak' overpressures of sonic booms and minimize the startling affect they produce on the ground. One of the first major experiments to be flown in the NASA SR-71 program was a laser air data collection system. It used laser light instead of air pressure to produce airspeed and attitude reference data, such as angle of attack and sideslip, which are normally obtained with small tubes and vanes extending into the airstream. One of Dryden's SR-71s was used for the Linear Aerospike Rocket Engine, or LASRE Experiment. Another earlier project consisted of a series of flights using the SR-71 as a science camera platform for NASA's Jet Propulsion Laboratory in Pasadena, California. An upward-looking ultraviolet video camera placed in the SR-71's nosebay studied a variety of celestial objects in wavelengths that are blocked to ground-based astronomers. Earlier in its history, Dryden had a decade of past experience at sustained speeds above Mach 3. Two YF-12A aircraft and an SR-71 designated as a YF-12C were flown at the center between December 1969 and November 1979 in a joint NASA/USAF program to learn more about the capabilities and limitations of high-speed, high-altitude flight. The YF-12As were prototypes of a planned interceptor aircraft based on a design that later evolved into the SR-71 reconnaissance aircraft. Dave Lux was the NASA SR-71 project manger for much of the decade of the 1990s, followed by Steve Schmidt. Developed for the USAF as reconnaissance aircraft more than 30 years ago, SR-71s are still the world's fastest and highest-flying production aircraft. The aircraft can fly at speeds of more than 2,200 miles per hour (Mach 3+, or more than three times the speed of sound) and at altitudes of over 85,000 feet. The Lockheed Skunk Works (now Lockheed Martin) built the original SR-71 aircraft. Each aircraft is 107.4 feet long, has a wingspan of 55.6 feet, and is 18.5 feet high (from the ground to the top of the rudders, when parked). Gross takeoff weight is about 140,000 pounds, including a possible fuel weight of 80,280 pounds. The airframes are built almost entirely of titanium and titanium alloys to withstand heat generated by sustained Mach 3 flight. Aerodynamic control surfaces consist of all-moving vertical tail surfaces, ailerons on the outer wings, and elevators on the trailing edges between the engine exhaust nozzles. The two SR-71s at Dryden have been assigned the following NASA tail numbers: NASA 844 (A model), military serial 61-7980 and NASA 831 (B model), military serial 61-7956. From 1990 through 1994, Dryden also had another 'A' model, NASA 832, military serial 61-7971. This aircraft was returned to the USAF inventory and was the first aircraft reactivated for USAF reconnaissance purposes in 1995. It has since returned to Dryden along with SR-71A 61-7967.

  13. SR-71 - Taxi on Ramp with Engines

    NASA Technical Reports Server (NTRS)

    1995-01-01

    This photo shows a head-on shot of NASA's SR-71A aircraft taxiing on the ramp at NASA's Dryden Flight Research Center, Edwards, California, heat waves from its engines blurring the hangars in the background. Two SR-71 aircraft have been used by NASA as testbeds for high-speed and high-altitude aeronautical research. The aircraft, an SR-71A and an SR-71B pilot trainer aircraft, have been based here at NASA's Dryden Flight Research Center, Edwards, California. They were transferred to NASA after the U.S. Air Force program was cancelled. As research platforms, the aircraft can cruise at Mach 3 for more than one hour. For thermal experiments, this can produce heat soak temperatures of over 600 degrees Fahrenheit (F). This operating environment makes these aircraft excellent platforms to carry out research and experiments in a variety of areas -- aerodynamics, propulsion, structures, thermal protection materials, high-speed and high-temperature instrumentation, atmospheric studies, and sonic boom characterization. The SR-71 was used in a program to study ways of reducing sonic booms or over pressures that are heard on the ground, much like sharp thunderclaps, when an aircraft exceeds the speed of sound. Data from this Sonic Boom Mitigation Study could eventually lead to aircraft designs that would reduce the 'peak' overpressures of sonic booms and minimize the startling affect they produce on the ground. One of the first major experiments to be flown in the NASA SR-71 program was a laser air data collection system. It used laser light instead of air pressure to produce airspeed and attitude reference data, such as angle of attack and sideslip, which are normally obtained with small tubes and vanes extending into the airstream. One of Dryden's SR-71s was used for the Linear Aerospike Rocket Engine, or LASRE Experiment. Another earlier project consisted of a series of flights using the SR-71 as a science camera platform for NASA's Jet Propulsion Laboratory in Pasadena, California. An upward-looking ultraviolet video camera placed in the SR-71's nosebay studied a variety of celestial objects in wavelengths that are blocked to ground-based astronomers. Earlier in its history, Dryden had a decade of past experience at sustained speeds above Mach 3. Two YF-12A aircraft and an SR-71 designated as a YF-12C were flown at the center between December 1969 and November 1979 in a joint NASA/USAF program to learn more about the capabilities and limitations of high-speed, high-altitude flight. The YF-12As were prototypes of a planned interceptor aircraft based on a design that later evolved into the SR-71 reconnaissance aircraft. Dave Lux was the NASA SR-71 project manger for much of the decade of the 1990s, followed by Steve Schmidt. Developed for the USAF as reconnaissance aircraft more than 30 years ago, SR-71s are still the world's fastest and highest-flying production aircraft. The aircraft can fly at speeds of more than 2,200 miles per hour (Mach 3+, or more than three times the speed of sound) and at altitudes of over 85,000 feet. The Lockheed Skunk Works (now Lockheed Martin) built the original SR-71 aircraft. Each aircraft is 107.4 feet long, has a wingspan of 55.6 feet, and is 18.5 feet high (from the ground to the top of the rudders, when parked). Gross takeoff weight is about 140,000 pounds, including a possible fuel weight of 80,280 pounds. The airframes are built almost entirely of titanium and titanium alloys to withstand heat generated by sustained Mach 3 flight. Aerodynamic control surfaces consist of all-moving vertical tail surfaces, ailerons on the outer wings, and elevators on the trailing edges between the engine exhaust nozzles. The two SR-71s at Dryden have been assigned the following NASA tail numbers: NASA 844 (A model), military serial 61-7980 and NASA 831 (B model), military serial 61-7956. From 1990 through 1994, Dryden also had another 'A' model, NASA 832, military serial 61-7971. This aircraft was returned to the USAF inventory and was the first aircraft reactivated for USAF reconnaissance purposes in 1995. It has since returned to Dryden along with SR-71A 61-7967.

  14. SR-71B - Mach 3 Trainer in Flight at Sunset

    NASA Technical Reports Server (NTRS)

    1995-01-01

    An SR-71B Blackbird aircraft, based at NASA's Dryden Flight Research Center, Edwards, California, is seen here silhouetted against the golden colors of a sunset sky on a 1995 flight. Two SR-71 aircraft have been used by NASA as testbeds for high-speed and high-altitude aeronautical research. The aircraft, an SR-71A and an SR-71B pilot trainer aircraft, have been based here at NASA's Dryden Flight Research Center, Edwards, California. They were transferred to NASA after the U.S. Air Force program was cancelled. As research platforms, the aircraft can cruise at Mach 3 for more than one hour. For thermal experiments, this can produce heat soak temperatures of over 600 degrees Fahrenheit (F). This operating environment makes these aircraft excellent platforms to carry out research and experiments in a variety of areas -- aerodynamics, propulsion, structures, thermal protection materials, high-speed and high-temperature instrumentation, atmospheric studies, and sonic boom characterization. The SR-71 was used in a program to study ways of reducing sonic booms or over pressures that are heard on the ground, much like sharp thunderclaps, when an aircraft exceeds the speed of sound. Data from this Sonic Boom Mitigation Study could eventually lead to aircraft designs that would reduce the 'peak' overpressures of sonic booms and minimize the startling affect they produce on the ground. One of the first major experiments to be flown in the NASA SR-71 program was a laser air data collection system. It used laser light instead of air pressure to produce airspeed and attitude reference data, such as angle of attack and sideslip, which are normally obtained with small tubes and vanes extending into the airstream. One of Dryden's SR-71s was used for the Linear Aerospike Rocket Engine, or LASRE Experiment. Another earlier project consisted of a series of flights using the SR-71 as a science camera platform for NASA's Jet Propulsion Laboratory in Pasadena, California. An upward-looking ultraviolet video camera placed in the SR-71's nosebay studied a variety of celestial objects in wavelengths that are blocked to ground-based astronomers. Earlier in its history, Dryden had a decade of past experience at sustained speeds above Mach 3. Two YF-12A aircraft and an SR-71 designated as a YF-12C were flown at the center between December 1969 and November 1979 in a joint NASA/USAF program to learn more about the capabilities and limitations of high-speed, high-altitude flight. The YF-12As were prototypes of a planned interceptor aircraft based on a design that later evolved into the SR-71 reconnaissance aircraft. Dave Lux was the NASA SR-71 project manger for much of the decade of the 1990s, followed by Steve Schmidt. Developed for the USAF as reconnaissance aircraft more than 30 years ago, SR-71s are still the world's fastest and highest-flying production aircraft. The aircraft can fly at speeds of more than 2,200 miles per hour (Mach 3+, or more than three times the speed of sound) and at altitudes of over 85,000 feet. The Lockheed Skunk Works (now Lockheed Martin) built the original SR-71 aircraft. Each aircraft is 107.4 feet long, has a wingspan of 55.6 feet, and is 18.5 feet high (from the ground to the top of the rudders, when parked). Gross takeoff weight is about 140,000 pounds, including a possible fuel weight of 80,280 pounds. The airframes are built almost entirely of titanium and titanium alloys to withstand heat generated by sustained Mach 3 flight. Aerodynamic control surfaces consist of all-moving vertical tail surfaces, ailerons on the outer wings, and elevators on the trailing edges between the engine exhaust nozzles. The two SR-71s at Dryden have been assigned the following NASA tail numbers: NASA 844 (A model), military serial 61-7980 and NASA 831 (B model), military serial 61-7956. From 1990 through 1994, Dryden also had another 'A' model, NASA 832, military serial 61-7971. This aircraft was returned to the USAF inventory and was the first aircraft reactivated for USAF reconnaissance purposes in 1995. It has since returned to Dryden along with SR-71A 61-7967.

  15. SR-71 in Flight over Rogers Dry Lakebed

    NASA Technical Reports Server (NTRS)

    1995-01-01

    This photo shows NASA Dryden Flight Research Center's SR-71B, tail number 831, over Rogers Dry Lakebed during a July 1995 flight. Two SR-71 aircraft have been used by NASA as testbeds for high-speed and high-altitude aeronautical research. The aircraft, an SR-71A and an SR-71B pilot trainer aircraft, have been based here at NASA's Dryden Flight Research Center, Edwards, California. They were transferred to NASA after the U.S. Air Force program was cancelled. As research platforms, the aircraft can cruise at Mach 3 for more than one hour. For thermal experiments, this can produce heat soak temperatures of over 600 degrees Fahrenheit (F). This operating environment makes these aircraft excellent platforms to carry out research and experiments in a variety of areas -- aerodynamics, propulsion, structures, thermal protection materials, high-speed and high-temperature instrumentation, atmospheric studies, and sonic boom characterization. The SR-71 was used in a program to study ways of reducing sonic booms or over pressures that are heard on the ground, much like sharp thunderclaps, when an aircraft exceeds the speed of sound. Data from this Sonic Boom Mitigation Study could eventually lead to aircraft designs that would reduce the 'peak' overpressures of sonic booms and minimize the startling affect they produce on the ground. One of the first major experiments to be flown in the NASA SR-71 program was a laser air data collection system. It used laser light instead of air pressure to produce airspeed and attitude reference data, such as angle of attack and sideslip, which are normally obtained with small tubes and vanes extending into the airstream. One of Dryden's SR-71s was used for the Linear Aerospike Rocket Engine, or LASRE Experiment. Another earlier project consisted of a series of flights using the SR-71 as a science camera platform for NASA's Jet Propulsion Laboratory in Pasadena, California. An upward-looking ultraviolet video camera placed in the SR-71's nosebay studied a variety of celestial objects in wavelengths that are blocked to ground-based astronomers. Earlier in its history, Dryden had a decade of past experience at sustained speeds above Mach 3. Two YF-12A aircraft and an SR-71 designated as a YF-12C were flown at the center between December 1969 and November 1979 in a joint NASA/USAF program to learn more about the capabilities and limitations of high-speed, high-altitude flight. The YF-12As were prototypes of a planned interceptor aircraft based on a design that later evolved into the SR-71 reconnaissance aircraft. Dave Lux was the NASA SR-71 project manger for much of the decade of the 1990s, followed by Steve Schmidt. Developed for the USAF as reconnaissance aircraft more than 30 years ago, SR-71s are still the world's fastest and highest-flying production aircraft. The aircraft can fly at speeds of more than 2,200 miles per hour (Mach 3+, or more than three times the speed of sound) and at altitudes of over 85,000 feet. The Lockheed Skunk Works (now Lockheed Martin) built the original SR-71 aircraft. Each aircraft is 107.4 feet long, has a wingspan of 55.6 feet, and is 18.5 feet high (from the ground to the top of the rudders, when parked). Gross takeoff weight is about 140,000 pounds, including a possible fuel weight of 80,280 pounds. The airframes are built almost entirely of titanium and titanium alloys to withstand heat generated by sustained Mach 3 flight. Aerodynamic control surfaces consist of all-moving vertical tail surfaces, ailerons on the outer wings, and elevators on the trailing edges between the engine exhaust nozzles. The two SR-71s at Dryden have been assigned the following NASA tail numbers: NASA 844 (A model), military serial 61-7980 and NASA 831 (B model), military serial 61-7956. From 1990 through 1994, Dryden also had another 'A' model, NASA 832, military serial 61-7971. This aircraft was returned to the USAF inventory and was the first aircraft reactivated for USAF reconnaissance purposes in 1995. It has since returned to Dryden along with SR-71A 61-7967.

  16. SR-71B - Mach 3 Trainer in Flight at Sunset

    NASA Technical Reports Server (NTRS)

    1995-01-01

    The setting sun peeks beneath a SR-71B Blackbird, silhouetted against the orange hues of the western sky on a 1995 flight from at NASA's Dryden Flight Research Center, Edwards, California. Two SR-71 aircraft have been used by NASA as testbeds for high-speed and high-altitude aeronautical research. The aircraft, an SR-71A and an SR-71B pilot trainer aircraft, have been based here at NASA's Dryden Flight Research Center, Edwards, California. They were transferred to NASA after the U.S. Air Force program was cancelled. As research platforms, the aircraft can cruise at Mach 3 for more than one hour. For thermal experiments, this can produce heat soak temperatures of over 600 degrees Fahrenheit (F). This operating environment makes these aircraft excellent platforms to carry out research and experiments in a variety of areas -- aerodynamics, propulsion, structures, thermal protection materials, high-speed and high-temperature instrumentation, atmospheric studies, and sonic boom characterization. The SR-71 was used in a program to study ways of reducing sonic booms or over pressures that are heard on the ground, much like sharp thunderclaps, when an aircraft exceeds the speed of sound. Data from this Sonic Boom Mitigation Study could eventually lead to aircraft designs that would reduce the 'peak' overpressures of sonic booms and minimize the startling affect they produce on the ground. One of the first major experiments to be flown in the NASA SR-71 program was a laser air data collection system. It used laser light instead of air pressure to produce airspeed and attitude reference data, such as angle of attack and sideslip, which are normally obtained with small tubes and vanes extending into the airstream. One of Dryden's SR-71s was used for the Linear Aerospike Rocket Engine, or LASRE Experiment. Another earlier project consisted of a series of flights using the SR-71 as a science camera platform for NASA's Jet Propulsion Laboratory in Pasadena, California. An upward-looking ultraviolet video camera placed in the SR-71's nosebay studied a variety of celestial objects in wavelengths that are blocked to ground-based astronomers. Earlier in its history, Dryden had a decade of past experience at sustained speeds above Mach 3. Two YF-12A aircraft and an SR-71 designated as a YF-12C were flown at the center between December 1969 and November 1979 in a joint NASA/USAF program to learn more about the capabilities and limitations of high-speed, high-altitude flight. The YF-12As were prototypes of a planned interceptor aircraft based on a design that later evolved into the SR-71 reconnaissance aircraft. Dave Lux was the NASA SR-71 project manger for much of the decade of the 1990s, followed by Steve Schmidt. Developed for the USAF as reconnaissance aircraft more than 30 years ago, SR-71s are still the world's fastest and highest-flying production aircraft. The aircraft can fly at speeds of more than 2,200 miles per hour (Mach 3+, or more than three times the speed of sound) and at altitudes of over 85,000 feet. The Lockheed Skunk Works (now Lockheed Martin) built the original SR-71 aircraft. Each aircraft is 107.4 feet long, has a wingspan of 55.6 feet, and is 18.5 feet high (from the ground to the top of the rudders, when parked). Gross takeoff weight is about 140,000 pounds, including a possible fuel weight of 80,280 pounds. The airframes are built almost entirely of titanium and titanium alloys to withstand heat generated by sustained Mach 3 flight. Aerodynamic control surfaces consist of all-moving vertical tail surfaces, ailerons on the outer wings, and elevators on the trailing edges between the engine exhaust nozzles. The two SR-71s at Dryden have been assigned the following NASA tail numbers: NASA 844 (A model), military serial 61-7980 and NASA 831 (B model), military serial 61-7956. From 1990 through 1994, Dryden also had another 'A' model, NASA 832, military serial 61-7971. This aircraft was returned to the USAF inventory and was the first aircraft reactivated for USAF reconnaissance purposes in 1995. It has since returned to Dryden along with SR-71A 61-7967.

  17. SR-71 Tail #844 Landing at Edwards Air Force Base

    NASA Technical Reports Server (NTRS)

    1996-01-01

    With distinctive heat waves trailing behind its engines, NASA Dryden Flight Research Center's SR-71A, tail number 844, lands at the Edwards AFB runway after a 1996 flight. Two SR-71 aircraft have been used by NASA as testbeds for high-speed and high-altitude aeronautical research. The aircraft, an SR-71A and an SR-71B pilot trainer aircraft, have been based here at NASA's Dryden Flight Research Center, Edwards, California. They were transferred to NASA after the U.S. Air Force program was cancelled. As research platforms, the aircraft can cruise at Mach 3 for more than one hour. For thermal experiments, this can produce heat soak temperatures of over 600 degrees Fahrenheit (F). This operating environment makes these aircraft excellent platforms to carry out research and experiments in a variety of areas -- aerodynamics, propulsion, structures, thermal protection materials, high-speed and high-temperature instrumentation, atmospheric studies, and sonic boom characterization. The SR-71 was used in a program to study ways of reducing sonic booms or over pressures that are heard on the ground, much like sharp thunderclaps, when an aircraft exceeds the speed of sound. Data from this Sonic Boom Mitigation Study could eventually lead to aircraft designs that would reduce the 'peak' overpressures of sonic booms and minimize the startling affect they produce on the ground. One of the first major experiments to be flown in the NASA SR-71 program was a laser air data collection system. It used laser light instead of air pressure to produce airspeed and attitude reference data, such as angle of attack and sideslip, which are normally obtained with small tubes and vanes extending into the airstream. One of Dryden's SR-71s was used for the Linear Aerospike Rocket Engine, or LASRE Experiment. Another earlier project consisted of a series of flights using the SR-71 as a science camera platform for NASA's Jet Propulsion Laboratory in Pasadena, California. An upward-looking ultraviolet video camera placed in the SR-71's nosebay studied a variety of celestial objects in wavelengths that are blocked to ground-based astronomers. Earlier in its history, Dryden had a decade of past experience at sustained speeds above Mach 3. Two YF-12A aircraft and an SR-71 designated as a YF-12C were flown at the center between December 1969 and November 1979 in a joint NASA/USAF program to learn more about the capabilities and limitations of high-speed, high-altitude flight. The YF-12As were prototypes of a planned interceptor aircraft based on a design that later evolved into the SR-71 reconnaissance aircraft. Dave Lux was the NASA SR-71 project manger for much of the decade of the 1990s, followed by Steve Schmidt. Developed for the USAF as reconnaissance aircraft more than 30 years ago, SR-71s are still the world's fastest and highest-flying production aircraft. The aircraft can fly at speeds of more than 2,200 miles per hour (Mach 3+, or more than three times the speed of sound) and at altitudes of over 85,000 feet. The Lockheed Skunk Works (now Lockheed Martin) built the original SR-71 aircraft. Each aircraft is 107.4 feet long, has a wingspan of 55.6 feet, and is 18.5 feet high (from the ground to the top of the rudders, when parked). Gross takeoff weight is about 140,000 pounds, including a possible fuel weight of 80,280 pounds. The airframes are built almost entirely of titanium and titanium alloys to withstand heat generated by sustained Mach 3 flight. Aerodynamic control surfaces consist of all-moving vertical tail surfaces, ailerons on the outer wings, and elevators on the trailing edges between the engine exhaust nozzles. The two SR-71s at Dryden have been assigned the following NASA tail numbers: NASA 844 (A model), military serial 61-7980 and NASA 831 (B model), military serial 61-7956. From 1990 through 1994, Dryden also had another 'A' model, NASA 832, military serial 61-7971. This aircraft was returned to the USAF inventory and was the first aircraft reactivated for USAF reconnaissance purposes in 1995. It has since returned to Dryden along with SR-71A 61-7967.

  18. SR-71A on Ramp with Dual Max Afterburner Engines Firing

    NASA Technical Reports Server (NTRS)

    1998-01-01

    This night shot shows one of NASA's SR-71 Blackbird research aircraft on the ramp at the Dryden Flight Research Center, Edwards, California, with both engines running in max afterburner. Two SR-71 aircraft have been used by NASA as testbeds for high-speed and high-altitude aeronautical research. The aircraft, an SR-71A and an SR-71B pilot trainer aircraft, have been based here at NASA's Dryden Flight Research Center, Edwards, California. They were transferred to NASA after the U.S. Air Force program was cancelled. As research platforms, the aircraft can cruise at Mach 3 for more than one hour. For thermal experiments, this can produce heat soak temperatures of over 600 degrees Fahrenheit (F). This operating environment makes these aircraft excellent platforms to carry out research and experiments in a variety of areas -- aerodynamics, propulsion, structures, thermal protection materials, high-speed and high-temperature instrumentation, atmospheric studies, and sonic boom characterization. The SR-71 was used in a program to study ways of reducing sonic booms or over pressures that are heard on the ground, much like sharp thunderclaps, when an aircraft exceeds the speed of sound. Data from this Sonic Boom Mitigation Study could eventually lead to aircraft designs that would reduce the 'peak' overpressures of sonic booms and minimize the startling affect they produce on the ground. One of the first major experiments to be flown in the NASA SR-71 program was a laser air data collection system. It used laser light instead of air pressure to produce airspeed and attitude reference data, such as angle of attack and sideslip, which are normally obtained with small tubes and vanes extending into the airstream. One of Dryden's SR-71s was used for the Linear Aerospike Rocket Engine, or LASRE Experiment. Another earlier project consisted of a series of flights using the SR-71 as a science camera platform for NASA's Jet Propulsion Laboratory in Pasadena, California. An upward-looking ultraviolet video camera placed in the SR-71's nosebay studied a variety of celestial objects in wavelengths that are blocked to ground-based astronomers. Earlier in its history, Dryden had a decade of past experience at sustained speeds above Mach 3. Two YF-12A aircraft and an SR-71 designated as a YF-12C were flown at the center between December 1969 and November 1979 in a joint NASA/USAF program to learn more about the capabilities and limitations of high-speed, high-altitude flight. The YF-12As were prototypes of a planned interceptor aircraft based on a design that later evolved into the SR-71 reconnaissance aircraft. Dave Lux was the NASA SR-71 project manger for much of the decade of the 1990s, followed by Steve Schmidt. Developed for the USAF as reconnaissance aircraft more than 30 years ago, SR-71s are still the world's fastest and highest-flying production aircraft. The aircraft can fly at speeds of more than 2,200 miles per hour (Mach 3+, or more than three times the speed of sound) and at altitudes of over 85,000 feet. The Lockheed Skunk Works (now Lockheed Martin) built the original SR-71 aircraft. Each aircraft is 107.4 feet long, has a wingspan of 55.6 feet, and is 18.5 feet high (from the ground to the top of the rudders, when parked). Gross takeoff weight is about 140,000 pounds, including a possible fuel weight of 80,280 pounds. The airframes are built almost entirely of titanium and titanium alloys to withstand heat generated by sustained Mach 3 flight. Aerodynamic control surfaces consist of all-moving vertical tail surfaces, ailerons on the outer wings, and elevators on the trailing edges between the engine exhaust nozzles. The two SR-71s at Dryden have been assigned the following NASA tail numbers: NASA 844 (A model), military serial 61-7980 and NASA 831 (B model), military serial 61-7956. From 1990 through 1994, Dryden also had another 'A' model, NASA 832, military serial 61-7971. This aircraft was returned to the USAF inventory and was the first aircraft reactivated for USAF reconnaissance purposes in 1995. It has since returned to Dryden along with SR-71A 61-7967.

  19. SR-71A in Flight with Test Fixture Mounted Atop the Aft Section of the Aircraft

    NASA Technical Reports Server (NTRS)

    1999-01-01

    This close-up, head-on view of NASA's SR-71A Blackbird in flight shows the aircraft with an experimental test fixture mounted on the back of the airplane. Two SR-71 aircraft have been used by NASA as testbeds for high-speed and high-altitude aeronautical research. The aircraft, an SR-71A and an SR-71B pilot trainer aircraft, have been based here at NASA's Dryden Flight Research Center, Edwards, California. They were transferred to NASA after the U.S. Air Force program was cancelled. As research platforms, the aircraft can cruise at Mach 3 for more than one hour. For thermal experiments, this can produce heat soak temperatures of over 600 degrees Fahrenheit (F). This operating environment makes these aircraft excellent platforms to carry out research and experiments in a variety of areas -- aerodynamics, propulsion, structures, thermal protection materials, high-speed and high-temperature instrumentation, atmospheric studies, and sonic boom characterization. The SR-71 was used in a program to study ways of reducing sonic booms or over pressures that are heard on the ground, much like sharp thunderclaps, when an aircraft exceeds the speed of sound. Data from this Sonic Boom Mitigation Study could eventually lead to aircraft designs that would reduce the 'peak' overpressures of sonic booms and minimize the startling affect they produce on the ground. One of the first major experiments to be flown in the NASA SR-71 program was a laser air data collection system. It used laser light instead of air pressure to produce airspeed and attitude reference data, such as angle of attack and sideslip, which are normally obtained with small tubes and vanes extending into the airstream. One of Dryden's SR-71s was used for the Linear Aerospike Rocket Engine, or LASRE Experiment. Another earlier project consisted of a series of flights using the SR-71 as a science camera platform for NASA's Jet Propulsion Laboratory in Pasadena, California. An upward-looking ultraviolet video camera placed in the SR-71's nosebay studied a variety of celestial objects in wavelengths that are blocked to ground-based astronomers. Earlier in its history, Dryden had a decade of past experience at sustained speeds above Mach 3. Two YF-12A aircraft and an SR-71 designated as a YF-12C were flown at the center between December 1969 and November 1979 in a joint NASA/USAF program to learn more about the capabilities and limitations of high-speed, high-altitude flight. The YF-12As were prototypes of a planned interceptor aircraft based on a design that later evolved into the SR-71 reconnaissance aircraft. Dave Lux was the NASA SR-71 project manger for much of the decade of the 1990s, followed by Steve Schmidt. Developed for the USAF as reconnaissance aircraft more than 30 years ago, SR-71s are still the world's fastest and highest-flying production aircraft. The aircraft can fly at speeds of more than 2,200 miles per hour (Mach 3+, or more than three times the speed of sound) and at altitudes of over 85,000 feet. The Lockheed Skunk Works (now Lockheed Martin) built the original SR-71 aircraft. Each aircraft is 107.4 feet long, has a wingspan of 55.6 feet, and is 18.5 feet high (from the ground to the top of the rudders, when parked). Gross takeoff weight is about 140,000 pounds, including a possible fuel weight of 80,280 pounds. The airframes are built almost entirely of titanium and titanium alloys to withstand heat generated by sustained Mach 3 flight. Aerodynamic control surfaces consist of all-moving vertical tail surfaces, ailerons on the outer wings, and elevators on the trailing edges between the engine exhaust nozzles. The two SR-71s at Dryden have been assigned the following NASA tail numbers: NASA 844 (A model), military serial 61-7980 and NASA 831 (B model), military serial 61-7956. From 1990 through 1994, Dryden also had another 'A' model, NASA 832, military serial 61-7971. This aircraft was returned to the USAF inventory and was the first aircraft reactivated for USAF reconnaissance purposes in 1995. It has since returned to Dryden along with SR-71A 61-7967.

  20. SR-71B - in Flight - View from Air Force Tanker

    NASA Technical Reports Server (NTRS)

    1997-01-01

    This look-down view shows NASA 831, an SR-71B flown by Dryden Flight Research Center, Edwards, California, as it cruises over the Mojave Desert. The photo was from an Air Force refueling tanker taken on a 1997 mission. Two SR-71 aircraft have been used by NASA as testbeds for high-speed and high-altitude aeronautical research. The aircraft, an SR-71A and an SR-71B pilot trainer aircraft, have been based here at NASA's Dryden Flight Research Center, Edwards, California. They were transferred to NASA after the U.S. Air Force program was cancelled. As research platforms, the aircraft can cruise at Mach 3 for more than one hour. For thermal experiments, this can produce heat soak temperatures of over 600 degrees Fahrenheit (F). This operating environment makes these aircraft excellent platforms to carry out research and experiments in a variety of areas -- aerodynamics, propulsion, structures, thermal protection materials, high-speed and high-temperature instrumentation, atmospheric studies, and sonic boom characterization. The SR-71 was used in a program to study ways of reducing sonic booms or over pressures that are heard on the ground, much like sharp thunderclaps, when an aircraft exceeds the speed of sound. Data from this Sonic Boom Mitigation Study could eventually lead to aircraft designs that would reduce the 'peak' overpressures of sonic booms and minimize the startling affect they produce on the ground. One of the first major experiments to be flown in the NASA SR-71 program was a laser air data collection system. It used laser light instead of air pressure to produce airspeed and attitude reference data, such as angle of attack and sideslip, which are normally obtained with small tubes and vanes extending into the airstream. One of Dryden's SR-71s was used for the Linear Aerospike Rocket Engine, or LASRE Experiment. Another earlier project consisted of a series of flights using the SR-71 as a science camera platform for NASA's Jet Propulsion Laboratory in Pasadena, California. An upward-looking ultraviolet video camera placed in the SR-71's nosebay studied a variety of celestial objects in wavelengths that are blocked to ground-based astronomers. Earlier in its history, Dryden had a decade of past experience at sustained speeds above Mach 3. Two YF-12A aircraft and an SR-71 designated as a YF-12C were flown at the center between December 1969 and November 1979 in a joint NASA/USAF program to learn more about the capabilities and limitations of high-speed, high-altitude flight. The YF-12As were prototypes of a planned interceptor aircraft based on a design that later evolved into the SR-71 reconnaissance aircraft. Dave Lux was the NASA SR-71 project manger for much of the decade of the 1990s, followed by Steve Schmidt. Developed for the USAF as reconnaissance aircraft more than 30 years ago, SR-71s are still the world's fastest and highest-flying production aircraft. The aircraft can fly at speeds of more than 2,200 miles per hour (Mach 3+, or more than three times the speed of sound) and at altitudes of over 85,000 feet. The Lockheed Skunk Works (now Lockheed Martin) built the original SR-71 aircraft. Each aircraft is 107.4 feet long, has a wingspan of 55.6 feet, and is 18.5 feet high (from the ground to the top of the rudders, when parked). Gross takeoff weight is about 140,000 pounds, including a possible fuel weight of 80,280 pounds. The airframes are built almost entirely of titanium and titanium alloys to withstand heat generated by sustained Mach 3 flight. Aerodynamic control surfaces consist of all-moving vertical tail surfaces, ailerons on the outer wings, and elevators on the trailing edges between the engine exhaust nozzles. The two SR-71s at Dryden have been assigned the following NASA tail numbers: NASA 844 (A model), military serial 61-7980 and NASA 831 (B model), military serial 61-7956. From 1990 through 1994, Dryden also had another 'A' model, NASA 832, military serial 61-7971. This aircraft was returned to the USAF inventory and was the first aircraft reactivated for USAF reconnaissance purposes in 1995. It has since returned to Dryden along with SR-71A 61-7967.

  1. SR-71 Ship #1 on Ramp

    NASA Technical Reports Server (NTRS)

    1994-01-01

    This look-down, front view of NASA's SR-71A aircraft shows the Blackbird on the ramp at the Dryden Flight Research Center, Edwards, California. Two SR-71 aircraft have been used by NASA as testbeds for high-speed and high-altitude aeronautical research. The aircraft, an SR-71A and an SR-71B pilot trainer aircraft, have been based here at NASA's Dryden Flight Research Center, Edwards, California. They were transferred to NASA after the U.S. Air Force program was cancelled. As research platforms, the aircraft can cruise at Mach 3 for more than one hour. For thermal experiments, this can produce heat soak temperatures of over 600 degrees Fahrenheit (F). This operating environment makes these aircraft excellent platforms to carry out research and experiments in a variety of areas -- aerodynamics, propulsion, structures, thermal protection materials, high-speed and high-temperature instrumentation, atmospheric studies, and sonic boom characterization. The SR-71 was used in a program to study ways of reducing sonic booms or over pressures that are heard on the ground, much like sharp thunderclaps, when an aircraft exceeds the speed of sound. Data from this Sonic Boom Mitigation Study could eventually lead to aircraft designs that would reduce the 'peak' overpressures of sonic booms and minimize the startling affect they produce on the ground. One of the first major experiments to be flown in the NASA SR-71 program was a laser air data collection system. It used laser light instead of air pressure to produce airspeed and attitude reference data, such as angle of attack and sideslip, which are normally obtained with small tubes and vanes extending into the airstream. One of Dryden's SR-71s was used for the Linear Aerospike Rocket Engine, or LASRE Experiment. Another earlier project consisted of a series of flights using the SR-71 as a science camera platform for NASA's Jet Propulsion Laboratory in Pasadena, California. An upward-looking ultraviolet video camera placed in the SR-71's nosebay studied a variety of celestial objects in wavelengths that are blocked to ground-based astronomers. Earlier in its history, Dryden had a decade of past experience at sustained speeds above Mach 3. Two YF-12A aircraft and an SR-71 designated as a YF-12C were flown at the center between December 1969 and November 1979 in a joint NASA/USAF program to learn more about the capabilities and limitations of high-speed, high-altitude flight. The YF-12As were prototypes of a planned interceptor aircraft based on a design that later evolved into the SR-71 reconnaissance aircraft. Dave Lux was the NASA SR-71 project manger for much of the decade of the 1990s, followed by Steve Schmidt. Developed for the USAF as reconnaissance aircraft more than 30 years ago, SR-71s are still the world's fastest and highest-flying production aircraft. The aircraft can fly at speeds of more than 2,200 miles per hour (Mach 3+, or more than three times the speed of sound) and at altitudes of over 85,000 feet. The Lockheed Skunk Works (now Lockheed Martin) built the original SR-71 aircraft. Each aircraft is 107.4 feet long, has a wingspan of 55.6 feet, and is 18.5 feet high (from the ground to the top of the rudders, when parked). Gross takeoff weight is about 140,000 pounds, including a possible fuel weight of 80,280 pounds. The airframes are built almost entirely of titanium and titanium alloys to withstand heat generated by sustained Mach 3 flight. Aerodynamic control surfaces consist of all-moving vertical tail surfaces, ailerons on the outer wings, and elevators on the trailing edges between the engine exhaust nozzles. The two SR-71s at Dryden have been assigned the following NASA tail numbers: NASA 844 (A model), military serial 61-7980 and NASA 831 (B model), military serial 61-7956. From 1990 through 1994, Dryden also had another 'A' model, NASA 832, military serial 61-7971. This aircraft was returned to the USAF inventory and was the first aircraft reactivated for USAF reconnaissance purposes in 1995. It has since returned to Dryden along with SR-71A 61-7967.

  2. SR-71 - In-flight from Tanker

    NASA Technical Reports Server (NTRS)

    1994-01-01

    Dryden's SR-71B, NASA 831, slices across the snow-covered southern Sierra Nevada Mountains of California after being refueled by an Air Force tanker during a 1994 flight. Two SR-71 aircraft have been used by NASA as testbeds for high-speed and high-altitude aeronautical research. The aircraft, an SR-71A and an SR-71B pilot trainer aircraft, have been based here at NASA's Dryden Flight Research Center, Edwards, California. They were transferred to NASA after the U.S. Air Force program was cancelled. As research platforms, the aircraft can cruise at Mach 3 for more than one hour. For thermal experiments, this can produce heat soak temperatures of over 600 degrees Fahrenheit (F). This operating environment makes these aircraft excellent platforms to carry out research and experiments in a variety of areas -- aerodynamics, propulsion, structures, thermal protection materials, high-speed and high-temperature instrumentation, atmospheric studies, and sonic boom characterization. The SR-71 was used in a program to study ways of reducing sonic booms or over pressures that are heard on the ground, much like sharp thunderclaps, when an aircraft exceeds the speed of sound. Data from this Sonic Boom Mitigation Study could eventually lead to aircraft designs that would reduce the 'peak' overpressures of sonic booms and minimize the startling affect they produce on the ground. One of the first major experiments to be flown in the NASA SR-71 program was a laser air data collection system. It used laser light instead of air pressure to produce airspeed and attitude reference data, such as angle of attack and sideslip, which are normally obtained with small tubes and vanes extending into the airstream. One of Dryden's SR-71s was used for the Linear Aerospike Rocket Engine, or LASRE Experiment. Another earlier project consisted of a series of flights using the SR-71 as a science camera platform for NASA's Jet Propulsion Laboratory in Pasadena, California. An upward-looking ultraviolet video camera placed in the SR-71's nosebay studied a variety of celestial objects in wavelengths that are blocked to ground-based astronomers. Earlier in its history, Dryden had a decade of past experience at sustained speeds above Mach 3. Two YF-12A aircraft and an SR-71 designated as a YF-12C were flown at the center between December 1969 and November 1979 in a joint NASA/USAF program to learn more about the capabilities and limitations of high-speed, high-altitude flight. The YF-12As were prototypes of a planned interceptor aircraft based on a design that later evolved into the SR-71 reconnaissance aircraft. Dave Lux was the NASA SR-71 project manger for much of the decade of the 1990s, followed by Steve Schmidt. Developed for the USAF as reconnaissance aircraft more than 30 years ago, SR-71s are still the world's fastest and highest-flying production aircraft. The aircraft can fly at speeds of more than 2,200 miles per hour (Mach 3+, or more than three times the speed of sound) and at altitudes of over 85,000 feet. The Lockheed Skunk Works (now Lockheed Martin) built the original SR-71 aircraft. Each aircraft is 107.4 feet long, has a wingspan of 55.6 feet, and is 18.5 feet high (from the ground to the top of the rudders, when parked). Gross takeoff weight is about 140,000 pounds, including a possible fuel weight of 80,280 pounds. The airframes are built almost entirely of titanium and titanium alloys to withstand heat generated by sustained Mach 3 flight. Aerodynamic control surfaces consist of all-moving vertical tail surfaces, ailerons on the outer wings, and elevators on the trailing edges between the engine exhaust nozzles. The two SR-71s at Dryden have been assigned the following NASA tail numbers: NASA 844 (A model), military serial 61-7980 and NASA 831 (B model), military serial 61-7956. From 1990 through 1994, Dryden also had another 'A' model, NASA 832, military serial 61-7971. This aircraft was returned to the USAF inventory and was the first aircraft reactivated for USAF reconnaissance purposes in 1995. It has since returned to Dryden along with SR-71A 61-7967.

  3. SR-71B - in flight over snow-capped mountains

    NASA Technical Reports Server (NTRS)

    1995-01-01

    Dryden's SR-71B, NASA 831, slices across the snowy southern Sierra Nevada Mountains of California after being refueled by an Air Force Flight Test Center tanker during a recent flight. The Mach 3 aircraft, on loan to NASA by the U.S. Air Force, were flown by the Dryden Flight Research Center, Edwards, California, during the decade of the 1990s as testbeds for high-speed, high-altitude aeronautical research. Capable of flying more than 2200 mph and at altitudes of over 80,000 feet, they were excellent platforms for research and experiments in aerodynamics, propulsion, structures, thermal protection materials, atmospheric studies, and sonic boom characterization. Two SR-71 aircraft have been used by NASA as testbeds for high-speed and high-altitude aeronautical research. The aircraft, an SR-71A and an SR-71B pilot trainer aircraft, have been based here at NASA's Dryden Flight Research Center, Edwards, California. They were transferred to NASA after the U.S. Air Force program was cancelled. As research platforms, the aircraft can cruise at Mach 3 for more than one hour. For thermal experiments, this can produce heat soak temperatures of over 600 degrees Fahrenheit (F). This operating environment makes these aircraft excellent platforms to carry out research and experiments in a variety of areas -- aerodynamics, propulsion, structures, thermal protection materials, high-speed and high-temperature instrumentation, atmospheric studies, and sonic boom characterization. The SR-71 was used in a program to study ways of reducing sonic booms or over pressures that are heard on the ground much like sharp thunderclaps when an aircraft exceeds the speed of sound. Data from this Sonic Boom Mitigation Study could eventually lead to aircraft designs that would reduce the 'peak' overpressures of sonic booms and minimize the startle affect they produce on the ground. One of the first major experiments to be flown in the NASA SR-71 program was a laser air data collection system. It used laser light instead of air pressure to produce airspeed and attitude reference data, such as angle of attack and sideslip, which are normally obtained with small tubes and vanes extending into the airstream. One of Dryden's SR-71s was used for the Linear Aerospike, or LASRE Experiment. Another earlier project consisted of a series of flights using the SR-71 as a science camera platform for NASA's Jet Propulsion Laboratory in Pasadena, California. An upward-looking ultraviolet video camera placed in the SR-71's nosebay studied a variety of celestial objects in wavelengths that are blocked to ground-based astronomers. Dryden has had a decade of past experience at sustained speeds above Mach 3. Two YF-12A aircraft and an SR-71 designated as a YF-12C were flown at the center between December 1969 and November 1979 in a joint NASA/USAF program to learn more about the capabilities and limitations of high-speed, high-altitude flight. The YF-12As were prototypes of a planned interceptor aircraft based on a design that later evolved into the SR-71 reconnaissance aircraft. Dave Lux was the NASA SR-71 project manger for much of the decade of the 1990s, followed by Steve Schmidt. Developed for the USAF as reconnaissance aircraft more than 30 years ago, SR-71s are still the world's fastest and highest-flying production aircraft. The aircraft can fly at speeds of more than 2,200 miles per hour (Mach 3+ or more than three times the speed of sound) and at altitudes of over 85,000 feet. The Lockheed Skunk Works (now Lockheed Martin) built the original SR-71 aircraft. Each aircraft is 107.4 feet long, has a wingspan of 55.6 feet, and is 18.5 feet high (from the ground to the top of the rudders, when parked). Gross takeoff weight is about 140,000 pounds, including a possible fuel weight of 80,280 pounds. The airframes are built almost entirely of titanium and titanium alloys to withstand heat generated by sustained Mach 3 flight. Aerodynamic control surfaces consist of all-moving vertical tail surfaces, ailerons on the outer wings, and elevators on the trailing edges between the engine exhaust nozzles. The two SR-71s at Dryden have been assigned the following NASA tail numbers: NASA 844 (A model), military serial 61-7980 and NASA 831 (B model), military serial 61-7956. From 1990 through 1994, Dryden also had another 'A' model, NASA 832, military serial 61-7971. This aircraft was returned to the USAF inventory and was the first aircraft reactivated for USAF reconnaissance purposes in 1995. It has since returned to Dryden along with SR-71A 61-7967.

  4. SR-71A - in Flight from Below at Takeoff

    NASA Technical Reports Server (NTRS)

    1997-01-01

    With landing gear retracting, NASA Dryden Flight Research Center's SR-71A Blackbird, tail number 844, powers its way off the Edwards AFB runway with two Pratt & Whitney JT11D-20 engines rated at 34,000 pounds of thrust each, on a 1997 flight. Two SR-71 aircraft have been used by NASA as testbeds for high-speed and high-altitude aeronautical research. The aircraft, an SR-71A and an SR-71B pilot trainer aircraft, have been based here at NASA's Dryden Flight Research Center, Edwards, California. They were transferred to NASA after the U.S. Air Force program was cancelled. As research platforms, the aircraft can cruise at Mach 3 for more than one hour. For thermal experiments, this can produce heat soak temperatures of over 600 degrees Fahrenheit (F). This operating environment makes these aircraft excellent platforms to carry out research and experiments in a variety of areas -- aerodynamics, propulsion, structures, thermal protection materials, high-speed and high-temperature instrumentation, atmospheric studies, and sonic boom characterization. The SR-71 was used in a program to study ways of reducing sonic booms or over pressures that are heard on the ground, much like sharp thunderclaps, when an aircraft exceeds the speed of sound. Data from this Sonic Boom Mitigation Study could eventually lead to aircraft designs that would reduce the 'peak' overpressures of sonic booms and minimize the startling affect they produce on the ground. One of the first major experiments to be flown in the NASA SR-71 program was a laser air data collection system. It used laser light instead of air pressure to produce airspeed and attitude reference data, such as angle of attack and sideslip, which are normally obtained with small tubes and vanes extending into the airstream. One of Dryden's SR-71s was used for the Linear Aerospike Rocket Engine, or LASRE Experiment. Another earlier project consisted of a series of flights using the SR-71 as a science camera platform for NASA's Jet Propulsion Laboratory in Pasadena, California. An upward-looking ultraviolet video camera placed in the SR-71's nosebay studied a variety of celestial objects in wavelengths that are blocked to ground-based astronomers. Earlier in its history, Dryden had a decade of past experience at sustained speeds above Mach 3. Two YF-12A aircraft and an SR-71 designated as a YF-12C were flown at the center between December 1969 and November 1979 in a joint NASA/USAF program to learn more about the capabilities and limitations of high-speed, high-altitude flight. The YF-12As were prototypes of a planned interceptor aircraft based on a design that later evolved into the SR-71 reconnaissance aircraft. Dave Lux was the NASA SR-71 project manger for much of the decade of the 1990s, followed by Steve Schmidt. Developed for the USAF as reconnaissance aircraft more than 30 years ago, SR-71s are still the world's fastest and highest-flying production aircraft. The aircraft can fly at speeds of more than 2,200 miles per hour (Mach 3+, or more than three times the speed of sound) and at altitudes of over 85,000 feet. The Lockheed Skunk Works (now Lockheed Martin) built the original SR-71 aircraft. Each aircraft is 107.4 feet long, has a wingspan of 55.6 feet, and is 18.5 feet high (from the ground to the top of the rudders, when parked). Gross takeoff weight is about 140,000 pounds, including a possible fuel weight of 80,280 pounds. The airframes are built almost entirely of titanium and titanium alloys to withstand heat generated by sustained Mach 3 flight. Aerodynamic control surfaces consist of all-moving vertical tail surfaces, ailerons on the outer wings, and elevators on the trailing edges between the engine exhaust nozzles. The two SR-71s at Dryden have been assigned the following NASA tail numbers: NASA 844 (A model), military serial 61-7980 and NASA 831 (B model), military serial 61-7956. From 1990 through 1994, Dryden also had another 'A' model, NASA 832, military serial 61-7971. This aircraft was returned to the USAF inventory and was the first aircraft reactivated for USAF reconnaissance purposes in 1995. It has since returned to Dryden along with SR-71A 61-7967.

  5. Edward (Ed) T. Schneider in Front of SR-71 Blackbird

    NASA Technical Reports Server (NTRS)

    1995-01-01

    SR-71 research pilot Ed Schneider is pictured here in front of an SR-71 Blackbird on the ramp at the Dryden Flight Research Center, Edwards, California. Schneider became a NASA research pilot at Dryden in 1983. Data from the SR-71 program will be used to aid designers of future supersonic aircraft and propulsion systems. He retired as a NASA research pilot in September 2000. Two SR-71 aircraft have been used by NASA as testbeds for high-speed and high-altitude aeronautical research. The aircraft, an SR-71A and an SR-71B pilot trainer aircraft, have been based here at NASA's Dryden Flight Research Center, Edwards, California. They were transferred to NASA after the U.S. Air Force program was cancelled. As research platforms, the aircraft can cruise at Mach 3 for more than one hour. For thermal experiments, this can produce heat soak temperatures of over 600 degrees Fahrenheit (F). This operating environment makes these aircraft excellent platforms to carry out research and experiments in a variety of areas -- aerodynamics, propulsion, structures, thermal protection materials, high-speed and high-temperature instrumentation, atmospheric studies, and sonic boom characterization. The SR-71 was used in a program to study ways of reducing sonic booms or over pressures that are heard on the ground, much like sharp thunderclaps, when an aircraft exceeds the speed of sound. Data from this Sonic Boom Mitigation Study could eventually lead to aircraft designs that would reduce the 'peak' overpressures of sonic booms and minimize the startling affect they produce on the ground. One of the first major experiments to be flown in the NASA SR-71 program was a laser air data collection system. It used laser light instead of air pressure to produce airspeed and attitude reference data, such as angle of attack and sideslip, which are normally obtained with small tubes and vanes extending into the airstream. One of Dryden's SR-71s was used for the Linear Aerospike Rocket Engine, or LASRE Experiment. Another earlier project consisted of a series of flights using the SR-71 as a science camera platform for NASA's Jet Propulsion Laboratory in Pasadena, California. An upward-looking ultraviolet video camera placed in the SR-71's nosebay studied a variety of celestial objects in wavelengths that are blocked to ground-based astronomers. Earlier in its history, Dryden had a decade of past experience at sustained speeds above Mach 3. Two YF-12A aircraft and an SR-71 designated as a YF-12C were flown at the center between December 1969 and November 1979 in a joint NASA/USAF program to learn more about the capabilities and limitations of high-speed, high-altitude flight. The YF-12As were prototypes of a planned interceptor aircraft based on a design that later evolved into the SR-71 reconnaissance aircraft. Dave Lux was the NASA SR-71 project manger for much of the decade of the 1990s, followed by Steve Schmidt. Developed for the USAF as reconnaissance aircraft more than 30 years ago, SR-71s are still the world's fastest and highest-flying production aircraft. The aircraft can fly at speeds of more than 2,200 miles per hour (Mach 3+, or more than three times the speed of sound) and at altitudes of over 85,000 feet. The Lockheed Skunk Works (now Lockheed Martin) built the original SR-71 aircraft. Each aircraft is 107.4 feet long, has a wingspan of 55.6 feet, and is 18.5 feet high (from the ground to the top of the rudders, when parked). Gross takeoff weight is about 140,000 pounds, including a possible fuel weight of 80,280 pounds. The airframes are built almost entirely of titanium and titanium alloys to withstand heat generated by sustained Mach 3 flight. Aerodynamic control surfaces consist of all-moving vertical tail surfaces, ailerons on the outer wings, and elevators on the trailing edges between the engine exhaust nozzles. The two SR-71s at Dryden have been assigned the following NASA tail numbers: NASA 844 (A model), military serial 61-7980 and NASA 831 (B model), military serial 61-7956. From 1990 through 1994, Dryden also had another 'A' model, NASA 832, military serial 61-7971. This aircraft was returned to the USAF inventory and was the first aircraft reactivated for USAF reconnaissance purposes in 1995. It has since returned to Dryden along with SR-71A 61-7967.

  6. SR-71 Ship #1 on Ramp

    NASA Technical Reports Server (NTRS)

    1994-01-01

    This look-down view of NASA's SR-71A aircraft shows the Blackbird on the ramp at the Dryden Flight Research Center, Edwards, California, with Rogers Dry Lake in the background. NASA operated two SR-71s, an SR-71A and an SR- 71B pilot trainer aircraft at that point in time, both based at Dryden. Two SR-71 aircraft have been used by NASA as testbeds for high-speed and high-altitude aeronautical research. The aircraft, an SR-71A and an SR-71B pilot trainer aircraft, have been based here at NASA's Dryden Flight Research Center, Edwards, California. They were transferred to NASA after the U.S. Air Force program was cancelled. As research platforms, the aircraft can cruise at Mach 3 for more than one hour. For thermal experiments, this can produce heat soak temperatures of over 600 degrees Fahrenheit (F). This operating environment makes these aircraft excellent platforms to carry out research and experiments in a variety of areas -- aerodynamics, propulsion, structures, thermal protection materials, high-speed and high-temperature instrumentation, atmospheric studies, and sonic boom characterization. The SR-71 was used in a program to study ways of reducing sonic booms or over pressures that are heard on the ground, much like sharp thunderclaps, when an aircraft exceeds the speed of sound. Data from this Sonic Boom Mitigation Study could eventually lead to aircraft designs that would reduce the 'peak' overpressures of sonic booms and minimize the startling affect they produce on the ground. One of the first major experiments to be flown in the NASA SR-71 program was a laser air data collection system. It used laser light instead of air pressure to produce airspeed and attitude reference data, such as angle of attack and sideslip, which are normally obtained with small tubes and vanes extending into the airstream. One of Dryden's SR-71s was used for the Linear Aerospike Rocket Engine, or LASRE Experiment. Another earlier project consisted of a series of flights using the SR-71 as a science camera platform for NASA's Jet Propulsion Laboratory in Pasadena, California. An upward-looking ultraviolet video camera placed in the SR-71's nosebay studied a variety of celestial objects in wavelengths that are blocked to ground-based astronomers. Earlier in its history, Dryden had a decade of past experience at sustained speeds above Mach 3. Two YF-12A aircraft and an SR-71 designated as a YF-12C were flown at the center between December 1969 and November 1979 in a joint NASA/USAF program to learn more about the capabilities and limitations of high-speed, high-altitude flight. The YF-12As were prototypes of a planned interceptor aircraft based on a design that later evolved into the SR-71 reconnaissance aircraft. Dave Lux was the NASA SR-71 project manger for much of the decade of the 1990s, followed by Steve Schmidt. Developed for the USAF as reconnaissance aircraft more than 30 years ago, SR-71s are still the world's fastest and highest-flying production aircraft. The aircraft can fly at speeds of more than 2,200 miles per hour (Mach 3+, or more than three times the speed of sound) and at altitudes of over 85,000 feet. The Lockheed Skunk Works (now Lockheed Martin) built the original SR-71 aircraft. Each aircraft is 107.4 feet long, has a wingspan of 55.6 feet, and is 18.5 feet high (from the ground to the top of the rudders, when parked). Gross takeoff weight is about 140,000 pounds, including a possible fuel weight of 80,280 pounds. The airframes are built almost entirely of titanium and titanium alloys to withstand heat generated by sustained Mach 3 flight. Aerodynamic control surfaces consist of all-moving vertical tail surfaces, ailerons on the outer wings, and elevators on the trailing edges between the engine exhaust nozzles. The two SR-71s at Dryden have been assigned the following NASA tail numbers: NASA 844 (A model), military serial 61-7980 and NASA 831 (B model), military serial 61-7956. From 1990 through 1994, Dryden also had another 'A' model, NASA 832, military serial 61-7971. This aircraft was returned to the USAF inventory and was the first aircraft reactivated for USAF reconnaissance purposes in 1995. It has since returned to Dryden along with SR-71A 61-7967.

  7. SR-71 Pilot Stephen (Steve) D. Ishmael

    NASA Technical Reports Server (NTRS)

    1992-01-01

    NASA research pilot Stephen D. Ishmael is pictured here in front of an SR-71 Blackbird on the ramp at the Dryden Flight Research Center, Edwards, California. Ishmael was one of two NASA research pilots assigned to the SR-71 high speed research program in the early 1990s at NASA's Dryden Flight Research Facility (redesignated the Dryden Flight Research Center in 1994), Edwards, California. Ishmael became a NASA research pilot in 1977. Data from the SR-71 program will be used to aid designers of future supersonic aircraft and propulsion systems. Two SR-71 aircraft have been used by NASA as testbeds for high-speed and high-altitude aeronautical research. The aircraft, an SR-71A and an SR-71B pilot trainer aircraft, have been based here at NASA's Dryden Flight Research Center, Edwards, California. They were transferred to NASA after the U.S. Air Force program was cancelled. As research platforms, the aircraft can cruise at Mach 3 for more than one hour. For thermal experiments, this can produce heat soak temperatures of over 600 degrees Fahrenheit (F). This operating environment makes these aircraft excellent platforms to carry out research and experiments in a variety of areas -- aerodynamics, propulsion, structures, thermal protection materials, high-speed and high-temperature instrumentation, atmospheric studies, and sonic boom characterization. The SR-71 was used in a program to study ways of reducing sonic booms or over pressures that are heard on the ground, much like sharp thunderclaps, when an aircraft exceeds the speed of sound. Data from this Sonic Boom Mitigation Study could eventually lead to aircraft designs that would reduce the 'peak' overpressures of sonic booms and minimize the startling affect they produce on the ground. One of the first major experiments to be flown in the NASA SR-71 program was a laser air data collection system. It used laser light instead of air pressure to produce airspeed and attitude reference data, such as angle of attack and sideslip, which are normally obtained with small tubes and vanes extending into the airstream. One of Dryden's SR-71s was used for the Linear Aerospike Rocket Engine, or LASRE Experiment. Another earlier project consisted of a series of flights using the SR-71 as a science camera platform for NASA's Jet Propulsion Laboratory in Pasadena, California. An upward-looking ultraviolet video camera placed in the SR-71's nosebay studied a variety of celestial objects in wavelengths that are blocked to ground-based astronomers. Earlier in its history, Dryden had a decade of past experience at sustained speeds above Mach 3. Two YF-12A aircraft and an SR-71 designated as a YF-12C were flown at the center between December 1969 and November 1979 in a joint NASA/USAF program to learn more about the capabilities and limitations of high-speed, high-altitude flight. The YF-12As were prototypes of a planned interceptor aircraft based on a design that later evolved into the SR-71 reconnaissance aircraft. Dave Lux was the NASA SR-71 project manger for much of the decade of the 1990s, followed by Steve Schmidt. Developed for the USAF as reconnaissance aircraft more than 30 years ago, SR-71s are still the world's fastest and highest-flying production aircraft. The aircraft can fly at speeds of more than 2,200 miles per hour (Mach 3+, or more than three times the speed of sound) and at altitudes of over 85,000 feet. The Lockheed Skunk Works (now Lockheed Martin) built the original SR-71 aircraft. Each aircraft is 107.4 feet long, has a wingspan of 55.6 feet, and is 18.5 feet high (from the ground to the top of the rudders, when parked). Gross takeoff weight is about 140,000 pounds, including a possible fuel weight of 80,280 pounds. The airframes are built almost entirely of titanium and titanium alloys to withstand heat generated by sustained Mach 3 flight. Aerodynamic control surfaces consist of all-moving vertical tail surfaces, ailerons on the outer wings, and elevators on the trailing edges between the engine exhaust nozzles. The two SR-71s at Dryden have been assigned the following NASA tail numbers: NASA 844 (A model), military serial 61-7980 and NASA 831 (B model), military serial 61-7956. From 1990 through 1994, Dryden also had another 'A' model, NASA 832, military serial 61-7971. This aircraft was returned to the USAF inventory and was the first aircraft reactivated for USAF reconnaissance purposes in 1995. It has since returned to Dryden along with SR-71A 61-7967.

  8. SR-71 Research Engineer Marta Bohn-Meyer

    NASA Technical Reports Server (NTRS)

    1992-01-01

    This 1992 photo shows SR-71 flight engineer Marta Bohn-Meyer in front of one of NASA's SR-71 aircraft on the ramp at the Ames-Dryden Flight Research Facility (later, Dryden Flight Research Center), Edwards, California. An aerospace engineer who has been at Dryden since 1979, Bohn-Meyer is the first female crew member ever assigned to fly in the SR-71. Data from the SR-71 program carried out by NASA will be used to aid designers of future supersonic aircraft and propulsion systems. Two SR-71 aircraft have been used by NASA as testbeds for high-speed and high-altitude aeronautical research. The aircraft, an SR-71A and an SR-71B pilot trainer aircraft, have been based here at NASA's Dryden Flight Research Center, Edwards, California. They were transferred to NASA after the U.S. Air Force program was cancelled. As research platforms, the aircraft can cruise at Mach 3 for more than one hour. For thermal experiments, this can produce heat soak temperatures of over 600 degrees Fahrenheit (F). This operating environment makes these aircraft excellent platforms to carry out research and experiments in a variety of areas -- aerodynamics, propulsion, structures, thermal protection materials, high-speed and high-temperature instrumentation, atmospheric studies, and sonic boom characterization. The SR-71 was used in a program to study ways of reducing sonic booms or over pressures that are heard on the ground, much like sharp thunderclaps, when an aircraft exceeds the speed of sound. Data from this Sonic Boom Mitigation Study could eventually lead to aircraft designs that would reduce the 'peak' overpressures of sonic booms and minimize the startling affect they produce on the ground. One of the first major experiments to be flown in the NASA SR-71 program was a laser air data collection system. It used laser light instead of air pressure to produce airspeed and attitude reference data, such as angle of attack and sideslip, which are normally obtained with small tubes and vanes extending into the airstream. One of Dryden's SR-71s was used for the Linear Aerospike Rocket Engine, or LASRE Experiment. Another earlier project consisted of a series of flights using the SR-71 as a science camera platform for NASA's Jet Propulsion Laboratory in Pasadena, California. An upward-looking ultraviolet video camera placed in the SR-71's nosebay studied a variety of celestial objects in wavelengths that are blocked to ground-based astronomers. Earlier in its history, Dryden had a decade of past experience at sustained speeds above Mach 3. Two YF-12A aircraft and an SR-71 designated as a YF-12C were flown at the center between December 1969 and November 1979 in a joint NASA/USAF program to learn more about the capabilities and limitations of high-speed, high-altitude flight. The YF-12As were prototypes of a planned interceptor aircraft based on a design that later evolved into the SR-71 reconnaissance aircraft. Dave Lux was the NASA SR-71 project manger for much of the decade of the 1990s, followed by Steve Schmidt. Developed for the USAF as reconnaissance aircraft more than 30 years ago, SR-71s are still the world's fastest and highest-flying production aircraft. The aircraft can fly at speeds of more than 2,200 miles per hour (Mach 3+, or more than three times the speed of sound) and at altitudes of over 85,000 feet. The Lockheed Skunk Works (now Lockheed Martin) built the original SR-71 aircraft. Each aircraft is 107.4 feet long, has a wingspan of 55.6 feet, and is 18.5 feet high (from the ground to the top of the rudders, when parked). Gross takeoff weight is about 140,000 pounds, including a possible fuel weight of 80,280 pounds. The airframes are built almost entirely of titanium and titanium alloys to withstand heat generated by sustained Mach 3 flight. Aerodynamic control surfaces consist of all-moving vertical tail surfaces, ailerons on the outer wings, and elevators on the trailing edges between the engine exhaust nozzles. The two SR-71s at Dryden have been assigned the following NASA tail numbers: NASA 844 (A model), military serial 61-7980 and NASA 831 (B model), military serial 61-7956. From 1990 through 1994, Dryden also had another 'A' model, NASA 832, military serial 61-7971. This aircraft was returned to the USAF inventory and was the first aircraft reactivated for USAF reconnaissance purposes in 1995. It has since returned to Dryden along with SR-71A 61-7967.

  9. SR-71 Pilots and Crew (Smith, Meyer, Bohn-Meyer, Ishmael)

    NASA Technical Reports Server (NTRS)

    1991-01-01

    The two pilot-engineer teams that flew the SR-71 aircraft at the NASA Ames-Dryden Flight Research Facility (later, Dryden Flight Research Center, Edwards, California, are, from left, pilot Rogers Smith, flight engineers Robert Meyer and Marta Bohn-Meyer, and pilot Steven Ishmael. The Meyers are the first husband-wife team of aeronautical engineers at Dryden on flight status. Two SR-71 aircraft have been used by NASA as testbeds for high-speed and high-altitude aeronautical research. The aircraft, an SR-71A and an SR-71B pilot trainer aircraft, have been based here at NASA's Dryden Flight Research Center, Edwards, California. They were transferred to NASA after the U.S. Air Force program was cancelled. As research platforms, the aircraft can cruise at Mach 3 for more than one hour. For thermal experiments, this can produce heat soak temperatures of over 600 degrees Fahrenheit (F). This operating environment makes these aircraft excellent platforms to carry out research and experiments in a variety of areas -- aerodynamics, propulsion, structures, thermal protection materials, high-speed and high-temperature instrumentation, atmospheric studies, and sonic boom characterization. The SR-71 was used in a program to study ways of reducing sonic booms or over pressures that are heard on the ground, much like sharp thunderclaps, when an aircraft exceeds the speed of sound. Data from this Sonic Boom Mitigation Study could eventually lead to aircraft designs that would reduce the 'peak' overpressures of sonic booms and minimize the startling affect they produce on the ground. One of the first major experiments to be flown in the NASA SR-71 program was a laser air data collection system. It used laser light instead of air pressure to produce airspeed and attitude reference data, such as angle of attack and sideslip, which are normally obtained with small tubes and vanes extending into the airstream. One of Dryden's SR-71s was used for the Linear Aerospike Rocket Engine, or LASRE Experiment. Another earlier project consisted of a series of flights using the SR-71 as a science camera platform for NASA's Jet Propulsion Laboratory in Pasadena, California. An upward-looking ultraviolet video camera placed in the SR-71's nosebay studied a variety of celestial objects in wavelengths that are blocked to ground-based astronomers. Earlier in its history, Dryden had a decade of past experience at sustained speeds above Mach 3. Two YF-12A aircraft and an SR-71 designated as a YF-12C were flown at the center between December 1969 and November 1979 in a joint NASA/USAF program to learn more about the capabilities and limitations of high-speed, high-altitude flight. The YF-12As were prototypes of a planned interceptor aircraft based on a design that later evolved into the SR-71 reconnaissance aircraft. Dave Lux was the NASA SR-71 project manger for much of the decade of the 1990s, followed by Steve Schmidt. Developed for the USAF as reconnaissance aircraft more than 30 years ago, SR-71s are still the world's fastest and highest-flying production aircraft. The aircraft can fly at speeds of more than 2,200 miles per hour (Mach 3+, or more than three times the speed of sound) and at altitudes of over 85,000 feet. The Lockheed Skunk Works (now Lockheed Martin) built the original SR-71 aircraft. Each aircraft is 107.4 feet long, has a wingspan of 55.6 feet, and is 18.5 feet high (from the ground to the top of the rudders, when parked). Gross takeoff weight is about 140,000 pounds, including a possible fuel weight of 80,280 pounds. The airframes are built almost entirely of titanium and titanium alloys to withstand heat generated by sustained Mach 3 flight. Aerodynamic control surfaces consist of all-moving vertical tail surfaces, ailerons on the outer wings, and elevators on the trailing edges between the engine exhaust nozzles. The two SR-71s at Dryden have been assigned the following NASA tail numbers: NASA 844 (A model), military serial 61-7980 and NASA 831 (B model), military serial 61-7956. From 1990 through 1994, Dryden also had another 'A' model, NASA 832, military serial 61-7971. This aircraft was returned to the USAF inventory and was the first aircraft reactivated for USAF reconnaissance purposes in 1995. It has since returned to Dryden along with SR-71A 61-7967.

  10. SR-71 Pilots and Crew (Smith, Meyer, Bohn-Meyer, Ishmael)

    NASA Technical Reports Server (NTRS)

    1991-01-01

    The two pilot-engineer teams that flew the SR-71 aircraft at the NASA Ames-Dryden Flight Research Facility (later, Dryden Flight Research Center), Edwards, California, are, from top of ladder, pilot Rogers Smith, flight engineer Robert Meyer, pilot Steven Ishmael, and flight engineer Marta Bohn-Meyer. The Meyers are the first husband-wife team of aeronautical engineers at Dryden on flight status. Two SR-71 aircraft have been used by NASA as testbeds for high-speed and high-altitude aeronautical research. The aircraft, an SR-71A and an SR-71B pilot trainer aircraft, have been based here at NASA's Dryden Flight Research Center, Edwards, California. They were transferred to NASA after the U.S. Air Force program was cancelled. As research platforms, the aircraft can cruise at Mach 3 for more than one hour. For thermal experiments, this can produce heat soak temperatures of over 600 degrees Fahrenheit (F). This operating environment makes these aircraft excellent platforms to carry out research and experiments in a variety of areas -- aerodynamics, propulsion, structures, thermal protection materials, high-speed and high-temperature instrumentation, atmospheric studies, and sonic boom characterization. The SR-71 was used in a program to study ways of reducing sonic booms or over pressures that are heard on the ground, much like sharp thunderclaps, when an aircraft exceeds the speed of sound. Data from this Sonic Boom Mitigation Study could eventually lead to aircraft designs that would reduce the 'peak' overpressures of sonic booms and minimize the startling affect they produce on the ground. One of the first major experiments to be flown in the NASA SR-71 program was a laser air data collection system. It used laser light instead of air pressure to produce airspeed and attitude reference data, such as angle of attack and sideslip, which are normally obtained with small tubes and vanes extending into the airstream. One of Dryden's SR-71s was used for the Linear Aerospike Rocket Engine, or LASRE Experiment. Another earlier project consisted of a series of flights using the SR-71 as a science camera platform for NASA's Jet Propulsion Laboratory in Pasadena, California. An upward-looking ultraviolet video camera placed in the SR-71's nosebay studied a variety of celestial objects in wavelengths that are blocked to ground-based astronomers. Earlier in its history, Dryden had a decade of past experience at sustained speeds above Mach 3. Two YF-12A aircraft and an SR-71 designated as a YF-12C were flown at the center between December 1969 and November 1979 in a joint NASA/USAF program to learn more about the capabilities and limitations of high-speed, high-altitude flight. The YF-12As were prototypes of a planned interceptor aircraft based on a design that later evolved into the SR-71 reconnaissance aircraft. Dave Lux was the NASA SR-71 project manger for much of the decade of the 1990s, followed by Steve Schmidt. Developed for the USAF as reconnaissance aircraft more than 30 years ago, SR-71s are still the world's fastest and highest-flying production aircraft. The aircraft can fly at speeds of more than 2,200 miles per hour (Mach 3+, or more than three times the speed of sound) and at altitudes of over 85,000 feet. The Lockheed Skunk Works (now Lockheed Martin) built the original SR-71 aircraft. Each aircraft is 107.4 feet long, has a wingspan of 55.6 feet, and is 18.5 feet high (from the ground to the top of the rudders, when parked). Gross takeoff weight is about 140,000 pounds, including a possible fuel weight of 80,280 pounds. The airframes are built almost entirely of titanium and titanium alloys to withstand heat generated by sustained Mach 3 flight. Aerodynamic control surfaces consist of all-moving vertical tail surfaces, ailerons on the outer wings, and elevators on the trailing edges between the engine exhaust nozzles. The two SR-71s at Dryden have been assigned the following NASA tail numbers: NASA 844 (A model), military serial 61-7980 and NASA 831 (B model), military serial 61-7956. From 1990 through 1994, Dryden also had another 'A' model, NASA 832, military serial 61-7971. This aircraft was returned to the USAF inventory and was the first aircraft reactivated for USAF reconnaissance purposes in 1995. It has since returned to Dryden along with SR-71A 61-7967.

  11. SR-71 Pilot Rogers E. Smith

    NASA Technical Reports Server (NTRS)

    1992-01-01

    Research pilot Rogers E. Smith is shown here in front of the SR-71 Blackbird he flew for NASA. Rogers was one of the two original NASA research pilots assigned to the SR-71 high speed research program at NASA's Ames-Dryden Flight Research Facility (later, Dryden Flight Research Center, Edwards, California. Smith has been a NASA research pilot at Dryden since 1982. Data from the SR-71 program will be used to aid designers of future supersonic aircraft and propulsion systems. The SR-71 is capable of flying more than 2200 mph (Mach 3+) and at altitudes of over 80,000 feet. Two SR-71 aircraft have been used by NASA as testbeds for high-speed and high-altitude aeronautical research. The aircraft, an SR-71A and an SR-71B pilot trainer aircraft, have been based here at NASA's Dryden Flight Research Center, Edwards, California. They were transferred to NASA after the U.S. Air Force program was cancelled. As research platforms, the aircraft can cruise at Mach 3 for more than one hour. For thermal experiments, this can produce heat soak temperatures of over 600 degrees Fahrenheit (F). This operating environment makes these aircraft excellent platforms to carry out research and experiments in a variety of areas -- aerodynamics, propulsion, structures, thermal protection materials, high-speed and high-temperature instrumentation, atmospheric studies, and sonic boom characterization. The SR-71 was used in a program to study ways of reducing sonic booms or over pressures that are heard on the ground, much like sharp thunderclaps, when an aircraft exceeds the speed of sound. Data from this Sonic Boom Mitigation Study could eventually lead to aircraft designs that would reduce the 'peak' overpressures of sonic booms and minimize the startling affect they produce on the ground. One of the first major experiments to be flown in the NASA SR-71 program was a laser air data collection system. It used laser light instead of air pressure to produce airspeed and attitude reference data, such as angle of attack and sideslip, which are normally obtained with small tubes and vanes extending into the airstream. One of Dryden's SR-71s was used for the Linear Aerospike Rocket Engine, or LASRE Experiment. Another earlier project consisted of a series of flights using the SR-71 as a science camera platform for NASA's Jet Propulsion Laboratory in Pasadena, California. An upward-looking ultraviolet video camera placed in the SR-71's nosebay studied a variety of celestial objects in wavelengths that are blocked to ground-based astronomers. Earlier in its history, Dryden had a decade of past experience at sustained speeds above Mach 3. Two YF-12A aircraft and an SR-71 designated as a YF-12C were flown at the center between December 1969 and November 1979 in a joint NASA/USAF program to learn more about the capabilities and limitations of high-speed, high-altitude flight. The YF-12As were prototypes of a planned interceptor aircraft based on a design that later evolved into the SR-71 reconnaissance aircraft. Dave Lux was the NASA SR-71 project manger for much of the decade of the 1990s, followed by Steve Schmidt. Developed for the USAF as reconnaissance aircraft more than 30 years ago, SR-71s are still the world's fastest and highest-flying production aircraft. The aircraft can fly at speeds of more than 2,200 miles per hour (Mach 3+, or more than three times the speed of sound) and at altitudes of over 85,000 feet. The Lockheed Skunk Works (now Lockheed Martin) built the original SR-71 aircraft. Each aircraft is 107.4 feet long, has a wingspan of 55.6 feet, and is 18.5 feet high (from the ground to the top of the rudders, when parked). Gross takeoff weight is about 140,000 pounds, including a possible fuel weight of 80,280 pounds. The airframes are built almost entirely of titanium and titanium alloys to withstand heat generated by sustained Mach 3 flight. Aerodynamic control surfaces consist of all-moving vertical tail surfaces, ailerons on the outer wings, and elevators on the trailing edges between the engine exhaust nozzles. The two SR-71s at Dryden have been assigned the following NASA tail numbers: NASA 844 (A model), military serial 61-7980 and NASA 831 (B model), military serial 61-7956. From 1990 through 1994, Dryden also had another 'A' model, NASA 832, military serial 61-7971. This aircraft was returned to the USAF inventory and was the first aircraft reactivated for USAF reconnaissance purposes in 1995. It has since returned to Dryden along with SR-71A 61-7967.

  12. SR-71B - in Flight with F-18 Chase Aircraft - View from Air Force Tanker

    NASA Technical Reports Server (NTRS)

    1996-01-01

    NASA 831, an SR-71B operated by the Dryden Flight Research Center, Edwards, California, cruises over the Mojave Desert with an F/A-18 Hornet flying safety chase. They were photographed on a 1996 mission from an Air Force refueling tanker The F/A-18 Hornet is used primarily as a safety chase and support aircraft at Dryden. As support aircraft, the F-18s are used for safety chase, pilot proficiency and aerial photography. Two SR-71 aircraft have been used by NASA as testbeds for high-speed and high-altitude aeronautical research. The aircraft, an SR-71A and an SR-71B pilot trainer aircraft, have been based here at NASA's Dryden Flight Research Center, Edwards, California. They were transferred to NASA after the U.S. Air Force program was cancelled. As research platforms, the aircraft can cruise at Mach 3 for more than one hour. For thermal experiments, this can produce heat soak temperatures of over 600 degrees Fahrenheit (F). This operating environment makes these aircraft excellent platforms to carry out research and experiments in a variety of areas -- aerodynamics, propulsion, structures, thermal protection materials, high-speed and high-temperature instrumentation, atmospheric studies, and sonic boom characterization. The SR-71 was used in a program to study ways of reducing sonic booms or over pressures that are heard on the ground, much like sharp thunderclaps, when an aircraft exceeds the speed of sound. Data from this Sonic Boom Mitigation Study could eventually lead to aircraft designs that would reduce the 'peak' overpressures of sonic booms and minimize the startling affect they produce on the ground. One of the first major experiments to be flown in the NASA SR-71 program was a laser air data collection system. It used laser light instead of air pressure to produce airspeed and attitude reference data, such as angle of attack and sideslip, which are normally obtained with small tubes and vanes extending into the airstream. One of Dryden's SR-71s was used for the Linear Aerospike Rocket Engine, or LASRE Experiment. Another earlier project consisted of a series of flights using the SR-71 as a science camera platform for NASA's Jet Propulsion Laboratory in Pasadena, California. An upward-looking ultraviolet video camera placed in the SR-71's nosebay studied a variety of celestial objects in wavelengths that are blocked to ground-based astronomers. Earlier in its history, Dryden had a decade of past experience at sustained speeds above Mach 3. Two YF-12A aircraft and an SR-71 designated as a YF-12C were flown at the center between December 1969 and November 1979 in a joint NASA/USAF program to learn more about the capabilities and limitations of high-speed, high-altitude flight. The YF-12As were prototypes of a planned interceptor aircraft based on a design that later evolved into the SR-71 reconnaissance aircraft. Dave Lux was the NASA SR-71 project manger for much of the decade of the 1990s, followed by Steve Schmidt. Developed for the USAF as reconnaissance aircraft more than 30 years ago, SR-71s are still the world's fastest and highest-flying production aircraft. The aircraft can fly at speeds of more than 2,200 miles per hour (Mach 3+, or more than three times the speed of sound) and at altitudes of over 85,000 feet. The Lockheed Skunk Works (now Lockheed Martin) built the original SR-71 aircraft. Each aircraft is 107.4 feet long, has a wingspan of 55.6 feet, and is 18.5 feet high (from the ground to the top of the rudders, when parked). Gross takeoff weight is about 140,000 pounds, including a possible fuel weight of 80,280 pounds. The airframes are built almost entirely of titanium and titanium alloys to withstand heat generated by sustained Mach 3 flight. Aerodynamic control surfaces consist of all-moving vertical tail surfaces, ailerons on the outer wings, and elevators on the trailing edges between the engine exhaust nozzles. The two SR-71s at Dryden have been assigned the following NASA tail numbers: NASA 844 (A model), military serial 61-7980 and NASA 831 (B model), military serial 61-7956. From 1990 through 1994, Dryden also had another 'A' model, NASA 832, military serial 61-7971. This aircraft was returned to the USAF inventory and was the first aircraft reactivated for USAF reconnaissance purposes in 1995. It has since returned to Dryden along with SR-71A 61-7967.

  13. SR-71A Taking Off with Test Fixture Mounted Atop the Aft Section of the Aircraft and F-18 Chase Airc

    NASA Technical Reports Server (NTRS)

    1999-01-01

    This photo shows a NASA's SR-71A Blackbird, followed by a NASA F/A-18 chase plane, taking off from the runway at the Dryden Flight Research Center, Edwards, California, on a 1999 flight. Two SR-71 aircraft have been used by NASA as testbeds for high-speed and high-altitude aeronautical research. The aircraft, an SR-71A and an SR-71B pilot trainer aircraft, have been based here at NASA's Dryden Flight Research Center, Edwards, California. They were transferred to NASA after the U.S. Air Force program was cancelled. As research platforms, the aircraft can cruise at Mach 3 for more than one hour. For thermal experiments, this can produce heat soak temperatures of over 600 degrees Fahrenheit (F). This operating environment makes these aircraft excellent platforms to carry out research and experiments in a variety of areas -- aerodynamics, propulsion, structures, thermal protection materials, high-speed and high-temperature instrumentation, atmospheric studies, and sonic boom characterization. The SR-71 was used in a program to study ways of reducing sonic booms or over pressures that are heard on the ground, much like sharp thunderclaps, when an aircraft exceeds the speed of sound. Data from this Sonic Boom Mitigation Study could eventually lead to aircraft designs that would reduce the 'peak' overpressures of sonic booms and minimize the startling affect they produce on the ground. One of the first major experiments to be flown in the NASA SR-71 program was a laser air data collection system. It used laser light instead of air pressure to produce airspeed and attitude reference data, such as angle of attack and sideslip, which are normally obtained with small tubes and vanes extending into the airstream. One of Dryden's SR-71s was used for the Linear Aerospike Rocket Engine, or LASRE Experiment. Another earlier project consisted of a series of flights using the SR-71 as a science camera platform for NASA's Jet Propulsion Laboratory in Pasadena, California. An upward-looking ultraviolet video camera placed in the SR-71's nosebay studied a variety of celestial objects in wavelengths that are blocked to ground-based astronomers. Earlier in its history, Dryden had a decade of past experience at sustained speeds above Mach 3. Two YF-12A aircraft and an SR-71 designated as a YF-12C were flown at the center between December 1969 and November 1979 in a joint NASA/USAF program to learn more about the capabilities and limitations of high-speed, high-altitude flight. The YF-12As were prototypes of a planned interceptor aircraft based on a design that later evolved into the SR-71 reconnaissance aircraft. Dave Lux was the NASA SR-71 project manger for much of the decade of the 1990s, followed by Steve Schmidt. Developed for the USAF as reconnaissance aircraft more than 30 years ago, SR-71s are still the world's fastest and highest-flying production aircraft. The aircraft can fly at speeds of more than 2,200 miles per hour (Mach 3+, or more than three times the speed of sound) and at altitudes of over 85,000 feet. The Lockheed Skunk Works (now Lockheed Martin) built the original SR-71 aircraft. Each aircraft is 107.4 feet long, has a wingspan of 55.6 feet, and is 18.5 feet high (from the ground to the top of the rudders, when parked). Gross takeoff weight is about 140,000 pounds, including a possible fuel weight of 80,280 pounds. The airframes are built almost entirely of titanium and titanium alloys to withstand heat generated by sustained Mach 3 flight. Aerodynamic control surfaces consist of all-moving vertical tail surfaces, ailerons on the outer wings, and elevators on the trailing edges between the engine exhaust nozzles. The two SR-71s at Dryden have been assigned the following NASA tail numbers: NASA 844 (A model), military serial 61-7980 and NASA 831 (B model), military serial 61-7956. From 1990 through 1994, Dryden also had another 'A' model, NASA 832, military serial 61-7971. This aircraft was returned to the USAF inventory and was the first aircraft reactivated for USAF reconnaissance purposes in 1995. It has since returned to Dryden along with SR-71A 61-7967.

  14. USAF Bioenvironmental Noise Data Handbook. Volume 156. HH-1N In-flight Crew Noise

    NASA Astrophysics Data System (ADS)

    Hille, H. K.

    1982-11-01

    The HH-IN is a USAF multi-purpose utility helicopter providing support for various USAF missions. This report provides measured data defining the bioacoustic environments at flight crew locations inside this helicopter during normal flight operations. Data are reported for two locations in a wide variety of physical and psychoacoustic measures: overall and band sound pressure levels, C-weighted and A-weighted sound levels, preferred speech interference level, perceived noise level, and limiting times for total daily exposure of personnel with and without standard Air Force ear protectors. Refer to Volume 1 of this handbook, USAF Bioenvironmental Noise Data Handbook, Vol. 1: Organization, Content and Application, AMRL-TR-75-50(1) 1975, for discussion of the objective and design of the handbook, the types of data presented, measurement procedures, instrumentation, data processing, definitions of quantities, symbols, equations, applications, limitations, etc.

  15. YF-12C in flight at sunset

    NASA Technical Reports Server (NTRS)

    1974-01-01

    The so-called YF-12C in flight at sunset. The YF-12C was the second production SR-71A (61-7951), modified with YF-12A inlets and engines, and given a bogus tail number (06937). It replaced a YF-12A (60-6936) that crashed during a joint USAF-NASA research program. The Flight Research Center's involvement with the YF-12A, an interceptor version of the Lockheed A-12, began in 1967. Ames Research Center was interested in using wind tunnel data that had been generated at Ames under extreme secrecy. Also, the Office of Advanced Research and Technology (OART) saw the YF-12A as a means to advance high-speed technology, which would help in designing the Supersonic Transport (SST). The Air Force needed technical assistance to get the latest reconnaissance version of the A-12 family, the SR-71A, fully operational. Eventually, the Air Force offered NASA the use of two YF-12A aircraft, 60-6935 and 60-6936. A joint NASA-USAF program was mapped out in June 1969. NASA and Air Force technicians spent three months readying 935 for flight. On 11 December 1969, the flight program got underway with a successful maiden flight piloted by Col. Joe Rogers and Maj. Gary Heidelbaugh of the SR-71/F-12 Test Force. During the program, the Air Force concentrated on military applications, and NASA pursued a loads research program. NASA studies included inflight heating, skin-friction cooling, 'coldwall' research (a heat transfer experiment), flowfield studies, shaker vane research, and tests in support of the Space Shuttle landing program. Ultimately, 935 became the workhorse of the program, with 146 flights between 11 December 1969 and 7 November 1979. The second YF-12A, 936, made 62 flights. It was lost in a non-fatal crash on 24 June 1971. It was replaced by the YF-12C. The YF-12C was delivered to NASA on 16 July 1971. From then until 22 December 1978, it made 90 flights. The Lockheed A-12 family, known as the Blackbirds, were designed by Clarence 'Kelly' Johnson. They were constructed mostly of titanium to withstand aerodynamic heating. Fueled by JP-7, the Blackbirds were capable of cruising at Mach 3.2 and attaining altitudes in excess of 80,000 feet. The first version, a CIA reconnaissance aircraft that first flew in April 1962 was called the A-12. An interceptor version was developed in 1963 under the designation YF-12A. A USAF reconnaissance variant, called the SR-71, was first flown in 1964. The A-12 and SR-71 designs included leading and trailing edges made of high-temperature fiberglass-asbestos laminates. The NASA YF-12 research program was ambitious; the aircraft flew an average of once a week unless down for extended maintenance or modification. Program expenses averaged $3.1 million per year just to run the flight tests. NASA crews for the YF-12 included pilots Fitzhugh Fulton and Donald Mallick, anf flight test engineers Victor Horton and Ray Young. Other NASA test pilots checked out in the YF-12A included John Manke, William Dana, Gary Krier, Einar Enevoldson, Tom McMurtry, Steve Ishmael, and Michael Swann. The YF-12C was flown only by Fulton, Mallick, Horton and Young during its NASA research missions.

  16. Investigation of Pseudo Bi-Polar Nickel Cadmium Batteries as Filter Elements for Pulsed Power Loads.

    DTIC Science & Technology

    1984-12-01

    FOR PULSED POWER LOADS THESIS Michael B. Cimino Gregory M. Gearing Major, USAF Captain, USAF AFIT/GE/ENG/84D-1B DTIC SECETE D~rR~fl"N STATEMENT A...LOADS THESIS Presented to the Faculty of the School of Engineering of the Air Force Institute of Technology Air University In Partial Fulfillment of...with the intent to make batteries capable of out performing capacitors as power supply filters. Purpose This thesis investigated the use of nickel

  17. SR-71 Ship #1 on Ramp

    NASA Technical Reports Server (NTRS)

    1994-01-01

    This photo shows a head-on shot of NASA's SR-71A aircraft on the ramp at NASA's Dryden Flight Research Center, Edwards, California. NASA operated two SR-71s, an SR-71A and an SR- 71B pilot trainer aircraft, both based at Dryden, at that particular point in time. The SR-71 was designed and built by the Lockheed Skunk Works, now the Lockheed Martin Skunk Works. Studies have shown that less than 20 percent of the total thrust used to fly at Mach 3 is produced by the basic engine itself. The balance of the total thrust is produced by the unique design of the engine inlet and 'moveable spike' system at the front of the engine nacelles, and by the ejector nozzles at the exhaust which burn air compressed in the engine bypass system. Data from the SR-71 high speed research program will be used to aid designers of future supersonic/hypersonic aircraft and propulsion systems, including a high speed civil transport. Two SR-71 aircraft have been used by NASA as testbeds for high-speed and high-altitude aeronautical research. The aircraft, an SR-71A and an SR-71B pilot trainer aircraft, have been based here at NASA's Dryden Flight Research Center, Edwards, California. They were transferred to NASA after the U.S. Air Force program was cancelled. As research platforms, the aircraft can cruise at Mach 3 for more than one hour. For thermal experiments, this can produce heat soak temperatures of over 600 degrees Fahrenheit (F). This operating environment makes these aircraft excellent platforms to carry out research and experiments in a variety of areas -- aerodynamics, propulsion, structures, thermal protection materials, high-speed and high-temperature instrumentation, atmospheric studies, and sonic boom characterization. The SR-71 was used in a program to study ways of reducing sonic booms or over pressures that are heard on the ground, much like sharp thunderclaps, when an aircraft exceeds the speed of sound. Data from this Sonic Boom Mitigation Study could eventually lead to aircraft designs that would reduce the 'peak' overpressures of sonic booms and minimize the startling affect they produce on the ground. One of the first major experiments to be flown in the NASA SR-71 program was a laser air data collection system. It used laser light instead of air pressure to produce airspeed and attitude reference data, such as angle of attack and sideslip, which are normally obtained with small tubes and vanes extending into the airstream. One of Dryden's SR-71s was used for the Linear Aerospike Rocket Engine, or LASRE Experiment. Another earlier project consisted of a series of flights using the SR-71 as a science camera platform for NASA's Jet Propulsion Laboratory in Pasadena, California. An upward-looking ultraviolet video camera placed in the SR-71's nosebay studied a variety of celestial objects in wavelengths that are blocked to ground-based astronomers. Earlier in its history, Dryden had a decade of past experience at sustained speeds above Mach 3. Two YF-12A aircraft and an SR-71 designated as a YF-12C were flown at the center between December 1969 and November 1979 in a joint NASA/USAF program to learn more about the capabilities and limitations of high-speed, high-altitude flight. The YF-12As were prototypes of a planned interceptor aircraft based on a design that later evolved into the SR-71 reconnaissance aircraft. Dave Lux was the NASA SR-71 project manger for much of the decade of the 1990s, followed by Steve Schmidt. Developed for the USAF as reconnaissance aircraft more than 30 years ago, SR-71s are still the world's fastest and highest-flying production aircraft. The aircraft can fly at speeds of more than 2,200 miles per hour (Mach 3+, or more than three times the speed of sound) and at altitudes of over 85,000 feet. The Lockheed Skunk Works (now Lockheed Martin) built the original SR-71 aircraft. Each aircraft is 107.4 feet long, has a wingspan of 55.6 feet, and is 18.5 feet high (from the ground to the top of the rudders, when parked). Gross takeoff weight is about 140,000 pounds, including a possible fuel weight of 80,280 pounds. The airframes are built almost entirely of titanium and titanium alloys to withstand heat generated by sustained Mach 3 flight. Aerodynamic control surfaces consist of all-moving vertical tail surfaces, ailerons on the outer wings, and elevators on the trailing edges between the engine exhaust nozzles. The two SR-71s at Dryden have been assigned the following NASA tail numbers: NASA 844 (A model), military serial 61-7980 and NASA 831 (B model), military serial 61-7956. From 1990 through 1994, Dryden also had another 'A' model, NASA 832, military serial 61-7971. This aircraft was returned to the USAF inventory and was the first aircraft reactivated for USAF reconnaissance purposes in 1995. It has since returned to Dryden along with SR-71A 61-7967.

  18. SR-71 - In-flight Close-up from Tanker

    NASA Technical Reports Server (NTRS)

    1994-01-01

    This extreme close-up of the SR-71B operated by NASA's Dryden Flight Research Center, Edwards, California, gives an unusual view of the twin cockpit of Dryden's SR-71B, NASA 831, and its helmeted crew members. The photo was taken from an Air Force tanker refueling the Blackbird during a 1994 flight. The Mach 3 Blackbird aircraft were loaned to NASA by the U.S. Air Force for high-speed, high-altitude aeronautical research. Capable of flying more than 2200 mph and at altitudes of over 85,000 feet, they are excellent platforms for research and experiments in aerodynamics, propulsion, structures, thermal protection materials, atmospheric studies, and sonic boom characterization. Two SR-71 aircraft have been used by NASA as testbeds for high-speed and high-altitude aeronautical research. The aircraft, an SR-71A and an SR-71B pilot trainer aircraft, have been based here at NASA's Dryden Flight Research Center, Edwards, California. They were transferred to NASA after the U.S. Air Force program was cancelled. As research platforms, the aircraft can cruise at Mach 3 for more than one hour. For thermal experiments, this can produce heat soak temperatures of over 600 degrees Fahrenheit (F). This operating environment makes these aircraft excellent platforms to carry out research and experiments in a variety of areas -- aerodynamics, propulsion, structures, thermal protection materials, high-speed and high-temperature instrumentation, atmospheric studies, and sonic boom characterization. The SR-71 was used in a program to study ways of reducing sonic booms or over pressures that are heard on the ground, much like sharp thunderclaps, when an aircraft exceeds the speed of sound. Data from this Sonic Boom Mitigation Study could eventually lead to aircraft designs that would reduce the 'peak' overpressures of sonic booms and minimize the startling affect they produce on the ground. One of the first major experiments to be flown in the NASA SR-71 program was a laser air data collection system. It used laser light instead of air pressure to produce airspeed and attitude reference data, such as angle of attack and sideslip, which are normally obtained with small tubes and vanes extending into the airstream. One of Dryden's SR-71s was used for the Linear Aerospike Rocket Engine, or LASRE Experiment. Another earlier project consisted of a series of flights using the SR-71 as a science camera platform for NASA's Jet Propulsion Laboratory in Pasadena, California. An upward-looking ultraviolet video camera placed in the SR-71's nosebay studied a variety of celestial objects in wavelengths that are blocked to ground-based astronomers. Earlier in its history, Dryden had a decade of past experience at sustained speeds above Mach 3. Two YF-12A aircraft and an SR-71 designated as a YF-12C were flown at the center between December 1969 and November 1979 in a joint NASA/USAF program to learn more about the capabilities and limitations of high-speed, high-altitude flight. The YF-12As were prototypes of a planned interceptor aircraft based on a design that later evolved into the SR-71 reconnaissance aircraft. Dave Lux was the NASA SR-71 project manger for much of the decade of the 1990s, followed by Steve Schmidt. Developed for the USAF as reconnaissance aircraft more than 30 years ago, SR-71s are still the world's fastest and highest-flying production aircraft. The aircraft can fly at speeds of more than 2,200 miles per hour (Mach 3+, or more than three times the speed of sound) and at altitudes of over 85,000 feet. The Lockheed Skunk Works (now Lockheed Martin) built the original SR-71 aircraft. Each aircraft is 107.4 feet long, has a wingspan of 55.6 feet, and is 18.5 feet high (from the ground to the top of the rudders, when parked). Gross takeoff weight is about 140,000 pounds, including a possible fuel weight of 80,280 pounds. The airframes are built almost entirely of titanium and titanium alloys to withstand heat generated by sustained Mach 3 flight. Aerodynamic control surfaces consist of all-moving vertical tail surfaces, ailerons on the outer wings, and elevators on the trailing edges between the engine exhaust nozzles. The two SR-71s at Dryden have been assigned the following NASA tail numbers: NASA 844 (A model), military serial 61-7980 and NASA 831 (B model), military serial 61-7956. From 1990 through 1994, Dryden also had another 'A' model, NASA 832, military serial 61-7971. This aircraft was returned to the USAF inventory and was the first aircraft reactivated for USAF reconnaissance purposes in 1995. It has since returned to Dryden along with SR-71A 61-7967.

  19. A Study to Demonstrate the Application of a Graphical Method to Determine an Optimal Maintenance Task Interval for an Item in Air Force Inventory.

    DTIC Science & Technology

    1982-09-01

    SCHOOL OF SYST.. U14CLASSIFIED D C BECKWITH ET AL. SEP 82 AFIT-LSSR- 60 -82 F/ 5/1 NLI IIIIIIIIIIIIIIlfflfflf IIIIIIIIIIIIIIfllfllf IIIIIIIIIIIIIIl...Beckwith, Captain, USAF Anthony R. Roclevitch, Captain, USAF LSSR 60 -82 j1 -’~ The contents of the document are technically accurate, and no sensitive...Force, or the Department of Defense. II AFIT Control Number LSSR 60 -82 AFIT RESEARCH ASSESSMENT The purpose of this questionnaire is to determine the

  20. Defense Acquisition Research Journal. Volume 22, Number 1, Issue 72.

    DTIC Science & Technology

    2015-01-01

    Capt Allen J. DeNeve, USAF, Lt Col Erin T. Ryan , USAF, Lt Col Jonathan D. Ritschel, USAF, and Christine Schubert Kabban The Effects of System...USAF, Lt Col Erin T. Ryan , USAF, Lt Col Jonathan D. Ritschel, USAF, and Christine Schubert Kabban A regression technique is used to predict cost...practices. Capt Allen J. DeNeve, USAF, Lt Col Erin T. Ryan , USAF, Lt Col Jonathan D. Ritschel, USAF, and Christine Schubert Kabban, in “Taming the

  1. Training for the Air Force fitness assessment: the experience of postpartum women.

    PubMed

    Armitage, Nicole H; Severtsen, Billie M; Vandermause, Roxanne; Smart, Denise A

    2014-07-01

    Active duty personnel in the U.S. Air Force (USAF) are required to pass periodic fitness assessments in order to facilitate and evaluate physical readiness. Pregnant women are exempt from testing but must take the fitness test 6 months after childbirth. However, evidence from prior research indicates that in the first 6 months postpartum, women may not achieve prepregnancy fitness levels and may be more vulnerable to mental and physical health problems. It is important for health care clinicians to understand how training for the USAF fitness test after childbirth may impact health and well-being. The purpose of this study was to develop a deep understanding of the experiences of postpartum USAF women as they train for their fitness assessment. Understanding was sought through a phenomenological study by interpreting the meaning of the lived experiences of 17 active duty women at two USAF bases. Two overarching patterns emerged from this analysis: "Striving to Perform under Pressure through Profound Life Transitions of Childbirth" and "Seeking Understanding from Others." These results provide insight into the challenges postpartum women encounter while training for their fitness assessments, and they can inform practices that facilitate efforts of women in returning to optimal fitness and well-being. Reprint & Copyright © 2014 Association of Military Surgeons of the U.S.

  2. The rate of adverse events during IV conscious sedation.

    PubMed

    Schwamburger, Nathan T; Hancock, Raymond H; Chong, Chol H; Hartup, Grant R; Vandewalle, Kraig S

    2012-01-01

    Conscious sedation has become an integral part of dentistry; it is often used to reduce anxiety or fear in some patients during oral surgery, periodontal surgery, implant placement, and general dentistry procedures. The purpose of this study was to evaluate the frequency of adverse events during IV conscious sedation provided by credentialed general dentists and periodontists in the United States Air Force (USAF). Sedation clinical records (Air Force Form 1417) from calendar year 2009 were requested from all USAF bases. A total of 1,468 records were reviewed and 19 adverse events were noted in 17 patients. IV complication (infiltration) was the most common adverse event. The overall adverse event rate was 1.3 per 100 patients treated. The results of this study show that moderate sedation provided by general dentists and periodontists in the USAF has a low incidence of adverse events, and conscious sedation remains a viable option for providers for the reduction of anxiety in select patients.

  3. An analysis of post-traumatic stress symptoms in United States Air Force drone operators.

    PubMed

    Chappelle, Wayne; Goodman, Tanya; Reardon, Laura; Thompson, William

    2014-06-01

    Remotely piloted aircraft (RPA), commonly referred to as "drones," have emerged over the past decade as an innovative warfighting tool. Given there is a paucity of empirical research assessing drone operators, the purpose of this study was to assess for the prevalence of PTSD symptoms among this cohort. Of the 1084 United States Air Force (USAF) drone operators that participated, a total of 4.3% endorsed a pattern of symptoms of moderate to extreme level of severity meeting criteria outlined in the Diagnostic and Statistical Manual of Mental Disorders-4th edition. The incidence of PTSD among USAF drone operators in this study was lower than rates of PTSD (10-18%) among military personnel returning from deployment but higher than incidence rates (less than 1%) of USAF drone operators reported in electronic medical records. Although low PTSD rates may be promising, limitations to this study are discussed. Copyright © 2014 Elsevier Ltd. All rights reserved.

  4. An appraisal of the quality of surface water in the Sevier Lake basin, Utah, 1964

    USGS Publications Warehouse

    Hahl, D.C.; Mundorff, J.C.

    1968-01-01

    The Sevier and Beaver River systems are the two major river systems in the Sevier Lake basin in Utah. This report contains an analysis of reconnaissance data collected during the 1964 water year regarding the quality of water in these rivers and their tributaries. The purpose of the reconnaissance was to obtain needed water-quality information for the basin. Corollary purposes were to (1) determine the suitability of surface water for specificuses, (2) determine the need and criteria for a water-quality network, and (3) locate sources of organic pollution to the rivers. Data concerning item 3 are mentioned only briefly in this report and will be discussed in a report to be prepared by the Utah Water Pollution and Control Board. Data collected in connection with the reconnaissance and resulting analyses were reported by Hahl and Cabell (1965).

  5. A Tailored Systems Engineering Framework for Science and Technology Projects

    DTIC Science & Technology

    2009-03-01

    PROJECTS THESIS Stephen M. Behm Major, USAF J . Bradford Pitzer Major, USAF Jane F. White Civilian, US AFIT/GSE/ENV/09-M02 DEPARTMENT OF THE...Engineering Stephen M. Behm, Major, USAF J . Bradford Pitzer, Major, USAF Jane F. White, Civilian, US March 2009 APPROVED FOR PUBLIC...Stephen M. Behm, Major, USAF J . Bradford Pitzer, Major, USAF Jane F. White, Civilian, US Approved: iv AFIT/GSE/ENV

  6. Air and Space Power Journal. Volume 17, Number 4, Winter 2003

    DTIC Science & Technology

    2003-01-01

    Van Nederveen, USAF, Retired Gradual Failure: The Air War over North Vietnam, 1965–1966 . . . . . . . . . . . . . . . . . . . . . . . . . . . 99...Jacob Van Staaveren Reviewer: Maj Paul G. Niesen, USAF Flankers: The New Generation...Operations Directorate Headquarters USAF Brig Gen Phillip D. Caine, USAF, Retired Monument, Colorado Dr. Don D. Chipman USAF Squadron Officer College

  7. YF-12 in flight

    NASA Technical Reports Server (NTRS)

    1972-01-01

    The Flight Research Center's involvement with the YF-12A, an interceptor version of the Lockheed A-12, began in 1967. Ames Research Center was interested in using wind tunnel data that had been generated at Ames under extreme secrecy. Also, the Office of Advanced Research and Technology (OART) saw the YF-12A as a means to advance high-speed technology, which would help in designing the Supersonic Transport (SST). The Air Force needed technical assistance to get the latest reconnaissance version of the A-12 family, the SR-71A, fully operational. Eventually, the Air Force offered NASA the use of two YF-12A aircraft, 60-6935 and 60-6936. A joint NASA-USAF program was mapped out in June 1969. NASA and Air Force technicians spent three months readying 935 for flight. On 11 December 1969, the flight program got underway with a successful maiden flight piloted by Col. Joe Rogers and Maj. Gary Heidelbaugh of the SR-71/F-12 Test Force. During the program, the Air Force concentrated on military applications, and NASA pursued a loads research program. NASA studies included inflight heating, skin-friction cooling, 'coldwall' research (a heat transfer experiment), flowfield studies, shaker vane research, and tests in support of the Space Shuttle landing program. Ultimately, 935 became the workhorse of the program, with 146 flights between 11 December 1969 and 7 November 1979. The second YF-12A, 936, made 62 flights. It was lost in a non-fatal crash on 24 June 1971. It was replaced by the so-called YF-12C (SR-71A 61-7951, modified with YF-12A inlets and engines and a bogus tail number 06937). The Lockheed A-12 family, known as the Blackbirds, were designed by Clarence 'Kelly' Johnson. They were constructed mostly of titanium to withstand aerodynamic heating. Fueled by JP-7, the Blackbirds were capable of cruising at Mach 3.2 and attaining altitudes in excess of 80,000 feet. The first version, a CIA reconnaissance aircraft that first flew in April 1962 was called the A-12. An interceptor version was developed in 1963 under the designation YF-12A. A USAF reconnaissance variant, called the SR-71, was first flown in 1964. The A-12 and SR-71 designs included leading and trailing edges made of high-temperature fiberglass-asbestos laminates. The NASA YF-12 research program was ambitious; the aircraft flew an average of once a week unless down for extended maintenance or modification. Program expenses averaged $3.1 million per year just to run the flight tests. NASA crews for the YF-12 included pilots Fitzhugh Fulton and Donald Mallick, anf flight test engineers Victor Horton and Ray Young. Other NASA test pilots checked out in the YF-12A included John Manke, William Dana, Gary Krier, Einar Enevoldson, Tom McMurtry, Steve Ishmael, and Michael Swann. Except for its delivery and departure, the YF-12C was only flown by Fulton, Mallick, Horton, and Ray. It made 90 flights between 16 July 1971 and 22 December 1978.

  8. European Fiber Optics. USAF Laboratory Experts’ Visit,

    DTIC Science & Technology

    1979-12-01

    emitting at 480 ma. AE-Telefunken Telecomunications and Cable Systems Division Postfach 1120 7150 Backnang, Germany Principal Contact: Dr. K. D. 4chenkel...alignment purposes. Standard Telecomunication Laboratories, Inc. (STL) London Road Harlow, Essex 017 9NA, England Principal Contact: Dr. M. Chown - Manager

  9. Mechanisms of slow-pitch softball injuries reported to the HQ Air Force Safety Center a 10-year descriptive study, 1993-2002.

    PubMed

    Burnham, Bruce R; Copley, G Bruce; Shim, Matthew J; Kemp, Philip A; Jones, Bruce H

    2010-01-01

    Softball is a popular sport in civilian and military populations and results in a large number of lost-workday injuries. The purpose of this study is to describe the mechanisms associated with softball injuries occurring among active duty U.S. Air Force (USAF) personnel to better identify potentially effective countermeasures. Data derived from safety reports were obtained from the USAF Ground Safety Automated System in 2003. Softball injuries for the years 1993-2002 that resulted in at least one lost workday were included in the study. Narrative data were systematically reviewed and coded in order to categorize and summarize mechanisms associated with these injuries. This report documents a total of 1181 softball-related mishap reports, involving 1171 active duty USAF members who sustained one lost-workday injury while playing softball. Eight independent mechanisms were identified. Three specific scenarios (sliding, being hit by a ball, and colliding with a player) accounted for 60% of reported softball injuries. Mechanisms of injury for activities such as playing softball, necessary for prevention planning, can be identified using the detailed information found in safety reports. This information should also be used to develop better sports injury coding systems. Within the USAF and U.S. softball community, interventions to reduce injuries related to the most common mechanisms (sliding, being hit by a ball, and colliding with a player) should be developed, implemented, and evaluated. Published by Elsevier Inc.

  10. Acquisition Review Quarterly (ARQ): Volume 10, Number 3, Summer 2003

    DTIC Science & Technology

    2003-01-01

    PROJECT NUMBER Lt Col Robert L. Waller, USAF, (Ret), Robert Graham, Maj David R. King, USAF, Lt Col John D. Driessnack, USAF, LTC Michael D. Proctor...High-Technology Industries Implications for Industrial Policy Maj David R. King, USAF Lt Col John D. Driessnack, USAF Why the "T" in SMART A...Business School William H . Reed Director Michael Wynne Defense Contract Audit Agency Acting Under Secretary of Defense (Acquisition, Technology, and

  11. 32 CFR Appendix B to Part 68 - Addendum for Education Services Between [Name of Educational Institution] and the U.S. Air Force

    Code of Federal Regulations, 2013 CFR

    2013-07-01

    ... Educational Institution] and the U.S. Air Force B Appendix B to Part 68 National Defense Department of Defense...] and the U.S. Air Force 1. Purpose. This addendum is between (Name of Educational Institution), hereafter referred to as the “Institution,” and the United States Air Force (USAF). The purpose of this...

  12. 1977 Annual Typhoon Report

    DTIC Science & Technology

    1995-01-01

    George T. McKaige, USN *CAPT Frederick P. Milwer, USAF CAPT Alan W. Hassebrock, USAF CAPT Charles P. Guard , USAF CAPT”John D. Shewchuk, USAF ENS Edward...Det 1, lWW - USAF 1977 ANNUAL TYPHOON REPORT *Departed during 1977 season FRONTCOVER: ln&a.tedphoztogzaphof a - tmJ -A.toZmb.iaZatAn o.ulh a M dtig -&A...ships provide day and night coverage in the JTWC area of responsibility. Interpretation of this satellite imagery pro- vides cyclone positions, and for

  13. 32 CFR 855.14 - Unauthorized landings.

    Code of Federal Regulations, 2010 CFR

    2010-07-01

    ...) as specified in section 6 of the FAA Airman's Information Manual. (2) Notifies the Federal Aviation... registry, followed by written notification with an information copy to HQ USAF/XOOBC and the civil aviation...) Landed for a purpose not approved on the DD Form 2401. (iii) Operated an aircraft not of a model or...

  14. 1991 Annual Tropical Cyclone Report

    DTIC Science & Technology

    1995-01-01

    CAPT * CAPT lLT * MSGT MSGT...TSGT * TSGT TSGT TSGT TSGT * SSGT * SSGT SSGT * SSGT SSGT SSGT CAPT MR SGT SGT * SOT DR NICHOLASD.GURAL USN LESTERE.CARRrIII USN ROBEmL.BEARD USN...ANNR.GOETZ USAF BRUCEW.THOMPSON USAF ELIZABETHB.BORELLI USAF STEPHENC.HALLJN USAF DAVIDJ.STREMLER USN STACYR.STEWART USNR RICHARDA.JEFFRIES USN THOMAS

  15. Hydrologic reconnaissance of the southern Uinta basin, Utah and Colorado

    USGS Publications Warehouse

    Price, Don; Miller, Louise L.

    1975-01-01

    This report summarizes the findings of an investigation of the water resources of the southern Uinta Basin conducted by the U.S. Geological Survey in cooperation with the Utah Department of Natural Resources, Division of Water Rights. The purpose of the investigation was to evaluate the water resources of the southern Uinta Basin on a reconnaissance level and to provide information to assist in future planning and development of the water and related land resources.

  16. Bioenvironmental Engineering Career Ladder AFSC 907X0

    DTIC Science & Technology

    1991-05-01

    TTA 1 1 HQ USAF/DPPE 1 HQ USAF/SGPA ( BOLLING AFB DC 20332-6188) 1 1 HQ USAFE/DPAT 3 3 HQ USAFE/TTA 1 1 HSD/SOSP 1 1 NODAC 1 USAFOMS/OMDQ 1 USAFOMS...this report are available for use by operations and training officials. Mr Roberto Salinas developed the survey instrument, Ms Becky Hernandez provided

  17. YF-12C on ramp

    NASA Technical Reports Server (NTRS)

    1973-01-01

    The so-called YF-12C on the NASA Flight Research Center ramp. Following the loss of a YF-12A in a non-fatal accident in June 1971, NASA acquired the second production SR-71A (61-7951) from the Air Force. Because the SR-71 program was shrouded in the highest secrecy, the Air Force restricted NASA to using the aircraft solely for propulsion testing with YF-12A inlets and engines. It was designated the YF-12C, and given a bogus tail number (06937). The two YF-12As in the program had actual tail numbers 06935 and 06936. The first NASA flight of the YF-12C took place on 24 May 1972. The Flight Research Center's involvement with the YF-12A, an interceptor version of the Lockheed A-12, began in 1967. Ames Research Center was interested in using wind tunnel data that had been generated at Ames under extreme secrecy. Also, the Office of Advanced Research and Technology (OART) saw the YF-12A as a means to advance high-speed technology, which would help in designing the Supersonic Transport (SST). The Air Force needed technical assistance to get the latest reconnaissance version of the A-12 family, the SR-71A, fully operational. Eventually, the Air Force offered NASA the use of two YF-12A aircraft, 60-6935 and 606936. A joint NASA-USAF program was mapped out in June 1969. NASA and Air Force technicians spent three months readying 935 for flight. On 11 December 1969, the flight program got underway with a successful maiden flight piloted by Col. Joe Rogers and Maj. Gary Heidelbaugh of the SR-71/F-12 Test Force. During the program, the Air Force concentrated on military applications, and NASA pursued a loads research program. NASA studies included inflight heating, skin-friction cooling, 'coldwall' research (a heat transfer experiment), flowfield studies, shaker vane research, and tests in support of the Space Shuttle landing program. Ultimately, 935 became the workhorse of the program, with 146 flights between 11 December 1969 and 7 November 1979. The second YF-12A, 936, made 62 flights. It was lost in a non-fatal crash on 24 June 1971. It was replaced by the YF-12C. The Lockheed A-12 family, known as the Blackbirds, were designed by Clarence 'Kelly' Johnson. They were constructed mostly of titanium to withstand aerodynamic heating. Fueled by JP-7, the Blackbirds were capable of cruising at Mach 3.2 and attaining altitudes in excess of 80,000 feet. The first version, a CIA reconnaissance aircraft that first flew in April 1962 was called the A-12. An interceptor version was developed in 1963 under the designation YF-12A. A USAF reconnaissance variant, called the SR-71, was first flown in 1964. The A-12 and SR-71 designs included leading and trailing edges made of high-temperature fiberglass-asbestos laminates. The NASA YF-12 research program was ambitious; the aircraft flew an average of once a week unless down for extended maintenance or modification. Program expenses averaged $3.1 million per year just to run the flight tests. NASA crews for the YF-12 included pilots Fitzhugh Fulton and Donald Mallick, anf flight test engineers Victor Horton and Ray Young. Other NASA test pilots checked out in the YF-12A included John Manke, William Dana, Gary Krier, Einar Enevoldson, Tom McMurtry, Steve Ishmael, and Michael Swann. Only Fulton, Mallick, Ray, and Horton flew the YF-12C.

  18. Usaf Space Sensing Cryogenic Considerations

    NASA Astrophysics Data System (ADS)

    Roush, F.

    2010-04-01

    Infrared (IR) space sensing missions of the future depend upon low mass components and highly capable imaging technologies. Limitations in visible imaging due to the earth's shadow drive the use of IR surveillance methods for a wide variety of applications for Intelligence, Surveillance, and Reconnaissance (ISR), Ballistic Missile Defense (BMD) applications, and almost certainly in Space Situational Awareness (SSA) and Operationally Responsive Space (ORS) missions. Utilization of IR sensors greatly expands and improves mission capabilities including target and target behavioral discrimination. Background IR emissions and electronic noise that is inherently present in Focal Plane Arrays (FPAs) and surveillance optics bench designs prevents their use unless they are cooled to cryogenic temperatures. This paper describes the role of cryogenic coolers as an enabling technology for generic ISR and BMD missions and provides ISR and BMD mission and requirement planners with a brief glimpse of this critical technology implementation potential. The interaction between cryogenic refrigeration component performance and the IR sensor optics and FPA can be seen as not only mission enabling but also as mission performance enhancing when the refrigeration system is considered as part of an overall optimization problem.

  19. Mechanisms of flag-football injuries reported to the HQ Air Force Safety Center a 10-year descriptive study, 1993-2002.

    PubMed

    Burnham, Bruce R; Copley, G Bruce; Shim, Matthew J; Kemp, Philip A; Jones, Bruce H

    2010-01-01

    Flag (touch or intramural) football is a popular sport among the U.S. Air Force (USAF) active duty population and causes a substantial number of lost-workday injuries. The purpose of this study is to describe the mechanisms of flag-football injuries to better identify effective countermeasures. The data were derived from safety reports obtained from the USAF Ground Safety Automated System. Flag-football injuries for the years 1993-2002 that resulted in at least one lost workday were included in the study conducted in 2003. Narrative data were systematically reviewed for 32,812 USAF mishap reports; these were then coded in order to categorize and summarize mechanisms associated with flag football and other sports and occupational injuries. Nine hundred and forty-four mishap reports involving active duty USAF members playing flag football met the criteria for inclusion into this study. Eight mechanisms of injury were identified. The eight mechanisms accounted for 90% of all flag-football injuries. One scenario (contact with another player) accounted for 42% of all flag-football injuries. The most common mechanisms of injury caused by playing flag football can be identified using the detailed information found in safety reports. These scenarios are essential to developing evidence-based countermeasures. Results for flag football suggest that interventions that prevent player contact injuries deserve further research and evaluation. The broader implications of this study are that military safety data can be used to identify potentially modifiable mechanisms of injury for specific activities such as flag football. Published by Elsevier Inc.

  20. Geologic Reconnaissance and Lithologic Identification by Remote Sensing

    DTIC Science & Technology

    remote sensing in geologic reconnaissance for purposes of tunnel site selection was studied further and a test case was undertaken to evaluate this geological application. Airborne multispectral scanning (MSS) data were obtained in May, 1972, over a region between Spearfish and Rapid City, South Dakota. With major effort directed toward the analysis of these data, the following geologic features were discriminated: (1) exposed rock areas, (2) five separate rock groups, (3) large-scale structures. This discrimination was accomplished by ratioing multispectral channels.

  1. Dental Diamond Rotary Instruments. Test and Evaluation

    DTIC Science & Technology

    1983-09-01

    Gov’t. agencies only; Critical Technology; Test and Evaluation; 19 NOV 1982. Other requests shall be referred to Dental Investigation Service, School of... DENTAL DIAMOND ROTARY INSTRUMENTS Test and Evaluation Cad D. Foster, Major, USAF, DC Joseph M. Powell, Colonel, USAF, DC John M. Young, Colonel, USAF...19 November 1982. Other requests for this document must be referred to the Dental Investig tion Service, USAF School of Aerospace Medicine. SUBJECT TO

  2. Technology Support for Combat Casualty Related Medical Infrared Imaging

    DTIC Science & Technology

    2011-08-10

    LtCol. David Trant USAF as On-site PI, and the Duke Medical IR group (Drs. Pearlstein and Guenther) serving as Co-PI’s, was approved in January 2009...patient outcome. COLLABORATORS: LtCol. Kenneth Egerstrom, USAF; LtCol. David Trant, USAF; Dr. Larry Katz, Department of Emergency Medicine...University of North Carolina Hospitals; Col. Byron Funke, USAF; Dr. David Randall, USArmy Night Vision Laboratories (Ft. Belvoir); Mr. Wayne Antesberger

  3. Simplified Key Management for Digital Access Control of Information Objects

    DTIC Science & Technology

    2016-07-02

    0001, Task BC-5-2283, “Architecture, Design of Services for Air Force Wide Distributed Systems,” for USAF HQ USAF SAF/CIO A6. The views, opinions...Challenges for Cloud Computing,” Lecture Notes in Engineering and Computer Science: Proceedings World Congress on Engineering and Computer Science 2011...P. Konieczny USAF HQ USAF SAF/CIO A6 11. SPONSOR’S / MONITOR’S REPORT NUMBER(S) 12. DISTRIBUTION / AVAILABILITY STATEMENT Approved for public

  4. Information Assurance within the United States Air Force

    ERIC Educational Resources Information Center

    Cherry, John D.

    2010-01-01

    According to the Department of Defense (DoD), a review of information assurance (IA) in the United States Air Force (USAF) in 2009, cyber security is jeopardized because of information loss. This situation has occurred in large part because of less than optimal training practices or adherence to training protocols. The purpose of this study was…

  5. AF Ni-Cd cell qualification program

    NASA Technical Reports Server (NTRS)

    Hall, Steve; Brown, Harry; Collins, G.; Hwang, Warren

    1994-01-01

    The present status of the USAF NiCd cell qualification program, which is underway at the Naval Surface Warfare Center-Crane Division, is summarized. The following topics are discussed: overview; background; purpose; stress tests; results for super Ni-Cd; results for SAFT cells; GPS stress test; GPS simulated orbit; and results for gates cells. The discussion is presented in viewgraph format.

  6. Survey of Wastewater Discharge, Eielson AFB, Alaska, EHL(K) 73-24

    DTIC Science & Technology

    1973-12-01

    the Department of Defense. ii TABLE OF CONTENTS Section Page I. SUMMARY .................................................. 1 II. INTRODUCTION ...II. INTRODUCTION A. Purpose And Objectives The USAF Environmental Health Laboratories were requested to provide assistance in improving existing water...equivalent to best practicable control technology currently available as shall be defined for each industrial waste. 3. Proposed Performance Specifications

  7. Gravitational Lens: Deep Space Probe Design

    DTIC Science & Technology

    2012-03-01

    Lieutenant, USAF Approved: Timothy Lawrence, Col, USAF (Chairman) Date Carl Hartsfield, Lt Col, USAF (Member) Date Marc G. Millis (Member) Date Abstract A...23 RTG Radioisotope Thermoelectric Generators . . . . . . . . . . . . . . . . . 26 EOL End of Life...26 ASRG Advanced Stirling Radioisotope Generator . . . . . . . . . . . . . . . . 26 GPHS

  8. Asymptomatic Wolff-Parkinson-White Pattern ECG in USAF Aviators.

    PubMed

    Davenport, Eddie D; Rupp, Karen A N; Palileo, Edwin; Haynes, Jared

    2017-01-01

    Wolff-Parkinson-White (WPW) pattern is occasionally found in asymptomatic aviators during routine ECGs. Aeromedical concerns regarding WPW pattern include risk of dysrhythmia or sudden cardiac death (SCD), thus affecting the safety of flight. The purpose of this study was to determine the prevalence and outcomes of aviators with asymptomatic WPW pattern and assess for risk factors that contribute to progression to dysrhythmia or symptoms. The U.S. Air Force (USAF) ECG library database containing over 1.2 million ECGs collected over the past 68 yr was used to identify 638 individual aviators with WPW pattern. Demographic, medical history, and outcome data were obtained by medical record review. Aviators who developed high risk features defined as symptoms, arrhythmia, or ablation of a high risk pathway, were compared to those who remained asymptomatic. Prevalence of WPW pattern was 0.30% among all USAF aviators. Of the 638 individuals, 64 (10%) progressed to the combined endpoint of SCD, arrhythmia, and/or ablation of a high risk pathway over 6868 patient years, with average follow-up of 10.5 yr. There were two sudden cardiac deaths (0.3%). Annual risk of possible sudden incapacitation was 0.95% and of SCD 0.03%. Those that progressed to high risk were significantly younger, had lower diastolic blood pressure, lower total cholesterol, and better physical fitness testing scores. WPW pattern on ECG found in asymptomatic aviators confers < 1% annual risk of arrhythmia or incapacitating events with the highest risk in the younger, healthier, and most fit populations.Davenport ED, Rupp KAN, Palileo E, Haynes J. Asymptomatic Wolff-Parkinson-White pattern ECG in USAF aviators. Aerosp Med Hum Perform. 2017; 88(1):56-60.

  9. United States Air Force Statistical Digest, Fiscal Year 1956. Eleventh Edition

    DTIC Science & Technology

    1956-09-30

    340 •••••••••••••••••• USAF Dental Health Activitiea at USAF In.tallations, Worldwide - FY 1956 ••• USAF Veterinary Animal Origin Food ...Inspection Service Incident to Pro- curement - FY 1956 ••••••••••••••••••••••••• Summary - USAF Veterinary Non-Animal Origin Food Inspection Service Incident...to Procurement - FY 1956 •••••.•••••••• USAF Veterinary Animal Origin Food Inspection Service Incident to Surveillance - FY 1956

  10. Design Evolution of a Fighter Training Scheduling Decision Support System.

    DTIC Science & Technology

    1987-03-01

    SYSTEM THESIS Paul E. Trapp Jeffrey W. Grechanik Captain, USAF Captain, USAF AFIT/GST/ENS/87M-8 MAY 191987 " Approved for public release; distribution...E. Trapp, B.S., M.A. Jeffrey W. Grechanik, B.S. Captain, USAF Captain, USAF March 87 Approved for public release; distribution unlimited This work...DNIF, TDY, and other disruptions. Therefore, cycli- cal scheduling will not be used (3:1-18). ProgAMming. Arthur and Ravindran proposed a goal

  11. T-38C Optimal Landing Technique Determination (Project Talon Spot)

    DTIC Science & Technology

    2010-05-01

    USAF TPS, Class 09B. All objectives of the test were met. 15. SUBJECT TERMS T-38 Aircraft , T-38C Aircraft , J85-GE-5 engine, landing performance... aircraft crossed the threshold. The requesting agency was Headquarters AETC/A3FV, through the USAF TPS. The responsible test organization was the 412...13197 (Figure 1) instrumented test aircraft were flown. The USAF TPS personnel performed all testing at USAF Plant 42 in Palmdale, CA and Edwards

  12. A Parametric Regression of the Cost of Base Realignment Action (COBRA) Model

    DTIC Science & Technology

    1993-09-20

    Douglas D. Hardman , Captain, USAF Michael S. Nelson, Captain, USAF AFIT/GEE/ENS/93S-03 93 P’ 8 143 Approved for public release, distribution unlimited 93... Hardman CLASS: GEE 93S Captain Michael Nelson TITLE: A Parametric Regression of the Cost of Base Realignment Action (COBRA) Model DEFENSE DATE: 20...Science in Engineering and Environmental Management Douglas D. Hardman , B.S.E.E. Michael S. Nelson, B.S.C.E Captain, USAF Captain, USAF September 1993

  13. 50 CFR 84.47 - What are allowable costs?

    Code of Federal Regulations, 2013 CFR

    2013-10-01

    ... feasibility surveys, engineering design, biological reconnaissance, appraisals, or preparation of grant... designed to include purposes other than those eligible under the Act, the costs must be prorated among the...

  14. 50 CFR 84.47 - What are allowable costs?

    Code of Federal Regulations, 2010 CFR

    2010-10-01

    ... feasibility surveys, engineering design, biological reconnaissance, appraisals, or preparation of grant... designed to include purposes other than those eligible under the Act, the costs must be prorated among the...

  15. 50 CFR 84.47 - What are allowable costs?

    Code of Federal Regulations, 2012 CFR

    2012-10-01

    ... feasibility surveys, engineering design, biological reconnaissance, appraisals, or preparation of grant... designed to include purposes other than those eligible under the Act, the costs must be prorated among the...

  16. 50 CFR 84.47 - What are allowable costs?

    Code of Federal Regulations, 2011 CFR

    2011-10-01

    ... feasibility surveys, engineering design, biological reconnaissance, appraisals, or preparation of grant... designed to include purposes other than those eligible under the Act, the costs must be prorated among the...

  17. 50 CFR 84.47 - What are allowable costs?

    Code of Federal Regulations, 2014 CFR

    2014-10-01

    ... feasibility surveys, engineering design, biological reconnaissance, appraisals, or preparation of grant... designed to include purposes other than those eligible under the Act, the costs must be prorated among the...

  18. Basic Microsurgery Training Using the Laboratory Rat (Rattus norvegicus)

    DTIC Science & Technology

    2018-03-01

    all information . Use additional pages if necessary.) PROTOCOL #: FDG20170016A DATE: 1 March 2018 PROTOCOL TITLE: “Basic Microsurgery Training...2018__ RYAN M. DIEPENBROCK, Lt Col, USAF, DC (Date) 3 FDG20170016A Attachments: Attachment 1: Defense Technical Information Center (DTIC) Abstract...Submission Attachment 1 Defense Technical Information Center (DTIC) Abstract Submission Objectives: The purpose of this course is to

  19. Beyond the Horizon: Developing Future Airpower Strategy

    DTIC Science & Technology

    2014-01-01

    is or becomes more capable, then it is further evidence the USAF failed to proactively usher in these emerging and vital airpower capabilities...USAF airpower. 9. USAF chief of staff, Gen Norton Schwartz, 2009, offered in numerous speeches. 10. Carl H. Builder, The Icarus Syndrome : The Role of

  20. A Condition Based Maintenance Approach to Forecasting B-1 Aircraft Parts

    DTIC Science & Technology

    2017-03-23

    1 Problem Statement...aimed at making the USAF aware of CBM methods, and recommending which techniques to consider for implementation. Problem Statement The USAF relies on... problem , this research will seek to highlight common CBM forecasting methods that are well established and evaluate its suitability with current USAF

  1. 76 FR 59116 - Procurement List; Additions

    Federal Register 2010, 2011, 2012, 2013, 2014

    2011-09-23

    ... NSN: AF110--Shirt, Class A/Primary Duty, USAF, Men's, Long Sleeve, Dark Navy Blue, Numerous Sizes. NSN: AF111--Shirt, Class A/Primary Duty, USAF, Women's, Long Sleeve, Dark Navy Blue, Numerous Sizes. NSN: AF120--Shirt, Class A/Primary Duty, USAF, Men's, Short Sleeve, Dark Navy Blue, Numerous Sizes. NSN...

  2. Gulf Cooperation Council: Arabian Gulf Cooperation Continues Defense Forces (Peninsula Shield Force)

    DTIC Science & Technology

    2015-05-23

    Lieutenant Colonel Rhett Champagne , USAF, “The Case for a Gulf Cooperation Council Peninsula Shield Force,” The FAOA Journal of International Affairs...Anthony J. Mastalir USAF, Lieutenant Colonel Jim Keating USA, and Lieutenant Colonel Rhett Champagne , USAF. “The Case for a Gulf Cooperation Council

  3. Low Yield Nuclear Experiments: Should They Be Permitted Within a Comprehensive Test Ban Treaty?

    DTIC Science & Technology

    1996-10-01

    GRAVITY BOMB 83 AF A W87 ICBM REENTRY VEHICLE 86 AF A W88 SLBM REENTRY VEHICLE 89 NAVY C SAFETY FEATURES: A--(ENDS, IHE, FRP) B--(ENDS, IHE) C--(ENDS) o...NUCLEAR WEAPON DELIVERY PLATFORMS (NUCLEAR POSTURE REVIEW) STRATEGIC DELIVERY VEHICLES 20 B-2 BOMBERS USAF 66 B-52 BOMBERS USAF 500/450 MINUTEMAN III...ICBMs USAF 14 TRIBENT SUBMARINES USN W/ 24 D-5 MISSILES EACH TACTICAL DELIVERY VEHICLES DUAL CAPABLE AIRCRAFT USAF/USN SEA-LAUNCH CRUISE MISSILES USN

  4. USAF/SCEEE Graduate Student Summer Research Program (1984). Program Management Report. Volume 1.

    DTIC Science & Technology

    1984-10-01

    AFRL -TN-87, Air Force . Weapons Laboratory , Kirtland Air Foce...Mexico Research Location: Air Force Weapons Laboratory , NTATT, Kirtland Air Force Base, Albuquerque, NM 87117 .. USAF Research Contact: Dr. Carl E. Baum...Albuquerque, NM 87131 ... Research Location: Air Force Weapons Laboratory Kirtland Air Force Base Albuquerque, New Mexico 87117 USAF

  5. Unintended Consequences: Potential Downsides of the Air Force’s Conversion to Biofuels

    DTIC Science & Technology

    2011-01-01

    Mark N. Goltz , PhD, USAF, Retired Dr. Charles A. Bleckmann Dr. Douglas M. Mackay Maj Khai Vuong, USAF Capt Jerrod P. McComb, USAF* *Lieutenant...Colonel Goltz and Dr. Bleckmann are faculty members in the environmental engineering and science program at the Air Force Institute of Technology (AFIT

  6. Hydrologic reconnaissance of western Arctic Alaska, 1976 and 1977

    USGS Publications Warehouse

    Childers, Joseph M.; Kernodle, Donald R.; Loeffler, Robert M.

    1979-01-01

    Reconnaissance water-resource investigations were conducted on the western Alaskan Arctic Slope during April 1976 and August 1977; these months are times of winter and summer low flow. The information gathered is important for coordinated development in the area. Such development has been spurred by oil and gas discoveries on the North Slope, most notably at Prudhoe Bay. Little water resources information is currently available. The study area extended from the Colville River to the vicinity of Kotzebue. It included the western Arctic Slope and the western foothills of the Brooks Range. Nine springs, nine lakes and eleven rivers were sampled during the April 1976 reconnaissance trip. Its purpose was to locate winter flow and describe its quantity and quality. Field water-quality measurements made at these sites were: ice thickness, water depth, discharge (spring and streams), specific conductance, water temperature, dissolved oxygen, alkalinity (bicarbonate, HOC3), and pH. A followup summer trip was made in August 1977 to determine flood characteristics of twenty selected streams. Bankfull and maximum evident flood-peak discharges were determined by measuring channel geometry and estimating channel roughness. Aquatic invertebrate samples were collected at springs and flood survey sites visited during both reconnaissance trips. (Woodard-USGS)

  7. Design and Implementation of USAF Avionics Integration Support Facilities

    DTIC Science & Technology

    1981-12-01

    specification for taking the bbranch Vt -Routing indicator (No activity): Allocate Node: All’ocation of resources: R= Allocation rule. Res Resource type number...problems, and the integration and testing of the ECS. The purpose of this investigation is to establish a standard software development system...Corrections to equipment problems. -Compensation for equipment degradation. -New Developments . This approach is intended to centralize essential

  8. An Enhanced Fuselage Ultrasound Inspection Approach for ISHM Purposes

    DTIC Science & Technology

    2012-03-01

    daily reflections, this would not have been possible. Many thanks to the glorious Colombian Air Force “Asi se va a las Alturas” Francisco Ospina...ASIP Policies After the Aloha Accident, the public concerns increased and the United States Congress passed legislation known as the Aviation...Sensors: on- ground Optimization plus False Alarm Probability?, Useful Life?, Environmental Factors?, others Crack Found? FAA/USAF Approval of FMP

  9. USAF/SCEEE Graduate Student Summer Research Program (1984). Program Management Report.

    DTIC Science & Technology

    1984-10-01

    adjunct effort to the SFRP. Its purpose is to provide funds for selected graduate students to do research at an appropriate Air Force laboratory or...under the Summer Faculty Research Program or an Air Force laboratory designated *- colleague. The students were U.S. citizens, working toward . an...faculty member; excellent laboratory experience. Good opportunity to become acquainted with Air Force research . Good concept. Good stipend

  10. Filling the Fighter Gap

    DTIC Science & Technology

    2010-03-18

    1 Filling the Fighter Gap by Major Justin DeMarco, USAF The purpose of this paper is to suggest how the Air Force can mitigate the...estimate or any other aspect of this collection of information, including suggestions for reducing this burden, to Washington Headquarters Services...SUBTITLE Filling the Fighter Gap 5a. CONTRACT NUMBER 5b. GRANT NUMBER 5c. PROGRAM ELEMENT NUMBER 6. AUTHOR(S) 5d. PROJECT NUMBER 5e. TASK NUMBER

  11. USAF/SCEEE Graduate Student Summer Support Program (1982). Management and Technical Report.

    DTIC Science & Technology

    1982-10-01

    AD-A130 767 USAF/SCEEE GRADUATE STUDENT SUMMER SUPPORT PROGRAM (1982) MANAGEMENT AND..(U) SOUTHEASTERN CENTER FORELECTRICAL ENGINEERING EDUCATION INC...SUMMER SUPPORT PROGRAM Conducted by Southeastern Center for Electrical Engineering Education under USAF Contract Number F49620-82-C-0035 MANAGEMENT ...UNITED STATES AIR FORCE GRADUATE STUDENT SL24MER SUPPORT PROGRAM 1982 PROGRAM MANAGEMENT AND TECHNICAL REPORT SOUTHEASTERN CENTER FOR ELECTRICAL

  12. The Relationship between Physical Activity and Productivity

    DTIC Science & Technology

    1984-04-01

    suggestions as our advisor. Captain Jeffrey S. Austin, USAF, of the Leadership and Management Development Center (LMDC) served unofficially yet willingly as...youthful and healthy population. It is recommended that the USAF: (1) develop fitness standards based on wartime requirements for skills requiring high...encouraged its military personnel to develop and maintain physical fitness. In the USAF’s view, regular physical conditioning and a balanced diet

  13. Incidence of Testicular Cancer in U.S. Air Force Officer Aviators: 1998-2008

    DTIC Science & Technology

    2011-06-01

    DAVID B. RHODES, Col, USAF, MC ROBERT E. CARROLL , Col, USAF, MC, CFS This... S ) Christopher Walker 5d. PROJECT NUMBER 5e. TASK NUMBER 5f. WORK UNIT NUMBER 7. PERFORMING ORGANIZATION NAME( S ) AND ADDRESS(ES) USAF...REPORT NUMBER AFRL-SA-WP-SR-2012-0001 9. SPONSORING / MONITORING AGENCY NAME( S ) AND ADDRESS(ES) 10. SPONSORING/MONITOR’S ACRONYM( S

  14. Reconnaissance of the water resources of the Lonesome Valley area, Yavapai County, Arizona

    USGS Publications Warehouse

    Metzger, Donald G.

    1957-01-01

    In accordance with a request from its cooperating agency, the Arizona State Land Department, the U.S. Geological Survey has made a brief reconnaissance of the water resources of the Lonesome Valley area, Yavapai County, Ariz., to determine the probable hydrologic effects of a proposed dam on Lynx Creek. The construction of this dam has been proposed by the Arizona Game and Fish Department, for recreational and fish-cultural purposes. Data on the geology of the area were furnished by Mrs. Medora M. Krieger, geologist, Geologic Division, U.S. Geological Survey, and the map was prepared by Floyd R. Twenter, geologist, Ground Water Branch.

  15. Joint NASA/USAF Airborne Field Mill Program - Operation and safety considerations during flights of a Lear 28 airplane in adverse weather

    NASA Technical Reports Server (NTRS)

    Fisher, Bruce D.; Phillips, Michael R.; Maier, Launa M.

    1992-01-01

    A NASA Langley Research Center Learjet 28 research airplane was flown in various adverse weather conditions in the vicinity of the NASA Kennedy Space Center from 1990-1992 to measure airborne electric fields during the Joint NASA/USAF Airborne Field Mill Program. The objective of this program was to characterize the electrical activity in various weather phenomena common to the NASA-Kennedy area in order to refine Launch Commit Criteria for natural and triggered lightning. The purpose of the program was to safely relax the existing launch commit criteria, thereby increasing launch availability and reducing the chance for weather holds and delays. This paper discusses the operational conduct of the flight test, including environmental/safety considerations, aircraft instrumentation and modification, test limitations, flight procedures, and the procedures and responsibilities of the personnel in the ground station. Airborne field mill data were collected for all the Launch Commit Criteria during two summer and two winter deployments. These data are now being analyzed.

  16. Two YF-12 aircraft in flight

    NASA Technical Reports Server (NTRS)

    1975-01-01

    The YF-12A (60-6935) carries the 'coldwall' heat transfer pod on a pylon beneath the forward fuselage. The pod is seen with its insulating coating intact. In the foreground, the YF-12C flies photo chase. The coldwall project, supported by Langley Research Center, consisted of a stainless steel tube equipped with thermocouples and pressure-sensors. A special insulating coating covered the tube, which was chilled with liquid nitrogen. At Mach 3, the insulation could be pyrotechnically blown away from the tube, instantly exposing it to the thermal environment. The experiment caused many inflight difficulties, such as engine unstarts, but eventually researchers got a successful flight. The Flight Research Center's involvement with the YF-12A, an interceptor version of the Lockheed A-12, began in 1967. Ames Research Center was interested in using wind tunnel data that had been generated at Ames under extreme secrecy. Also, the Office of Advanced Research and Technology (OART) saw the YF-12A as a means to advance high-speed technology, which would help in designing the Supersonic Transport (SST). The Air Force needed technical assistance to get the latest reconnaissance version of the A-12 family, the SR-71A, fully operational. Eventually, the Air Force offered NASA the use of two YF-12A aircraft, 60-6935 and 60-6936. A joint NASA-USAF program was mapped out in June 1969. NASA and Air Force technicians spent three months readying 935 for flight. On 11 December 1969, the flight program got underway with a successful maiden flight piloted by Col. Joe Rogers and Maj. Gary Heidelbaugh of the SR-71/F-12 Test Force. During the program, the Air Force concentrated on military applications, and NASA pursued a loads research program. NASA studies included inflight heating, skin-friction cooling, 'coldwall' research (a heat transfer experiment), flowfield studies, shaker vane research, and tests in support of the Space Shuttle landing program. Ultimately, 935 became the workhorse of the program, with 146 flights between 11 December 1969 and 7 November 1979. The second YF-12A, 936, made 62 flights. It was lost in a non-fatal crash on 24 June 1971. It was replaced by the so-called YF-12C (SR-71A 61-7951, modified with YF-12A inlets and engines and a bogus tail number 06937). The Lockheed A-12 family, known as the Blackbirds, were designed by Clarence 'Kelly' Johnson. They were constructed mostly of titanium to withstand aerodynamic heating. Fueled by JP-7, the Blackbirds were capable of cruising at Mach 3.2 and attaining altitudes in excess of 80,000 feet. The first version, a CIA reconnaissance aircraft that first flew in April 1962 was called the A-12. An interceptor version was developed in 1963 under the designation YF-12A. A USAF reconnaissance variant, called the SR-71, was first flown in 1964. The A-12 and SR-71 designs included leading and trailing edges made of high-temperature fiberglass-asbestos laminates. The NASA YF-12 research program was ambitious; the aircraft flew an average of once a week unless down for extended maintenance or modification. Program expenses averaged $3.1 million per year just to run the flight tests. NASA crews for the YF-12 included pilots Fitzhugh Fulton and Donald Mallick, anf flight test engineers Victor Horton and Ray Young. Other NASA test pilots checked out in the YF-12A included John Manke, William Dana, Gary Krier, Einar Enevoldson, Tom McMurtry, Steve Ishmael, and Michael Swann. The YF-12C was only flown by Fulton, Mallick, Horton, and Ray.

  17. YF-12A and YF-12C in flight formation at dawn

    NASA Technical Reports Server (NTRS)

    1975-01-01

    The YF-12A (60-6935) carries the 'coldwall' heat transfer pod on a pylon beneath the forward fuselage. The pod is seen with its insulating coating intact. In the background, the YF-12C flies photo chase. The coldwall project, supported by Langley Research Center, consisted of a stainless steel tube equipped with thermocouples and pressure-sensors. A special insulating coating covered the tube, which was chilled with liquid nitrogen. At Mach 3, the insulation could be pyrotechnically blown away from the tube, instantly exposing it to the thermal environment. The experiment caused many inflight difficulties, such as engine unstarts, but eventually researchers got a successful flight. The Flight Research Center's involvement with the YF-12A, an interceptor version of the Lockheed A-12, began in 1967. Ames Research Center was interested in using wind tunnel data that had been generated at Ames under extreme secrecy. Also, the Office of Advanced Research and Technology (OART) saw the YF-12A as a means to advance high-speed technology, which would help in designing the Supersonic Transport (SST). The Air Force needed technical assistance to get the latest reconnaissance version of the A-12 family, the SR-71A, fully operational. Eventually, the Air Force offered NASA the use of two YF-12A aircraft, 60-6935 and 60-6936. A joint NASA-USAF program was mapped out in June 1969. NASA and Air Force technicians spent three months readying 935 for flight. On 11 December 1969, the flight program got underway with a successful maiden flight piloted by Col. Joe Rogers and Maj. Gary Heidelbaugh of the SR-71/F-12 Test Force. During the program, the Air Force concentrated on military applications, and NASA pursued a loads research program. NASA studies included inflight heating, skin-friction cooling, 'coldwall' research (a heat transfer experiment), flowfield studies, shaker vane research, and tests in support of the Space Shuttle landing program. Ultimately, 935 became the workhorse of the program, with 146 flights between 11 December 1969 and 7 November 1979. The second YF-12A, 936, made 62 flights. It was lost in a non-fatal crash on 24 June 1971. It was replaced by the so-called YF-12C (SR-71A 61-7951, modified with YF-12A inlets and engines and a bogus tail number 06937). The Lockheed A-12 family, known as the Blackbirds, were designed by Clarence 'Kelly' Johnson. They were constructed mostly of titanium to withstand aerodynamic heating. Fueled by JP-7, the Blackbirds were capable of cruising at Mach 3.2 and attaining altitudes in excess of 80,000 feet. The first version, a CIA reconnaissance aircraft that first flew in April 1962 was called the A-12. An interceptor version was developed in 1963 under the designation YF-12A. A USAF reconnaissance variant, called the SR-71, was first flown in 1964. The A-12 and SR-71 designs included leading and trailing edges made of high-temperature fiberglass-asbestos laminates. The NASA YF-12 research program was ambitious; the aircraft flew an average of once a week unless down for extended maintenance or modification. Program expenses averaged $3.1 million per year just to run the flight tests. NASA crews for the YF-12 included pilots Fitzhugh Fulton and Donald Mallick, anf flight test engineers Victor Horton and Ray Young. Other NASA test pilots checked out in the YF-12A included John Manke, William Dana, Gary Krier, Einar Enevoldson, Tom McMurtry, Steve Ishmael, and Michael Swann. The YF-12C was only flown by Fulton, Mallick, Horton, and Ray.

  18. Leadership Competencies for the USAF Acquisition Community

    DTIC Science & Technology

    2002-04-01

    RAND National Defense Fellow writing on leadership for the 21st USAF) labeled “the intellectual progeny of Burn’s transformational theory .”21 In 1999...1) a historical perspective of leadership and management in academic theory , (2) challenges facing the USAF that suggest a new leadership paradigm...the question at hand. Her research reflects a more studied academic understanding of leadership and management theory than does the work of Brolin

  19. Air and Space Power Journal. Volume 30, Number 2, Summer 2016

    DTIC Science & Technology

    2016-01-01

    Nicholas J. Thomas, USAF, PE Features Thinking beyond the Books ❙ 15 Sociological Biases of Our Military Institutions Ben Zweibelson Institutional ...Retired Editor, Strategic Studies Quarterly Air Force Research Institute Dr. Grant T. Hammond USAF Center for Strategy and Technology Dr. Dale L...Hayden Air Force Research Institute Col S. Clinton Hinote Military Fellow Council on Foreign Relations Dr. Thomas Hughes USAF School of Advanced Air and

  20. A Cost Analysis of Dining Facilities: Should the Air Force Continue to Operate Dining Facilities

    DTIC Science & Technology

    2009-03-01

    accounted for. After receiving estimates from both WPAFB ( Burkholder , 2008) and Travis AFB (Yu, 2008) and comparing those estimates with actual...doc=GetTRDoc.pdf Brinker, Steven D. MSgt, USAF, FSS/FSVF, Peterson AFB, CO. Personal Correspondence. 25 August 2008. Burkholder , Dave E. Civilian...USAF, CEMM/AFMC, Wright Patterson AFB, OH. Personal Correspondence. 3 September 2008. Coats, John N. Captain, USAF, SAF/FMFF, Washington DC

  1. 3,700 USAF Junior Acquisition Officers! Rebalance USAF Manning Priorities Now

    DTIC Science & Technology

    2017-04-06

    duties because they represent basically “no-cost” manpower to the headquarters and base -level leaders. The USAF pays for their military salary and...Colonel, United States Air Force A Research Report Submitted to the Faculty In Partial Fulfillment of the Graduation Requirements Advisor: Colonel...academic research paper are those of the author and do not reflect the official policy or position of the US government, the Department of Defense

  2. Joint Force Quarterly. Number 19, Summer 1998

    DTIC Science & Technology

    1998-08-01

    Shelton, USA Publisher ADVISORY COMMITTEE LTG Richard A. Chilcoat, USA ■ National Defense University Chairman BG David A. Armstrong, USA (Ret.) ■ Office of...College Maj Gen Richard L. Engel, USAF ■ Industrial College of the Armed Forces Maj Gen Timothy A. Kinnan, USAF ■ Air War College Col David M. Lumsden...BOARD Hans Binnendijk ■ National Defense University Chairman Richard K. Betts ■ Columbia University Col J. Lee Blank, USAF ■ National War College Col

  3. An Application of Instructional System Development to Determine Financial Management Education Needs for Logistics Management Positions.

    DTIC Science & Technology

    1976-09-01

    The purpose of this research effort was to determine the financial management educational needs of USAF graduate logistics positions. Goal analysis...was used to identify financial management techniques and task analysis was used to develop a method to identify the use of financial management techniques...positions. The survey identified financial management techniques in five areas: cost accounting, capital budgeting, working capital, financial forecasting, and programming. (Author)

  4. Observations During GRIP from HIRAD: Ocean Surface Wind Speed and Rain Rate

    NASA Technical Reports Server (NTRS)

    Miller, Timothy L.; James, M. W.; Jones, L.; Ruf, C. S.; Uhlhorn, E. W.; Bailey, M. C.; Buckley, C. D.; Simmons, D. E.; Johnstone, S.; Peterson, A.; hide

    2011-01-01

    HIRAD (Hurricane Imaging Radiometer) flew on the WB-57 during NASA's GRIP (Genesis and Rapid Intensification Processes) campaign in August - September of 2010. HIRAD is a new C-band radiometer using a synthetic thinned array radiometer (STAR) technology to obtain cross-track resolution of approximately 3 degrees, out to approximately 60 degrees to each side of nadir. By obtaining measurements of emissions at 4, 5, 6, and 6.6 GHz, observations of ocean surface wind speed and rain rate can be inferred. This technique has been used for many years by precursor instruments, including the Stepped Frequency Microwave Radiometer (SFMR), which has been flying on the NOAA and USAF hurricane reconnaissance aircraft for several years. The advantage of HIRAD over SFMR is that HIRAD can observe a +/- 60-degree swath, rather than a single footprint at nadir angle. Results from the flights during the GRIP campaign will be shown, including images of brightness temperatures, wind speed, and rain rate. To the extent possible, comparisons will be made with observations from other instruments on the GRIP campaign, for which HIRAD observations are either directly comparable or are complementary. Potential impacts on operational ocean surface wind analyses and on numerical weather forecasts will also be discussed.

  5. Statistical Study of Aircraft Icing Probabilities at the 700- and 500- Millibar Levels over Ocean Areas in the Northern Hemisphere

    NASA Technical Reports Server (NTRS)

    Perkins, Porter J.; Lewis, William; Mulholland, Donald R.

    1957-01-01

    A statistical study is made of icing data reported from weather reconnaissance aircraft flown by Air Weather Service (USAF). The weather missions studied were flown at fixed flight levels of 500 millibars (18,000 ft) and 700 millibars (10,000 ft) over wide areas of the Pacific, Atlantic, and Arctic Oceans. This report is presented as part of a program conducted by the NACA to obtain extensive icing statistics relevant to aircraft design and operation. The thousands of in-flight observations recorded over a 2- to 4-year period provide reliable statistics on icing encounters for the specific areas, altitudes, and seasons included in the data. The relative frequencies of icing occurrence are presented, together with the estimated icing probabilities and the relation of these probabilities to the frequencies of flight in clouds and cloud temperatures. The results show that aircraft operators can expect icing probabilities to vary widely throughout the year from near zero in the cold Arctic areas in winter up to 7 percent in areas where greater cloudiness and warmer temperatures prevail. The data also reveal a general tendency of colder cloud temperatures to reduce the probability of icing in equally cloudy conditions.

  6. Sampling and Data Gathering Strategies for Future USAF Anthropometry

    DTIC Science & Technology

    1976-02-01

    of USAF body size data. The approach we suggest would be less costly and more responsive to the needs of the USAF than periodic massive surveys...has been that many of these photographs were taken primarily for somatotyping rather than for measure- ment. Another source of difficulty has been...goals and we have recently i j accepted responsibility under an AMRL research contract to demonstrate that this is so. V Of all the non-standard

  7. The Effect of Values on System Development Project Outcomes

    DTIC Science & Technology

    2009-03-01

    before me and upon whose broad shoulders I stand. Men like Col John Boyd (USAF, ret), Col Chet Richards (USAF, ret), Col James Burton (USAF, ret), Chuck...with new homes that could have housed more than 8,000 people. - President Dwight D. Eisenhower, April 19, 1953 I. Introduction This research...Boyne, 2007 RUBRIC SCORE: 30 F-Score:10 I-Score: 5 S-Score:10 T-Score:5 OUTCOME: A SAMPLE STATEMENTS: FAST “The Navy men liked everything

  8. The Military Casualty with Combat Related Acute Post Traumatic Stress Disorder

    DTIC Science & Technology

    1984-05-01

    explored. A researcher designed "Combat Fatigue Questionnaire" was mailed to 600 USAF nurses selected randomly. Three hundred sixty one USAF nurses...psychiatry noted: "Exhaustion was selected because it best described the appearance of most psychia- tric casualties" (p. xvii). Ernie Pyle, a World War II...Haber & Runyon, PL 1977), 600 (13.3% of the total USAF nurse population) names were selected . The "Combat Fatigue Questionnaire" was mailed between

  9. Pullout of a Rigid Insert Adhesively Bonded to an Elastic Half Plane.

    DTIC Science & Technology

    1983-12-01

    COMMAND UNITED STATES AIR FORCE C-= °84 02 13 071. C,, W % d 6 This document was prepared by the Department of Engineering Mechanics, USAF Academy Faculty...THOMAS E. KULLGREN, Lt Col, USAF Project Engineer /Scientist Professor and Acting Head, Department of Engineering Mechanics KENNETH E. SIEGETH Lt Col...Department of Engineering (Ifapphicable) Mechanics USAFA/DFEM 6c. ADDRESS (City. State and ZIP Code) 7b. ADDRESS (City, Slate and ZIP Code) USAF Academy

  10. 32 CFR 842.12 - HQ USAF claims responsibility.

    Code of Federal Regulations, 2010 CFR

    2010-07-01

    ... Administrative Management Program (CAMP) reviews. (2) Implements claims and tort litigation policies, issues... LITIGATION ADMINISTRATIVE CLAIMS Functions and Responsibilities § 842.12 HQ USAF claims responsibility. (a...

  11. The F-16 Onboard Oxygen Generating System: Performance Evaluation and Man Rating

    DTIC Science & Technology

    1983-08-01

    OXYGEN GENERATING , YSTEM: PERFORMANCE EVALUATION AND MAN RATING Thomas C. Horch , Captain, USAF Richard L. Miller, Ph.D. John B. Bomar, Jr...C. Horch , Capt, USAF; R. L. Miller, 8. CONTRACT OR GRANT NUMBER(i) Ph.D.; J. B. Bomar, Jr., Lt Col, IJSAF, BSC; J. B. Tedor, Maj, USAF, BSC; R. D...limitation (as of 1983); however, the information may no longer need protection since it is 14 years. At the time of its publication, Capt Thomas Horch

  12. Space Resilience and the Contested, Degraded, and Operationally Limited Environment: The Gaps in Tactical Space Operations

    DTIC Science & Technology

    2014-12-01

    Operationally Limited Environment The Gaps in Tactical Space Operations Capt Bryan M. Bell , USAF 2d Lt Even T. Rogers, USAF The ability of space...David S. Fadok, “John Boyd and John Warden: Airpower’s Quest for Strategic Paralysis ,” in The Paths of Heaven: The Evolution of Airpower Theory, ed...Warden,” 365. Capt Bryan M. Bell , USAF Captain Bell (BS, University of Florida; MS, Air Force Institute of Technology) is assistant operations officer and

  13. Project CHECO Southeast Asia Report. USAF Tactics Against Air & Ground Defenses in SEA, November 1968 - May 1970

    DTIC Science & Technology

    1970-09-25

    EB-66 Orbits for Drone Flight .......................... 50 16. ( EB-66 Orbits in Support of B-52 Mission ................ 50I 3 ix I~WI ’CNON.11...outmaneuver it. During the period of this report, while SAMs were fired at several USAF aircraft and shot down several drones , the USAF lost no manned...Oblique camaras had beendesigned to allow photography from a safe distance, but the heavy tree cover in Laos usually required vertical photography for

  14. Reassessment of Occupational Health Among U.S. Air Force Remotely Piloted Aircraft (Drone) Operators

    DTIC Science & Technology

    2017-04-05

    As a result, the U.S. Air Force (USAF) School of Aerospace Medicine was requested to conduct a field survey to assess for general areas of health...services; and reasons for increased prescription and over-the-counter medication usage ). The purpose of this study was to reevaluate for changes in...major commands within the continental United States completed the web-based survey , resulting in an estimated 40% response rate. Statistical analyses

  15. USAF Bioenvironmental Noise Data Handbook. Volume 172. Hush-House Noise Suppressor (Aero Systems Engineering, Inc.) Far-Field Noise.

    DTIC Science & Technology

    1982-07-01

    other data are used for any purpose other than a definitely related Government procurement operation, the GoverMent, therebY incur no responsiblity...Royal Road Springfield, Virginia 22161 Federal Government agencies and their contractors registered with Defense 1Tcbnlcal information Center should...As Specified in ANSI Standard Number S1.4-(R1976) PNLT Tone Corrected Perceived Noise Level As Specified in Federal Aviation Regulation (FAR) Part 36

  16. Installation Restoration Program Records Search for MacDill Air Force Base, Florida.

    DTIC Science & Technology

    1982-06-01

    in Jun 1981 to identify the potential for contamination resulting from past disposal practices. On 26-27 Jan 82, representatives of USAF OEHL, AFESC...13 May 1979 8 Major Plant Communities at MacDill AFB III - 15 9 Location Map of Possible Contaminated Areas at IV - 21 MacDill AFB 10 Historical...RCRA) and implementing regulations. The purpose of the DOD policy is to control the migration of hazardous material contaminants from DOD

  17. Health Care Providers Attitudes and Practices Regarding the Purpose and Use of Advance Directives in a Military Health Care Setting

    DTIC Science & Technology

    1998-05-01

    inadequate health care provider training and skills about advance directives have been cited for low completion rates. Family nurse practitioners (FNPs), in...Fry, S. (1996). Ethical dimensions of nursing and health care . In J. Creasa & B. Parker (Eds.). Conceptual foundations of professional nursing ...HEALTH CARE SETTING by Bridget L. Larew, Maj, USAF, NC Thesis Presented to the Graduate School of Nursing Faculty of the Uniformed Services University

  18. Wastewater Characterization and Hazardous Waste Technical Assistance Survey, Bergstrom AFB Texas

    DTIC Science & Technology

    1990-01-01

    1 FCTE " MAR 12J990 US NANCY S. HEDGECOCK, I t USAF BSC January 1990 Final Report Distribution Is unlimited; approved for public release AF...names or commercial products in this publication is for illustration purposes and does not constitute endorsement or recomendation for use by the United...States Air Force. The Public Affairs Office has reviewed this report, and it is releasable to the National lechnical Information Service, where it

  19. Why an Eye Limiting Display Resolution Matters

    NASA Technical Reports Server (NTRS)

    Kato, Kenji Hiroshi

    2013-01-01

    Many factors affect the suitability of an out-the-window simulator visual system. Contrast, brightness, resolution, field-of-view, update rate, scene content and a number of other criteria are common factors often used to define requirements for simulator visual systems. For the past 7 years, NASA has worked with the USAF on the Operational Based Vision Assessment Program. The purpose of this program has been to provide the USAF School of Aerospace Medicine with a scientific testing laboratory to study human vision and testing standards in an operationally relevant environment. It was determined early in the design that current commercial and military training systems wern't well suited for the available budget as well as the highly research oriented requirements. During various design review meetings, it was determined the OBVA requirements were best met by using commercial-off-the-shelf equipment to minimize technical risk and costs. In this paper we will describe how the simulator specifications were developed in order to meet the research objectives and the resulting architecture and design considerations. In particular we will discuss the image generator architecture and database developments to meet eye limited resolution.

  20. Reconnaissance of chemical quality of surface water and fluvial sediment in the Price River Basin, Utah

    USGS Publications Warehouse

    Mundorff, J.C.

    1972-01-01

    This report on the quality of surface water in the Price River basin was prepared by the U.S. Geological Survey in cooperation with the Utah Department of Natural Resources, Division of Water Rights. The primary purpose of the reconnaissance on which this report is based was to obtain information about (1) the general chemical characteristics of surface water throughout the basin, (2) the effect of the natural environment and of present water use on these chemical characteristics, and (3) general characteristics of the sediment discharge of selected streams in the basin. A secondary objective was the definition of specific problem areas or reaches in which marked deterioration in water quality was evident.

  1. Terrorist and Insurgent Unmanned Aerial Vehicles: Use, Potentials, and Military Implications

    DTIC Science & Technology

    2015-08-01

    Strategic. While the drone swarms of normal and micro - sized UAVs projected in this threat scenario may still be a few decades out and possibly...craft for reconnaissance and pro- paganda video purposes. Such groups are still very much in an experimental phase of using these craft and possess...technol- ogy trends influencing their potential uses, three red teaming threat scenarios have been created for early warning purposes: 1) Single UAV

  2. Corps Helicopter Attack Planning System (CHAPS). Positional Handbook. Appendix A. Messages. Appendix B. Statespace Construction Sample Session

    DTIC Science & Technology

    1989-10-01

    REVIEW MENU PROGRAM (S) CHAPS PURPOSE AND OVERVIEV The Do Review menu allows the user to select which missions to perform detailed analysis on and...input files must be resident on the computer you are running SUPR on. Any interface or file transfer programs must be successfully executed prior to... COMPUTER PROGRAM WAS DEVELOPED BY SYSTEMS CONTROL TECHNOLOGY FOR THE DEPUTY CHIEF OF STAFF/OPERATIONS,HQ USAFE. THE USE OF THE COMPUTER PROGRAM IS

  3. Impact of Scheduled Attrition Rates on Meeting Monthly Sortie Goals in United States Air Force Bomb Wings

    DTIC Science & Technology

    2009-06-12

    predict future losses in the monthly flying schedules. The purpose of the attrition is to ensure that units meet their sortie contract consistently. In...an era of decreasing force size, it is important for units to maximize aircrew training operations, without wasting manpower and resources. Thus, the ...primary research question is as follows: Is the current USAF scheduling technique of using a 5-year historical attrition rate an effective way to

  4. Innovative Surveillance and Risk Reduction Systems for Family Maltreatment, Suicidality, and Substance Problems in the USAF

    DTIC Science & Technology

    2006-03-01

    suicidality, and alcohol/drug problems. Managing risk and increasing resilience in military human resources (i.e., “Force Health Protection”) is a top...problems. Managing risk and increasing resilience in military human resources (i.e., “Force Health Protection”) is a top priority for DoD and Armed...Behavioral Health representatives, as well as at AF- IDS meetings. 4 Wave 1 Bases (Tyndall AFB, Barksdale AFB, Shaw AFB) The primary purpose of

  5. USAF Warrior Studies: Air Superiority in World War 2 and Korea,

    DTIC Science & Technology

    1983-01-01

    was impractical and seldom, if ever. achievable. So the concept evolved in World War 11 into theater counter-air force operations. The practice was to...Crete had fallen, and the British had practically no airplanes at all in the Western Desert. From my observations. I think the British were really in...our relationships to the Arm\\. the XII Air Support Command, tf.or all practical purposes. was under If C’orps,. At the t ime. 11 Corps s% as commnanded

  6. Optimizing the Weapons Officer in the Mobility Air Forces

    DTIC Science & Technology

    2015-06-19

    terms of professional development, what should the progression of a Weapons Officer in the MAF look like after graduation from the USAF Weapons School...appropriately. Many KC-135 commanders have openly admitted that they do not know what to do with their WOs at the unit level on a daily basis, and many...UCLA professor, and it relates to the Delphic oracle from ancient Greece whose prophetess would reveal the divine purpose of the gods in order to shape

  7. Health Care Providers’ Attitudes and Practices Regarding the use of Advance Directives in a Military Health Care Setting

    DTIC Science & Technology

    1998-10-02

    PROVIDERS’ ATTITUDES AND PRACTICES REGARDING THE USE OF ADVANCE DIRECTIVES IN A MILITARY HEALTH CARE SETTING by Bridget L. Larew, Maj, USAF, NC Thesis...entitled: "HEALTH CARE PROVIDER’S ATTITUDES AND PRACTICES REGARDING THE PURPOSE AND USE OF ADVANCE DIRECTIVES IN A MILITARY HEALTH CARE SETTING" beyond...health care, recognized under State law (whether statutory or as recognized by the courts of the State) and relating to the provision of such care

  8. Standard Procedures for Air Force Operational Test and Evaluation. Volume I.

    DTIC Science & Technology

    1974-10-01

    of the foregoing, and assuming the successful advocacy of the prcposed OT&E a Test Directive is drafted by AFTEC, reviewed by HQ USAF, and upon...design purposes. A successful approach to this problem used by both Air Force and Army OT&E agencies is to conduct an analysis of the operational mission...conduct an analysis of the mission structure involved in the OT&E. This constitutes a top level structure of the scenario with identification of the players

  9. An Assessment of the USAFE School Board Test Program

    DTIC Science & Technology

    2002-07-01

    2000. USAFE Strategic Plan on Dependent Education, Headquarters, USAFE, October 1998. Vajont ES, http://www.vajo-es.eu.odedodea.edu/ Vogelweh ES...Pordenone ES K–6 109 2/2/0 Vajont ES K–6 157 2/2/0 Aviano AB 4 1,365 11/11/1 4/4/1 10/0 Incirlik ES K–6 475 3/3/0 Incirlik HS 7–12 217...Aviano) K–6 109 AF SB VAJONT ES (Aviano) K–6 157 AVIANO ES K–6 629 AVIANO HS 7–12 470 VICENZA ES K–6 480 A IAC VICENZA HS 7–12 251

  10. Air-to-Air Encounters in Southeast Asia. Volume I. Account of F-4 and F-8 Events Prior to 1 March 1967

    DTIC Science & Technology

    1967-10-01

    Project of the following Air ) Force pilots is acknowledged: Thomas H. Curtis, Maj., USAF Leslie C . Long, Capt., USAF Robert S. Maxwell , Capt., USAF R. P...maneuvering combat. Aircrew of two valid in GC1 envlronment c Di. Dlstracting in v4 ual engagement, because must think about back seat. Coordinatuc 2-Jficult...EVENTS PRIOR TO MARCH 1967(U) John S. Atrincilo. Project Leader Reproduced From Best Available Copy October !967 /I L U J %r. ,-~i ’, *J * . oc,,,11C

  11. 2001 Industry Studies: Munitions

    DTIC Science & Technology

    2001-01-01

    Lt Col Michael P. Howe, USAF Lt Col William E . MacLure, USAF Mr. Terrence K. May, Dept of the Air Force LTC Paul M. McQuain, USA CDR David L. Prater...USN CAPT Steven K. Tucker, USN Lt Col Richard L. Wojick , Jr., USAF Mr. Michael J. Yurina, Dept of the Navy Dr. Thomas C. Hone, faculty CAPT Ralph...FY98 FY99 FY00 FY01 FY02 FY03 FY04 FY05 FY 00 $ BI LL IO N RDT& E - S&T (Far-Term) RDT& E - Development (Near- and Mid-Term) Procurement (Near-Term) 6 As

  12. The Seasonal Predictability of Extreme Wind Events in the Southwest United States

    NASA Astrophysics Data System (ADS)

    Seastrand, Simona Renee

    Extreme wind events are a common phenomenon in the Southwest United States. Entities such as the United States Air Force (USAF) find the Southwest appealing for many reasons, primarily for the an expansive, unpopulated, and electronically unpolluted space for large-scale training and testing. However, wind events can cause hazards for the USAF including: surface wind gusts can impact the take-off and landing of all aircraft, can tip the airframes of large wing-surface aircraft during the performance of maneuvers close to the ground, and can even impact weapons systems. This dissertation is comprised of three sections intended to further our knowledge and understanding of wind events in the Southwest. The first section builds a climatology of wind events for seven locations in the Southwest during the twelve 3-month seasons of the year. The first section further examines the wind events in relation to terrain and the large-scale flow of the atmosphere. The second section builds upon the first by taking the wind events and generating mid-level composites for each of the twelve 3-month seasons. In the third section, teleconnections identified as consistent with the large-scale circulation in the second paper were used as predictor variables to build a Poisson regression model for each of the twelve 3-month seasons. The purpose of this research is to increase our understanding of the climatology of extreme wind events, increase our understanding of how the large-scale circulation influences extreme wind events, and create a model to enhance predictability of extreme wind events in the Southwest. Knowledge from this paper will help protect personnel and property associated with not only the USAF, but all those in the Southwest.

  13. The Prevalence of E-Cigarette Use in a Sample of U.S. Air Force Recruits

    PubMed Central

    Little, Melissa A.; Derefinko, Karen J.; Colvin, Lauren; Ebbert, Jon O.; Bursac, Zoran; Talcott, Gerald W.; Richey, Phyllis A.; Klesges, Robert C.

    2015-01-01

    Introduction The prevalence of electronic cigarette (e-cigarette) use is increasing markedly in the general population. Yet, remarkably little research exists to examine these ongoing trends in at-risk populations, and nothing is known about the prevalence of e-cigarette use among military personnel. The purpose of the current study is to provide recent (2013–2014) data on the prevalence of regular e-cigarette use in a population of recruits prior to their entry into the U.S. military. Methods The study utilized a cross-sectional assessment of e-cigarette and other tobacco and nicotine–containing product (TNCP) use in 2013–2014 among 10,043 U.S. Air Force (USAF) recruits in Technical Training. Chi-square tests, the Cochran–Armitage test for trend, and logistic regression models tested differences and trends across time for e-cigarette use. Results The rate of e-cigarette use among recruits was 5.2%, which doubled (3% to 6.5%, p<0.0001) across a 1-year period. E-cigarette use was associated with increased odds of all measured TNCPs, as well as dual and poly use (all p<0.0001). Conclusions Rates of e-cigarette use are slightly higher in young USAF recruits than in the general population, and e-cigarette users are likely to be using other TNCPs in tandem. Although additional work is needed to understand the reasons for this concomitant use, this is a necessary first step to understanding e-cigarette use prevalence in military populations. Historic trends suggest that, like general populations, e-cigarette use is on the rise for those entering the USAF and should be monitored to inform future prevention programming. PMID:25896193

  14. Fuel freeze-point investigations. Final report, September 1982-March 1984

    DOE Office of Scientific and Technical Information (OSTI.GOV)

    Desmarais, L.A.; Tolle, F.F.

    1984-07-01

    The objective of this program was to conduct a detailed assessment of the low-temperature environment to which USAF aircraft are exposed for the purpose of defining a maximum acceptable fuel freeze-point and also to define any operational changes required with the use of a high freeze-point fuel. A previous study of B-52, C-141, and KC-135 operational missions indicated that the -58 C freeze point specification was too conservative. Based on recommendations resulting from the previous program, several improvements in the method of analysis were made, such as: expansion of the atmospheric temperature data base, the addition of ground temperature analysis,more » the addition of fuel-freezing analysis to the one-dimensional fuel-temperature computer program, and the examination of heat transfer in external fuel tanks, such as pylon or tip tanks. The B-52, C-141, and KC-135 mission were analyzed again, along with the operational missions of two tactical airplanes, the A-10 and F-15; -50C was determined to be the maximum allowable freeze point for a general-purpose USAF aviation turbine fuel. Higher freeze points can be tolerated if the probability of operational interference is acceptably low or if operational changes can be made. Study of atmospheric temperatures encountered for the missions of the five-study aircraft indicates that a maximum freeze point of -48 C would not likely create any operational difficulties in Northern Europe.« less

  15. Program Office Guide to Ada. Edition 1

    DTIC Science & Technology

    1986-09-17

    publication. MARK V. ZIEMBA , 2Lt, USAF Project Officer, Software Engineering Tools & Methods ARTHUR G. DECELLES, Capt, USAF Program Manager, Computer...UNLIMITED G3 SAME AS RPT D DTIC USERS 21 ABSTRACT SECURITY CLASSIFICATION UNCLASSIFIED 22a. NAME OF RESPONSIBLE INDIVIDUAL M.V. Ziemba

  16. Studying to Learn.

    ERIC Educational Resources Information Center

    Air Univ., Maxwell AFB, AL.

    This booklet was prepared in response to a demand from Air Force Officers returning to academic study after being out of school for several years. Its main purpose is to help returning veterans learn how to study. The guide is divided into three sections: (1) the "Reconnaissance-Read-Recall" (RRR) system of study, (2) concepts in "How We Learn,"…

  17. THe high altitude reconnaissance platform (HARP) and its capabilities

    DOE Office of Scientific and Technical Information (OSTI.GOV)

    Rusk, D.; Rose, R.L.; Gibeau, E.

    1996-10-01

    The High Altitude Reconnaissance Platform (HARP), a Learjet 36A, is a multi-purpose, long-range, high-altitude aircraft specially modified to serve as a meteorological observation platform. Its instrument suite includes: particle probes, Ka-band radar, two-color lidar, infrared spectroradiometer, thermometer, hygrometer, liquid water probe, and a gust probe. Aeromet scientists have developed software and hardware systems that combine data using sensor fusion concepts, providing detailed environmental information. The HARP answers the need for defining and predicting meteorological conditions throughout large atmospheric volumes particularly in areas where conventional surface and upper-air observations are not available. It also fills the need for gathering and predictingmore » meteorological conditions along an optical sensor`s line of sight or a missile`s reentry path. 6 refs., 2 figs., 4 tabs.« less

  18. New Observations of C-band Brightness Temperatures and Ocean Surface Wind Speed and Rain Rate From the Hurricane Imaging Radiometer (HIRAD)

    NASA Technical Reports Server (NTRS)

    Miller, Timothy L.; James, M. W.; Roberts, J. B.; Buckley, C. D.; Biswas, S.; May, C.; Ruf, C. S.; Uhlhorn, E. W.; Atlas, R.; Black, P.; hide

    2012-01-01

    HIRAD flew on the WB-57 during NASA's GRIP (Genesis and Rapid Intensification Processes) campaign in August September of 2010. HIRAD is a new C-band radiometer using a synthetic thinned array radiometer (STAR) technology to obtain cross-track resolution of approximately 3 degrees, out to approximately 60 degrees to each side of nadir. By obtaining measurements of emissions at 4, 5, 6, and 6.6 GHz, observations of ocean surface wind speed and rain rate can be retrieved. This technique has been used for many years by precursor instruments, including the Stepped Frequency Microwave Radiometer (SFMR), which has been flying on the NOAA and USAF hurricane reconnaissance aircraft for several years to obtain observations within a single footprint at nadir angle. Results from the flights during the GRIP campaign will be shown, including images of brightness temperatures, wind speed, and rain rate. Comparisons will be made with observations from other instruments on the GRIP campaign, for which HIRAD observations are either directly comparable or are complementary. Features such as storm eye and eyewall, location of storm wind and rain maxima, and indications of dynamical features such as the merging of a weaker outer wind/rain maximum with the main vortex may be seen in the data. Potential impacts on operational ocean surface wind analyses and on numerical weather forecasts will also be discussed.

  19. Lightning Launch Commit Criteria for America's Space Program

    NASA Technical Reports Server (NTRS)

    Roeder, W. P.; Sardonia, J. E.; Jacobs, S. C.; Hinson, M. S.; Harms, D. E.; Madura, J. T.; DeSordi, S. P.

    1999-01-01

    The danger of natural and triggered lightning significantly impacts space launch operations supported by the USAF. The lightning Launch Commit Criteria (LCC) are used by the USAF to avoid these lightning threats to space launches. This paper presents a brief overview of the LCC.

  20. Aircraft Control Using Engine Thrust: A History of Learning TOC Real-Time

    NASA Technical Reports Server (NTRS)

    Cole, Jennifer H.; Batteas, Frank; Fullerton, Gordon

    2006-01-01

    A history of learning the operation of Throttles Only Control (TOC) to control an aircraft in real time using engine thrust is shown. The topics include: 1) Past TOC Accidents/Incidents; 2) 1972: DC-10 American Airlines; 3) May 1974: USAF B-52H; 4) April 1975: USAF C-5A; 5) April 1975: USAF C-5A; 6) 1981: USAF B-52G; 7) August 1985: JAL 123 B-747; 8) JAL 123 Survivor Story; 9) JAL 123 Investigation Findings; 10) July 1989: UAL 232 DC-10; 11) UAL 232 DC-10; 12) Eastwind 517 B-737; 13) November 2003: DHL A-300; 14) Historically, TOC has saved lives; 15) Automated Throttles-Only Control; 16) PCA Project; 17) Propulsion-Controlled Aircraft; 18) MD-11 PCA System and Flight Test Envelope; 19) MD-11 Simulation, PCA ILS-Soupled Landing Dispersion; 20) Throttles-Only Pitch and Roll Control Power; 21) PCA in Commercial Fleet; 22) Fall 2005: PCAR Project; 23) PCAR Background - TOC; and 24) PCAR Background - TOC.

  1. Epidemiology of HIV among US Air Force Military Personnel, 1996–2011

    PubMed Central

    Hakre, Shilpa; Mydlarz, Dariusz G.; Dawson, Peter; Danaher, Patrick J.; Gould, Philip L.; Witkop, Catherine T.; Michael, Nelson L.; Peel, Sheila A.; Scott, Paul T.; Okulicz, Jason F.

    2015-01-01

    Objective The objectives of this study were to describe the epidemiology of HIV in the United States Air Force (USAF) from 1996 through 2011 and to assess whether socio-demographic characteristics and service-related mobility, including military deployments, were associated with HIV infection. Methods We conducted a retrospective cohort analysis of USAF personnel who were HIV-infected during the study period January 1, 1996 through December 31, 2011 and a matched case-control study. Cases were USAF personnel newly-diagnosed with HIV during the study period. Five randomly-selected HIV-uninfected controls were matched to each case by age, length of service, sex, race, service, component, and HIV test collection date. Socio-demographic and service-related mobility factors and HIV diagnosis were assessed using conditional logistic regression. Results During the study period, the USAF had 541 newly diagnosed HIV-infected cases. HIV incidence rate (per 100,000 person-years) among 473 active duty members was highest in 2007 (16.78), among black/ African-American USAF members (26.60) and those aged 25 to 29 years (10.84). In unadjusted analysis restricted to personnel on active duty, 10 characteristics were identified and considered for final multivariate analysis. Of these single (adjusted odds ratio [aOR], 8.15, 95% confidence interval [CI] 5.71–11.6) or other marital status (aOR 4.60, 95% CI 2.72–7.75), communications/ intelligence (aOR 2.57, 95% CI 1.84–3.60) or healthcare (aOR 2.07, 95% CI 1.28–3.35) occupations, and having no deployment in the past 2 years before diagnosis (aOR 2.02, 95% CI 1.47–2.78) conferred higher odds of HIV infection in adjusted analysis. Conclusion The highest risk of HIV infection in the USAF was among young unmarried deployment-naïve males, especially those in higher risk occupation groups. In an era when worldwide military operations have increased, these analyses identified potential areas where targeted HIV prevention efforts may be beneficial in reducing HIV incidence in the USAF military population. PMID:25961564

  2. QDR 2001: Strategy-Driven Choices for America’s Security

    DTIC Science & Technology

    2001-04-01

    McKenzie, Jr., USMC; Lieutenant Colonel Philip M. Ruhlman , USAF; Lieutenant Colonel John J. Spinelli, USA; and Captain Sam J. Tangredi, USN. Their...one chosen by their service: Lieutenant Colonel Frank McKenzie, USMC; Lieutenant Colonel Philip Ruhlman , USAF; Lieutenant Colonel John Spinelli, USA

  3. Special Features of the Air to Space Neutron Transport Problem

    DTIC Science & Technology

    2017-09-14

    Fig. 5 from (NOAA, NASA , USAF, 1976, p. 13). .......................................................... 194 Atmospheric density as a function of...75 Physical constants for 1976 U.S. Standard Atmosphere. (NOAA, NASA ... NASA , USAF, 1976, p. 3), and computed base temperatures and pressures from the surface to 86 geometric kilometers

  4. Make the Squadron Great Again: Rethinking the USAF Industrial Age Structure to Build Mission Centered Unit Cohesion

    DTIC Science & Technology

    2018-04-09

    Powers , “Air Force Jobs in Demand: When Careers are on the Stressed List,” The Balance website, https://www.thebalance.com/air-force-jobs-4052612...way to success and upon faith in the cause or program and in the leadership, usually connoting, esp. when qualified by the adjective high , a confident...from the Wright Brothers to Martin Luther King Jr. to examine the power of infusing a sense of purpose in the people one leads.16 Similarly, in The

  5. Addendum to the Closure Report for Corrective Action Unit 411: Double Tracks Plutonium Dispersion (Nellis), Nevada Test and Training Range, Nevada, Revision 0

    DOE Office of Scientific and Technical Information (OSTI.GOV)

    Burmeister, Mark

    2016-11-01

    The Corrective Action Unit (CAU) 411 Closure Report (CR) was published in June 2016 (NNSA/NFO, 2016). The purpose of this addendum is to clarify language in the CR relating to the field instrument for the detection of low-energy radiation (FIDLER), provide the waste disposal documentation for waste generated during the corrective action investigation (CAI), and reference a letter from the U.S. Air Force (USAF) regarding the closure of CAU 411.

  6. Air and Space Power Joumal. Volume 25, Number 3, Fall 2011

    DTIC Science & Technology

    2011-01-01

    Navarre, Florida Mr. Charles Tustin Kamps USAF Air Command and Staff College Dr. Tom Keaney Johns Hopkins University Col Merrick E. Krause , USAF, Retired...fighter pilots such as Wolfgang Falck, Hajo Herrmann, and Hans-Joachim Jabs. In this aspect, Heaton (a professor at the American Military University

  7. 2001 Industry Studies: Aircraft

    DTIC Science & Technology

    2001-01-01

    Air Force Mr Bill Craft, Dept of State LTC Conway Ellers, USA Col Bob D’Amico, USAF Mr Dave Hersh, Dept of Navy Mr John Krieger , Dept of Treasury Mr...the Navy), John Krieger (Department of Treasury), and Colonel James Solinski (USAF) 34 The world has changed significantly since the end of the Cold War

  8. Situational Leadership Theory to the USAF Officer Training School.

    DTIC Science & Technology

    1988-04-01

    Commanders Develop Leadership Styles ................... 4 FeedbacK Systems .............................................. 5 Conclusion...7 Leadership Styles ....................... . ..................... 9 CHAPTER THREE--THE SITUATIONAL LEADERSHIP THEORY AND OTS The USAF Officer...53 . 6 P N 5p* LIST OF ILLUSTRATIONS a- I" TABLES TABLE P-I-- Leadership Styles Matched With Maturity Levels

  9. 78 FR 41042 - Proposed Collection; Comment Request

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-07-09

    ... DEPARTMENT OF DEFENSE Department of the Air Force [Docket ID: USAF-2013-0030] Proposed Collection; Comment Request AGENCY: Air Force Chief of Chaplains Office (DOD/USAF/HQ AF/HC), Department of the Air Force, Department of Defense. ACTION: Notice. In compliance with Section 3506(c)(2)(A) of the Paperwork...

  10. Using Nanotechnology to Detect Nerve Agents

    DTIC Science & Technology

    2011-01-01

    56 | Air & Space Power Journal Air Force Institute of Technology Using Nanotechnology to Detect Nerve Agents Lt Col Mark N. Goltz , PhD, USAF...Retired Dr. Dong Shik Kim Maj LeeAnn Racz, PhD, USAF* *Lieutenant Colonel Goltz and Major Racz are faculty members in the Department of Systems and

  11. The 1984-1985 Antarctic Search for Meteorites (ANSMET) Field Program

    NASA Technical Reports Server (NTRS)

    Sandford, Scott A.

    1986-01-01

    The purpose of the 1984-1985 ANSMET (Antarctic Search for Meteorites) expedition was to recover meteorites from the Main, Near Western, Middle Western, and Far Western icefields in the Allan Hills area and to carry out a reconnaissance of other nearby blue icefields. A brief summary of the locations and maps visited are provided.

  12. Purposeful Development of the Intelligence, Surveillance, and Reconnaissance for Space Cadre

    DTIC Science & Technology

    2016-07-13

    available. For these reasons, an attack on US space assets seems an un- likely scenario. However, the threat to space has changed since 1967. Enhanced and...get them up to speed on issues that affect ISR support to ACC weapon systems. Context The above scenarios would seem unthinkable to ACC but are very

  13. Unmanned aerial vehicles (UAVs) in pest management: Progress in the development of a UAV-deployed mating disruption system for Wisconsin cranberries

    USDA-ARS?s Scientific Manuscript database

    Unmanned aerial vehicles (UAVs) hold significant promise for agriculture. Currently, UAVs are being employed for various reconnaissance purposes (“eyes in the sky”), but not as pest control delivery systems. Research in Wisconsin cranberries is taking UAVs in a new direction. The Steffan and Luck La...

  14. Air and Space Power Journal. Volume 25, Number 3, Fall 2011

    DTIC Science & Technology

    2011-01-01

    Charles Tustin Kamps USAF Air Command and Staff College Dr. Tom Keaney Johns Hopkins University Col Merrick E. Krause , USAF, Retired Department of Homeland...conducted face-to-face interviews with many of the air war leaders and noble night-fighter pilots such as Wolfgang Falck, Hajo Herrmann, and Hans

  15. Heritage, Image and Identity: The Evolution of USAF Leadership

    DTIC Science & Technology

    2011-02-16

    up-in-coming “ Generation Z ” (also known as the “Net or Digital Generation”), which is the most connected and high-tech generation ever seen. 40...for future RPA warrior leaders. 43 The USAF has already set the ground work to position “ Generation Z ” RPA pilots for future senior leadership

  16. 77 FR 43816 - Privacy Act of 1974; System of Records

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-07-26

    ... DEPARTMENT OF DEFENSE Department of the Air Force [Docket ID: USAF-2012-0012] Privacy Act of 1974; System of Records AGENCY: Department of the Air Force, DoD. ACTION: Notice to alter a system of records... OSD Federal Register Liaison Officer, Department of Defense. F033 AFCA C SYSTEM NAME: USAF Information...

  17. 13. DETAIL OF CENTER OF CENTRAL CONTROL CONSOLE IN SLC3W ...

    Library of Congress Historic Buildings Survey, Historic Engineering Record, Historic Landscapes Survey

    13. DETAIL OF CENTER OF CENTRAL CONTROL CONSOLE IN SLC-3W CONTROL ROOM SHOWING USAF LAUNCH CONTROLLER AND ASSISTANT USAF LAUNCH CONTROLLER PANELS. CONSOLES AND CHAIRS NEAR NORTH WALL IN BACKGROUND. - Vandenberg Air Force Base, Space Launch Complex 3, Launch Operations Building, Napa & Alden Roads, Lompoc, Santa Barbara County, CA

  18. 76 FR 15231 - Proposed Amendment of Class D and E Airspace; Palmdale, CA

    Federal Register 2010, 2011, 2012, 2013, 2014

    2011-03-21

    ... Palmdale Regional Airport/USAF Plant 42. This action would enhance the safety and management of aircraft operations at Palmdale Regional Airport/USAF Plant 42. This action would also correct the name of the airport..., economic, environmental, and energy-related aspects of the proposal. Communications should identify both...

  19. Army Fixed-Wing Ground Attack Aircraft: A Historical Precedent and Contemporary Rationale

    DTIC Science & Technology

    2015-06-12

    platforms at the tactical level. Fielding such aircraft would free the Air Force to focus on its broader missions while enhancing the capabilities of...ground forces. In fact, an Army attack aircraft would reduce, but not eliminate, the requirement for USAF CAS, freeing the USAF to focus on its

  20. 32 CFR 989.22 - Mitigation.

    Code of Federal Regulations, 2010 CFR

    2010-07-01

    ... EPF informed of the mitigation status. The EPF reports its status, through the MAJCOM, to HQ USAF/A7CI when requested. Upon request, the EPF must also provide the results of relevant mitigation monitoring... forwarded, through the MAJCOM EPF to HQ USAF/A7CI for review within 90 days from the date of signature of...

  1. 32 CFR Appendix A to Part 989 - Glossary of References, Abbreviations, Acronyms, and Terms

    Code of Federal Regulations, 2010 CFR

    2010-07-01

    ... Engineering and the Environment AFCEE/TDB AFCEE Technical Directorate, Built Infrastructure Division (AFCEE... Materiel Command HQ USAF Headquarters, United States Air Force HQ USAF/A7C The Air Force Civil Engineer.../AQR Deputy Assistant Secretary of the Air Force (Science, Technology, and Engineering) SAF/GC Air...

  2. USAF (United States Air Force) bioenvironmental noise data handbook. Volume 2: Index

    NASA Astrophysics Data System (ADS)

    Cole, J. N.; Peachey, N. J.

    1983-03-01

    This report is an index which identifies the individual volumes published during the 1975-1982 period by the Air Force Aerospace Medical Research Laboratory (AFAMRL) as a multi-volume report, ""USAF Bioenvironmental Noise Data Handbook'', AMRL-TR-75-50 and lists those aircraft, ground equipment and other systems reported there in.

  3. Command Structure for Theater Warfare: The Quest for Unity of Command

    DTIC Science & Technology

    1984-09-01

    that trryfari tail forth thr htst from iti—Btturki Major General« Pern M Smith. USAF. and Hark) A Hughe«. USAF. contributed more to the rndertaking...an air. ground, and sea component. These arc generic commands which control all combat operations in the media of the air. ground, and sea. There

  4. British Naval Aviation and the Anti-Submarine Campaign, 1917-18

    DTIC Science & Technology

    2004-01-01

    me. Also, I extend my gratitude to Col Phil Meilinger, USAF (Ret.) and Lt Col Roy Houchin, USAF, for reading some of my earlier chapter drafts and...Revolution, 1912-1918. London: Frank Cass, 1999. Barker, Ralph. A Brief History of the Royal Flying Corps in World War I. London: Robinson, 2002. Beckett

  5. Toward the Implementation of Augmented Reality Training

    ERIC Educational Resources Information Center

    Mayberry, Charles R.

    2013-01-01

    The United States Air Force (USAF) trains C-130H Loadmaster students at Little Rock Air Force Base (AFB) through a civilian contract. The Aircrew Training System (ATS) contractor utilizes a Fuselage Trainer (FuT) to provide scenarios for the Loadmaster students to practice loading and unloading a simulated aircraft. The problem was the USAF does…

  6. Integrating Sensor-Collected Intelligence

    DTIC Science & Technology

    2008-11-01

    collecting, processing, data storage and fusion, and the dissemination of information collected by Intelligence, Surveillance, and Reconnaissance (ISR...Grid – Bandwidth Expansion (GIG-BE) program) to provide the capability to transfer data from sensors to accessible storage and satellite and airborne...based ISR is much more fragile. There was a purposeful drawdown of these systems following the Cold War and modernization programs were planned to

  7. Anesthesia Provider’s Use of the Precordial or Esophageal Stethoscope: Is Anyone Still Listening to the Patient

    DTIC Science & Technology

    1996-06-01

    USAF, NC and Dr. Maura McAuliffe, Lt. Col. , USAF, NC. Dr. Hall served as my qualitative data advisor. Her assi stance ensured an accurate...esophageal stethoscope, Anesthesiology, 65 (5), 534-536. Prielipp, R. c., Kelly , J. S., & Roy, R. C. (1995, August). Use of esophageal or

  8. Evaluating the Impacts of Technology Education on Military Maintenance Students

    ERIC Educational Resources Information Center

    Jordan, Jeremy D.; Curtis, Christopher

    2010-01-01

    The United States Air Force (USAF) provides career and technical education (CTE) to a wide variety of specialty career fields. Training airmen to carry out the mission while honoring the USAF core values of integrity first, service before self, and excellence in all we do is the top priority of military leaders and trainers. Vehicle maintenance is…

  9. Cyberspace Human Capital: Building a Cadre Today to Win Tomorrows War

    DTIC Science & Technology

    2016-04-28

    sustainable and flexible framework that manages and develops a cyberspace cadre, today and into the future. This professional paper examines USAF and DoD...future conflicts, USAF leadership must develop a sustainable and flexible framework that manages and develops cyberspace cadre...international security and stability. CYBERSPACE FORCE MANAGEMENT ACCESSIONS RETENTION INSTITUTIONAL STRUCTURE FORCE DEVELOPMENT EDUCATION TRAINING

  10. Hydrologic reconnaissance of the southern Great Salt Lake Desert and summary of the hydrology of west-central Utah

    USGS Publications Warehouse

    Gates, Joseph S.; Kruer, Stacie A.

    1981-01-01

    This report is the last of 19 hydrologic reconnaissances of the basins in western Utah. The purposes of this series of studies are (1) to analyze available hydrologic data and describe the hydrologic system, (2) to evaluate existing and potential water-resources development, and (3) to identify additional studies that might be needed. Part 1 of this report gives an estimate of recharge and discharge, an estimate of the potential for water-resources development, and a statement on the quality of water in the southern Great Salt Lake Desert part of west-central Utah. Part 2 deals with the same aspects of west-central Utah as a whole. Part 2 also summarizes the evidence of interbasin ground-water flow in west-central Utah and presents a theory for the origin of the water discharged from Fish Springs.

  11. Orbit Determination and Navigation Software Testing for the Mars Reconnaissance Orbiter

    NASA Technical Reports Server (NTRS)

    Pini, Alex

    2011-01-01

    During the extended science phase of the Mars Reconnaissance Orbiter's lifecycle, the operational duties pertaining to navigation primarily involve orbit determination. The orbit determination process utilizes radiometric tracking data and is used for the prediction and reconstruction of MRO's trajectories. Predictions are done twice per week for ephemeris updates on-board the spacecraft and for planning purposes. Orbit Trim Maneuvers (OTM-s) are also designed using the predicted trajectory. Reconstructions, which incorporate a batch estimator, provide precise information about the spacecraft state to be synchronized with scientific measurements. These tasks were conducted regularly to validate the results obtained by the MRO Navigation Team. Additionally, the team is in the process of converting to newer versions of the navigation software and operating system. The capability to model multiple densities in the Martian atmosphere is also being implemented. However, testing outputs among these different configurations was necessary to ensure compliance to a satisfactory degree.

  12. United States Air Force F-35A Operational Basing Environmental Impact Statement. Appendix E: Comments

    DTIC Science & Technology

    2013-09-01

    Nicholas M Civ USAF HQ ACC/A7NS No F-35s in Burlington, Vermont, please! Wherever I go, when people hear I am from Vermont, they wax enthusiastic...them to upkeep a machine that’s sole purpose i s to fly cross t he ocean (or too wherever) and t ake the l ives of many others? Even i f we except this...monstrosi t y of a machine , can we really entrust it to the care of an organization that appears to be unable to write an accurate report? We may

  13. 1958 NASA/USAF Space Probes (ABLE-1). Volume 3; Vehicles, Trajectories, and Flight Histories

    NASA Technical Reports Server (NTRS)

    1959-01-01

    The three NASA/USAF lunar probes of August 17, October 13, and November 8, 1958 are described. Details of the program, the vehicles, the payloads, the firings, the tracking, and the results are presented. Principal result was the first experimental verification of a confined radiation zone of the type postulated by Van Allen and others.

  14. Will Empowerment of USAF Program Managers Mitigate the Acquisitions Crisis

    DTIC Science & Technology

    2016-06-10

    FAR Federal Acquisition Regulations GAO Government Accountability Office MDAP Major Defense Acquisition Program USAF United States Air Force ix...actually run the project. The Government Accountability Office (GAO),2 along with many other organizations, including Congress in their 2016 National...1 Government Accountability Office (GAO), GAO-06-110, Best Practices: Better Support of Weapons Systems Program Managers Needed to

  15. Clinging to the Past: The Air Force’s War on Dual-Career Families

    DTIC Science & Technology

    2014-06-01

    combines existing research on stress and work-family conflict with new primary research on current USAF dual-career families in the form of a case...incompatibilities between the Air Force family schema (conceptions of, and practices relating to, USAF families). The study combines existing research on stress ... Stress Pathways ..................................................... 74 Figure 5, Civilian Dual-Career Stress Pathways

  16. Tropical Cyclone Report, 1986.

    DTIC Science & Technology

    1986-01-01

    Gunzelman, USN CAPT Robert F. Crosby, USAF LT Harry S. Gatanis, USN *AG2 Kristopher W. Buttermore, USN TSGT Marguritta H. Smith, USAF *AG2 Kevin L. Cobb...dollars~ wuyur~v to a ’ U~se- rx nif, or est ,A te city. of’ ~ was seotrong nn5xa rttengsiv Iaag dito, n n.. N wAer ~z lins fr prted names. iedn eatthan

  17. Current Barriers to Successful Implementation of FIST Principles

    DTIC Science & Technology

    2013-07-01

    risks will surface during development that could not have been predicted. Managing a thin budget with no schedule slack for these unknown-unknowns is...Fleischer » Keywords: Fast, Inexpensive, Simple, Tiny (FIST); Program Management ; Heuristics; Innovation; Oversight Current Barriers to Successful...Implementation of FIST Principles Capt Brandon Keller, USAF, and Lt Col J. Robert Wirthlin, USAF The Fast, Inexpensive, Simple, and Tiny (FIST

  18. Time Critical Conventional Strike from Strategic Standoff

    DTIC Science & Technology

    2009-03-01

    Competitor with Emerging Counter-Space Capability has Destroyed U.S. Leo Satellite...destroyed a U.S. Low Earth Orbit ( LEO ) satellite. The U.S. desires to prevent future damage to other satellites in the constellation, but with...Precision from ISR Assets January 18 – 19 2007 Col Paul Gydesen USAF USAF ICBM, Ballistic Missile – Prompt Global Strike Dr. Barry Hannah Navy

  19. 32 CFR 842.121 - Referring a claim to the US Attorney.

    Code of Federal Regulations, 2011 CFR

    2011-07-01

    ... 32 National Defense 6 2011-07-01 2011-07-01 false Referring a claim to the US Attorney. 842.121... to the US Attorney. Only HQ USAF/JACC authorizes referral of a claim to the US Attorney. The base SJA...-case basis, HQ USAF/JACC will authorize referral of a case to the US Attorney by telephone. ...

  20. Establishing and Maintaining Trust for an Airborne Network. Search and Rescue Enterprise: Security Assessment Report

    DTIC Science & Technology

    2014-12-01

    Area Code) (937) 528-8142 Standard Form 298 (Rev. 8-98) Prescribed by ANSI Std. Z39-18 1 MITCHELL, LOLITA V CIV USAF AFMC AFRL/RYOX To...MITCHELL, LOLITA V CIV USAF AFMC AFRL/RYOX Subject: FW: Final Report Change - Search and Rescue Security Assessment From: J M Schlesselman [mailto:joe

  1. Keeping Our Eyes Open: Conducting Aerial Reconnaissance Without Space

    DTIC Science & Technology

    2016-05-01

    worldwide went haywire. Spark discharges shocked telegraph operators and set the telegraph paper on fire. Even when telegraphers disconnected the... CORONA , and satellite reconnaissance was born.156 (See Figure X) Lessons From The Eisenhower Years This era of bi-polar tension, ostensibly...satellite reconnaissance capability started with CORONA appeared to offer a way to achieve overhead reconnaissance without attribution or risk. For

  2. Reconnaissance Data Recording Study

    DTIC Science & Technology

    1996-02-15

    Sources The data sources listed are those sources that are currently being used for the Advanced Tactical Air Reconnaissance System ( ATARS ). This sensor...technology is about 10 years old (circa 1985). Current sensor technology is evolving towards farming type systems versus the ATARS pushbroom systems...Reconnaissance System ( ATARS ) or any Tactical Reconnaissance System (TRS). The emphasis of this analysis was to investigate the application of the Sony

  3. High area rate reconnaissance (HARR) and mine reconnaissance/hunter (MR/H) exploratory development programs

    NASA Astrophysics Data System (ADS)

    Lathrop, John D.

    1995-06-01

    This paper describes the sea mine countermeasures developmental context, technology goals, and progress to date of the two principal Office of Naval Research exploratory development programs addressing sea mine reconnaissance and minehunting technology development. The first of these programs, High Area Rate Reconnaissance, is developing toroidal volume search sonar technology, sidelooking sonar technology, and associated signal processing technologies (motion compensation, beamforming, and computer-aided detection and classification) for reconnaissance and hunting against volume mines and proud bottom mines from 21-inch diameter vehicles operating in deeper waters. The second of these programs, Amphibious Operation Area Mine Reconnaissance/Hunter, is developing a suite of sensor technologies (synthetic aperture sonar, ahead-looking sonar, superconducting magnetic field gradiometer, and electro-optic sensor) and associated signal processing technologies for reconnaissance and hunting against all mine types (including buried mines) in shallow water and very shallow water from 21-inch diameter vehicles. The technologies under development by these two programs must provide excellent capabilities for mine detection, mine classification, and discrimination against false targets.

  4. Proposed Doctrine Based Structure of the Armored Reconnaissance Squadron

    DTIC Science & Technology

    2017-06-09

    adversarial, non -state non -adversarial and International Organizations (IO). Non -state adversarial are groups that oppose the interest and priorities of...Canada and its partners; these groups include violent extremist organizations and criminal organizations. Non - state non -adversarial are groups that... Grouping can be executed to facilitate control , communications, function or output of a collection. Recall, that for the purpose of this analysis

  5. Project CHECO Southeast Asia Report. SEAsia Glossary, 1961-1970

    DTIC Science & Technology

    1970-02-01

    47 conducted reconnaissance approximately three times a month over the Gulf of Tonkin. 3 BPE Best Preliminary Estimate BPP Border Patrol Police (Thai...education, training, public works, agriculture, transportation, communications, health, and other areas. Military and civic leaders work with local...VC term for Strategic Village captured and fortified for VC purposes. COMBAT HORNET (S) CONUS tests, training, and procurement for AC-119/K aircraft

  6. Camouflage target reconnaissance based on hyperspectral imaging technology

    NASA Astrophysics Data System (ADS)

    Hua, Wenshen; Guo, Tong; Liu, Xun

    2015-08-01

    Efficient camouflaged target reconnaissance technology makes great influence on modern warfare. Hyperspectral images can provide large spectral range and high spectral resolution, which are invaluable in discriminating between camouflaged targets and backgrounds. Hyperspectral target detection and classification technology are utilized to achieve single class and multi-class camouflaged targets reconnaissance respectively. Constrained energy minimization (CEM), a widely used algorithm in hyperspectral target detection, is employed to achieve one class camouflage target reconnaissance. Then, support vector machine (SVM), a classification method, is proposed to achieve multi-class camouflage target reconnaissance. Experiments have been conducted to demonstrate the efficiency of the proposed method.

  7. Report of Evaluation of Decompression Sickness, Beale AFB, 10-14 Aug 2009

    DTIC Science & Technology

    2009-09-01

    MICHAELSON, Col, USAF, MC, SFS Chief, Hyperbaric Medicine Branch //SIGNED// JAMES W. WEISSMANN, Col, USAF, BSC Chief, Aerospace Medicine...Robert S Michaelson (Chief of Hyperbaric Medicine at USAFSAM), Dr. Andy Pilmanis (Consultant), and Dr. Tom Morgan (711 HPW/HPS). BACKGROUND The...without consent of originator’s office. MP = Mission Pilot HBOT = Hyperbaric Oxygen Treatment CNS = Central Nervous System HA = headache BAFB = Beale

  8. 5. Credit USAF, ca. 1942. Original housed in the Photograph ...

    Library of Congress Historic Buildings Survey, Historic Engineering Record, Historic Landscapes Survey

    5. Credit USAF, ca. 1942. Original housed in the Photograph Files, AFFTC/HO, Edwards AFB, California. View of Bell Aircraft XP-59A Airacomet in flight. This was the United States military's first jet propelled aircraft which was extensively flight tested in secrecy at the Muroc Flight Test Base (North Base). - Edwards Air Force Base, North Base, North Base Road, Boron, Kern County, CA

  9. Air Force Flight Screening: Evolutionary Changes, 1917-2003

    DTIC Science & Technology

    2004-12-01

    US), FFA (Switzerland), Siai Marchetti (Italy), SAAB (Sweden), Slingsby (United Kingdom), Glassair (US), Piper (US), American General (US), and...Jumper, USAF/CC, [Academy Flight Screening program], 10 Apr 03, 3) BBP , 557 FTS/CC, “USAF 66 As the...Academy Flight Screening (AFS) Program,” 4 Feb 03, 4) BBP , 557 FTS/CC, “AFS Funding,” 22 Jan 03, 5) Position Paper, 557 FTS/CC

  10. High Accuracy Attitude Control of a Spacecraft Using Feedback Linearization

    DTIC Science & Technology

    1992-05-01

    High Accuracy Attitude Control of a Spacecraft Using Feedback Linearization A Thesis Presented by Louis Joseph PoehIman, Captain, USAF B.S., U.S. Air...High Accuracy Attitude Control of a Spacecraft Using Feedback Linearization by Louis Joseph Poehlman, Captain, USAF Submitted to the Department of...31 2-4 Attitude Determination and Control System Architecture ................. 33 3-1 Exact Linearization Using Nonlinear Feedback

  11. Multi-Objective Optimization for Speed and Stability of a Sony AIBO Gait

    DTIC Science & Technology

    2007-09-01

    MULTI-OBJECTIVE OPTIMIZATION FOR SPEED AND STABILITY OF A SONY AIBO GAIT THESIS Christopher A. Patterson, Second Lieutenant, USAF AFIT/GCS...07-17 MULTI-OBJECTIVE OPTIMIZATION FOR SPEED AND STABILITY OF A SONY AIBO GAIT THESIS Presented to the Faculty Department of...MULTI-OBJECTIVE OPTIMIZATION FOR SPEED AND STABILITY OF A SONY AIBO GAIT Christopher A. Patterson, BS Second Lieutenant, USAF

  12. Project CHECO Southeast Asia Report. USAF Control of Airstrikes in Support of Indigenous Lao Ground Forces

    DTIC Science & Technology

    1972-07-19

    a low pass over the "airstrip" to clear the area of vehicles, children , and animals, and then return and land before the locals 287/ had a chance...II I • • • - SECit!T NO PORN - validating authority not given to other USAF FACs in Laos. The X-Ray per- sonnel were selected by local Lao

  13. United States Air Force F-35A Operational Basing Environmental Impact Statement. Appendix E: Comments

    DTIC Science & Technology

    2013-09-01

    Germanos, Nicholas M Civ USAF HQ ACC/A7NS From: Sent: To: Subject: Dear Mr. Germanos, Ginger Hobbs Monday, July 15, 2013 9:45PM Germanos...considerat ion of all t he facts. Thank you, Ginger Hobbs 1 E-757 Germanos, Nicholas M Civ USAF HQ ACC/A7NS From: Sent: To: Subject: Kara Schwartz

  14. Airborne Reconnoissance Pod Flijht Test

    NASA Astrophysics Data System (ADS)

    Henkel, P.; Sturz, R.

    1987-02-01

    Today's political environment has seen an increasing effort for deficit reduction resulting in defense budget cuts and decreased spending. Military capability is difficult to maintain under these circumstances unless innovation offers a low-cost alternative. One critical military capability is the ability to collect intelligence data efficiently. Tactical aerial reconnaissance its a large part of this capability. The aerial reconnaissance process usually involves dedicated aircraft with a single mission. The aircraft used for this mission are specially outfitted versions of fighter aircraft with avionics modified for the reconnaissance task. The luxury of such aircraft appears to be a thing of the past. This can be seen by recent attempts to designate a next-generation reconnaissance aircraft without success. Stopgap measures have been offered which consist of updating existing reconnaissance aircraft with new sensors and improved avionics. Upgrades definitely have their place, but do not take advantage of the multirole capabilities of modern tactical aircraft. Tactical aircraft avionics suites afford options not found in older aircraft, plus improved maintenance aspects of such systems. One method of overcoming aircraft generation gaps is to include a reconnaissance option in the form of a pod. The reconnaissance pod is not a new concept, but one which may have "found its time." The reconnaissance pod outfitted with modern sensors offers versatility, survivability and economy while reducing logistics, maintenance and training. This paper discusses a pod and sensor suite flight test program performed to verify the design features of the aerial reconnaissance pod.

  15. A decade of U.S. Air Force bat strikes

    USGS Publications Warehouse

    Peurach, Suzanne C.; Dove, Carla J.; Stepko, Laura

    2009-01-01

    From 1997 through 2007, 821 bat strikes were reported to the U.S. Air Force (USAF) Safety Center by aircraft personnel or ground crew and sent to the National Museum of Natural History, Smithsonian Institution, for identification. Many samples were identified by macroscopic and or microscopic comparisons with bat specimens housed in the museum and augmented during the last 2 years by DNA analysis. Bat remains from USAF strikes during this period were received at the museum from 40 states in the United States and from 20 countries. We confirmed that 46% of the strikes were caused by bats, but we did not identify them further; we identified 5% only to the family or genus level, and 49% to the species level. Fifty-five of the 101 bat-strike samples submitted for DNA analysis have been identified to the species level. Twenty-five bat species have been recorded striking USAF planes worldwide. The Brazilian free-tailed bat (Tadarida brasiliensis; n = 173) is the species most commonly identified in USAF strike impacts, followed by the red bat (Lasiurus borealis; n = 83). Bat strikes peak during the spring and fall, with >57% occurring from August through October; 82% of the reports that included time of strike were recorded between 2100 and 0900 hours. More than 12% of the bat strikes were reported at >300 m above ground level (AGL). Although <1% of the bat-strike reports indicated damage to USAF aircraft, cumulative damage for 1997 through 2007 totaled >$825,000 and >50% of this sum was attributable to 5 bat-strike incidents. Only 5 bats from the 10 most damaging bat strikes were identified to the species level, either because we did not receive remains with the reports or the sample was insufficient for identification.

  16. AN/ASQ-197 provides commonality to Recce systems and avionics upgrades

    NASA Astrophysics Data System (ADS)

    Regan, Brendan P.

    1993-02-01

    In an attempt to strike a balance between increases in multi-role tactical air reconnaissance mission tasking and simultaneous decreases in defense spending, many users are evaluating upgrades to existing sensors and reconnaissance systems. At the heart of any cost-effective reconnaissance system upgrade must be a flexible reconnaissance management system, capable of filling multiple rolls in today's film backed reconnaissance system, while enabling successful transition to the Electro-Optical (EO) system of tomorrow. As a case in point this paper describes enhanced effectiveness and growth potential that Fairchild's AN/ASQ-197 Sensor Control-Data Display Set (SC-DDS) can provide.

  17. GSOSTATS Database: USAF Synchronous Satellite Catalog Data Conversion Software. User's Guide and Software Maintenance Manual, Version 2.1

    NASA Technical Reports Server (NTRS)

    Mallasch, Paul G.; Babic, Slavoljub

    1994-01-01

    The United States Air Force (USAF) provides NASA Lewis Research Center with monthly reports containing the Synchronous Satellite Catalog and the associated Two Line Mean Element Sets. The USAF Synchronous Satellite Catalog supplies satellite orbital parameters collected by an automated monitoring system and provided to Lewis Research Center as text files on magnetic tape. Software was developed to facilitate automated formatting, data normalization, cross-referencing, and error correction of Synchronous Satellite Catalog files before loading into the NASA Geosynchronous Satellite Orbital Statistics Database System (GSOSTATS). This document contains the User's Guide and Software Maintenance Manual with information necessary for installation, initialization, start-up, operation, error recovery, and termination of the software application. It also contains implementation details, modification aids, and software source code adaptations for use in future revisions.

  18. USAF shale oil program status

    NASA Technical Reports Server (NTRS)

    Delaney, C. L.

    1984-01-01

    The test and evaluation program on shale derived fuel being conducted by the Air Force is intended to accomplish the minimum amount of testing necessary to assure both the safe use of shale oil derived turbine fuels in operational USAF aircraft and its compatibility with USAF handling systems. This program, which was designed to take advantage of existing R&D testing programs, began in 1981. However, due to a problem in acquiring the necessary fuel, the testing program was suspended until July 1983 when an additional sample of shale derived fuel was received. Tentatively, the Air Force is planning to make three relatively minor revisions to the procurement specifications requirements for the production shale derived fuel. These are: (1) Aromatic Contest (min) - 9% (by volume); (2) Nitrogen (max - 20 ppm by weight); and (3) Antioxidants - 9.1 g/100 gal (U.S.)

  19. USAF Bioenvironmental Noise Data Handbook. Volume 155. CH-3 in-flight crew noise

    NASA Astrophysics Data System (ADS)

    Hille, H. K.

    1982-09-01

    The CH-3 is a USAF tactical combat transport helicopter. This report provides measured data defining the bioacoustic environments at flight crew/passenger locations inside this helicopter during normal flight operations. Data are reported for nine locations in a wide variety of physical and psychoacoustic measures: overall and band sound pressure levels, C weighted and A weighted sound levels, preferred speech interference level, perceived noise levels and limiting times for total daily exposure of personnel with and without standard Air Force ear protectors. Refer to Volume 1 of this handbook, USAF Bioenvironmental Noise Data handbook, Vol. 1: Organization, Content and Application, AMRL-TR-75-50(1) 1975, for discussion of the objective and design of the handbook, the types of data presented, measurement procedures, instrumentation, data processing, definitions of quantities, symbols, equations, applications, limitations, etc.

  20. USAF Environmental Noise Data Handbook. Volume 150: C-140 in-flight crew noise

    NASA Astrophysics Data System (ADS)

    Hille, H. K.

    1982-09-01

    The C-140 is a USAF transport aircraft used for operational support. This report provides measured data defining the bioacoustic environments at flight crew/passenger locations inside this aircraft during normal flight operations. Date are reported for seven locations in a wide variety of physical and psychoacoustic measures: overall and band sound pressure levels, C-weighted and A-weighted sound levels, preferred speech interference level, perceived noise level, and limiting times for total daily exposure of personnel with and without standard Air Force ear protectors. Refer to Volume 1 of this handbook, USAF Bioenvironmental Noise Data Handbook, Vol. 1: Organization, Content and Application, AMRL-TR-75-50(1) 1975, for discussion of the objective and design of the handbook, the types of data presented, measurement procedures, instrumentation, data processing, definitions of quantities, symbols, equations, applications, limitations, etc.

  1. Soldier’s Load and the Multifunctional Utility/Logistics and Equipment-Transport

    DTIC Science & Technology

    2010-06-11

    Utility/Logistics Equipment-Countermine and an armed reconnaissance variant called the Armed Robotic Vehicle-Assault (Light). All three Lockheed...mission and requires various levels of human- robot interaction (National Institute of Standards and Technology 2004, 14). Teleoperation. A mode of...use of robots as an act of cowardice, especially in cultures which hold in high esteem the nobility of sacrificing oneself for a higher purpose (Singer

  2. Behavioral Profiling of Scada Network Traffic Using Machine Learning Algorithms

    DTIC Science & Technology

    2014-03-27

    BEHAVIORAL PROFILING OF SCADA NETWORK TRAFFIC USING MACHINE LEARNING ALGORITHMS THESIS Jessica R. Werling, Captain, USAF AFIT-ENG-14-M-81 DEPARTMENT...subject to copyright protection in the United States. AFIT-ENG-14-M-81 BEHAVIORAL PROFILING OF SCADA NETWORK TRAFFIC USING MACHINE LEARNING ...AFIT-ENG-14-M-81 BEHAVIORAL PROFILING OF SCADA NETWORK TRAFFIC USING MACHINE LEARNING ALGORITHMS Jessica R. Werling, B.S.C.S. Captain, USAF Approved

  3. Environmental Assessment: Hurlburt Field Soundside Boathouse and Restroom Facility Construction

    DTIC Science & Technology

    2007-08-01

    seq., and Air Force Instruction (AFI) 32-7061, The Environmental Impact Analysis Process, the USAF concludes that the Proposed Action will have no...U.S.C.) §4321, et seq., and Air Force Instruction (AFI) 32-7061, The Environmental Impact Analysis Process, the USAF concludes that the Proposed...et seq. • AFI 32-7061, The Environmental Impact Analysis Process These regulations require federal agencies to analyze the potential environmental

  4. Evaluation of Inventory Reduction Strategies: Balad Air Base Case Study

    DTIC Science & Technology

    2012-03-01

    produced by conducting individual simulations using a unique random seed generated by the default Anylogic © random number generator. The...develops an agent-based simulation model of the sustainment supply chain supporting Balad AB during its closure using the software AnyLogic ®. The...research. The goal of USAF Stockage Policy is to maximize customer support while minimizing inventory costs (DAF, 2011:1). USAF stocking decisions

  5. Fall of the Fighter Generals: The Future of USAF Leadership

    DTIC Science & Technology

    2001-06-01

    World War II, Colonel S . F. Giffen argued that one of the great lessons to be...Generals: The Future of USAF Leadership Contract Number Grant Number Program Element Number Author( s ) Danskine, Wm. Bruce Project Number Task...results of World War II led to the separation of part of the Army to form an independent Air Force. Or the transition can be smooth, such as when the

  6. The USAF Academy Honor System.

    DTIC Science & Technology

    1988-04-01

    Dec 1986, p. H- 8 . 3. Hosmer, Clark, Colonel (Retired), USAF. Personal Interview, 29 September 1987. 4 . Maus, Steven A. Cadet Wing Honor Education...the basic procedures of the Honor System. A. Strongly Agree 8 % B. Agree 53% C. Neutral 21% D. Disagree 14% E. Strongly Disagree 4 % 28. It is possible...DISTRIBUTION/AVAILABILITY OF REPORT STATEMENT "A" 2b. DECLASSIFICATION/DOWNGRADING SCHEDULE Approved for public release; Distribution is unlimited. 4

  7. Supplier Development: A Long-Term Supportability Option For USAF Engines

    DTIC Science & Technology

    2012-02-01

    Supply Chain Management Practices..................8 AF and DoD Regulations "Limitation or Hoax" Can USAF Develop Suppliers...integrated supply chain management (SCM) process providing engines and parts, aiding in the ability of the depots to meet the warfighter‟s needs. The... supply chain has struggled in the past to support the warfighter with enough engines to accomplish the mission. The engine supply chain management

  8. Case Report: Rhabdomyolysis in Service Member Following SERE Physical Training

    DTIC Science & Technology

    2017-09-19

    Member following SERE physical training. Sb. GRANT NUMBER Sc. PROGRAM ELEMENT NUMBER 6. AUTHOR(S) 5d. PROJECT NUMBER Capt Matthew A Pombo Se. TASK...NOTES 14. ABSTRACT Case Report: Rhabdomyolysis in Service Member following SERE physical training. Authors: Matthew A. Pombo, DO (Capt, USAF...in Service Member following SERE physical training. Authors: Matthew A. Pombo, DO (Capt, USAF); Dwaipayan Chakraborti, MD (MAJ, USA); Joseph Marcus

  9. Combat Medical Modernization: Posturing Low Supply And High Demand Assets To Meet Emerging And Future Capability Requirements

    DTIC Science & Technology

    2015-07-01

    OFFICE OF THE AIR FORCE SURGEON GENERAL FELLOWSHIP PAPER COMBAT MEDICAL MODERNIZATION: POSTURING LOW SUPPLY AND HIGH DEMAND ASSETS TO...Maj, USAF, MSC Scott A. Baker, Capt, USAF, MSC A Research Report Submitted to HQ AF/SG35X In Partial Fulfillment of Medical Plans Fellowship...i TABLE OF FIGURES 3 I. INTRODUCTION 5 II. CURRENT MEDICAL EN-ROUTE CARE CAPABILITY

  10. Application of a Micro Computer-Based Management Information System to Improve the USAF Service Reporting Process

    DTIC Science & Technology

    1990-09-01

    I. Introduction .......................................... 1 General Issue .................................. 1 Specific Research Problem...viii APPLICATION OF A MICRO COMPUTER-BASED MANAGEMENT INFORMATION SYSTEM TO IMPROVE THE USAF SERVICE REPORTING PROCESS I. Introduction General Issue...continued Transfer MIP Responsibility ,KNT WETSS0GEFORM UNCLASSIFIED 904 JAUG 19: iRR iRRl UUUUI HOWE271652_ D- FF:MCH INFO: NONE E. iUCH DATA DEF: NONE F

  11. Assessment of USAFs Hiring Potential of Civilian Scientists and Engineers of the Millennial Generation

    DTIC Science & Technology

    2016-02-12

    AIR WAR COLLEGE AIR UNIVERSITY ASSESSMENT OF USAF’S HIRING POTENTIAL OF CIVILIAN SCIENTISTS AND ENGINEERS OF THE MILLENNIAL GENERATION...government organizations. iv Abstract The Millennial Generation (individuals born 1981-2000) is entering the workforce in large numbers and...of Millennials and what they view as important in their work and social lives revealed policy approaches that could ensure the USAF maximizes it

  12. CAD/CAM Preparation Design Effects on Endodontically Treated and Restored Molars

    DTIC Science & Technology

    2016-05-24

    ii APPROVED: Col Drew W . Fallis Dean, Air Force Postgraduate Dental School iii Acknowledgements Special thanks to Col Howard Roberts, Maj...excerpts, is with the permission of the copyright owner. Signature AARON T. DANCB. MAJ. USAF, DC v Printed Name USAF Postgraduate Dental School Keesler...internal amalgam-dentin 3 interface. Preparations were accomplished by one operator using a high speed electric dental hand piece (EA-SlLT, Adee

  13. Multidimensional Aptitude Battery-Second Edition Intelligence Testing of Remotely Piloted Aircraft Training Candidates Compared with Manned Airframe Training Candidates

    DTIC Science & Technology

    2015-03-01

    assessing the general intelligence and neuropsychological aptitudes of USAF RPA pilot training candidates. Chappelle et al. obtained comprehensive...computer-based intelligence testing (Multidimensional Aptitude Battery-Second Edition [MAB-II]) and neuropsychological screening (MicroCog) on USAF MQ-1... schizophrenia , attention deficit hyperactivity disorder, and autism spectrum disorders) and not on very high functioning populations such as aviators

  14. Military Air Cargo Containerization.

    DTIC Science & Technology

    1996-05-01

    MILITARY AIR CARGO CONTAINERIZATION GRADUATE RESEARCH PAPER Joseph W. Mancy, Major, USAF AFIT/ GMO /LAL/96J-4 : ."•" ’* ■- ’ DEPARTMENT OF...Approved to public release; Distribution UnHmlted ? DTIC QUALITY INSPECTED 1 AFIT/ GMO /LAL/96J-4 MILITARY AIR CARGO CONTAINERIZATION GRADUATE RESEARCH...PAPER Joseph W. Mancy, Major, USAF AFIT/ GMO /LAL/96J-4 19960617 134 Approved for public release; distribution unlimited The views expressed in this

  15. USAF Hearing Conservation Program, DOEHRS-HC Data Repository Annual Report: CY15

    DTIC Science & Technology

    2017-05-31

    AFRL-SA-WP-SR-2017-0014 USAF Hearing Conservation Program, DOEHRS-HC Data Repository Annual Report: CY15 Daniel A. Williams...Conservation Program, DOEHRS-HC Data Repository Annual Report: CY15 5a. CONTRACT NUMBER 5b. GRANT NUMBER 5c. PROGRAM ELEMENT NUMBER 6. AUTHOR...Health Readiness System-Hearing Conservation Data Repository (DOEHRS-HC DR). Major command- and installation-level reports are available quarterly

  16. Characterization of Construction Material Properties through Gamma Spectroscopy, X-ray Fluorescence, and Hyper-spectral Imagery for Background Correction Applications in Nuclear Detection

    DTIC Science & Technology

    2014-03-27

    14 Mar 2014 David J. Bunker, Ph.D. (Chairman) Date ____________//signed//_________________ 14 Mar 2014 Tay W. Johannes, Ph.D...Lt Col, USAF (Member) Date ____________//signed//_________________ 12 Mar 2014 Benjamin R. Kowash, Ph.D., Maj, USAF (Member) Date AFIT-ENP...by Test Date ........................ 28 Figure 3: Comparison of background spectra from 6 October (blue) and 16 September (green

  17. 4. Credit USAF, ca. 1945. Original housed in the Muroc ...

    Library of Congress Historic Buildings Survey, Historic Engineering Record, Historic Landscapes Survey

    4. Credit USAF, ca. 1945. Original housed in the Muroc Flight Test Base, Unit History, 1 September 1942 - 30 June 1945. Alfred F. Simpson Historical Research Agency. United States Air Force. Maxwell AFB, Alabama. Photographic copy of photograph captioned "Hangar No. 2 Hydraulics Room." Location within Building 4402 not determined. - Edwards Air Force Base, North Base, Hangar No. 2, First & A Streets, Boron, Kern County, CA

  18. Copper Doping of Zinc Oxide by Nuclear Transmutation

    DTIC Science & Technology

    2014-03-27

    Copper Doping of Zinc Oxide by Nuclear Transmutation THESIS Matthew C. Recker, Captain, USAF AFIT-ENP-14-M-30 DEPARTMENT OF THE AIR FORCE AIR...NUCLEAR TRANSMUTATION THESIS Presented to the Faculty Department of Engineering Physics Graduate School of Engineering and Management Air Force...COPPER DOPING OF ZINC OXIDE BY NUCLEAR TRANSMUTATION Matthew C. Recker, BS Captain, USAF Approved: //signed// 27 February 2014 John W. McClory, PhD

  19. Religious Accommodation for Military Members in the Twenty-First Century

    DTIC Science & Technology

    2012-02-01

    order and discipline is speculative. He presented a scenario where a female Airman had permission to wear her hijab indoors. When she transferred to the...Lieutenant Colonel, USAF A Research Report Submitted to the Faculty In Partial Fulfillment of the Graduation Requirements Advisor: Dr. Stefan Eisen, Jr...Colonel, USAF (Retired) Maxwell Air Force Base, Alabama February 2012 DISTRIBUTION A . Approved for public release: distribution unlimited 2

  20. Semantic Interpretation of An Artificial Neural Network

    DTIC Science & Technology

    1995-12-01

    ARTIFICIAL NEURAL NETWORK .7,’ THESIS Stanley Dale Kinderknecht Captain, USAF 770 DEAT7ET77,’H IR O C 7... ARTIFICIAL NEURAL NETWORK THESIS Stanley Dale Kinderknecht Captain, USAF AFIT/GCS/ENG/95D-07 Approved for public release; distribution unlimited The views...Government. AFIT/GCS/ENG/95D-07 SEMANTIC INTERPRETATION OF AN ARTIFICIAL NEURAL NETWORK THESIS Presented to the Faculty of the School of Engineering of

  1. United States Air Force Statistical Digest, Fiscal Year 1960. Fifteenth Edition

    DTIC Science & Technology

    1960-09-30

    USAF CIVILIAN EMPLOYEES IN SALARIED AND WAGE BOARD GROUPS EMPLOYED UNDER MILITARY , ASSISTANCE PROGRAM (MAP), AT END OF QUARTER - FY � (Previous year...provide summary data on all aspects of the Mlli_ 165 tary Assistance program administered by the Air Force. The data were compiled from progress reports...Military Assistance . MAP AIRCRAFT - Aircraft in foreign countries provided by the USAF under Military Assistance Program . AIRCRAFT ATTRITION - Aircraft

  2. Moderating Effects of Perceived Organizational Support on the Relationship between Job Satisfaction and Turnover Intentions for Recently Retrained USAF Enlisted Members

    DTIC Science & Technology

    2006-03-01

    career in the service. The turnover body of knowledge was furthered because POS was eliminated as a moderator in the relationship of job satisfaction and...MODERATING EFFECTS OF PERCEIVED ORGANIZATIONAL SUPPORT ON THE RELATIONSHIP BETWEEN JOB SATISFACTION ...EFFECTS OF PERCEIVED ORGANIZATIONAL SUPPORT ON THE RELATIONSHIP BETWEEN JOB SATISFACTION AND TURNOVER INTENTIONS FOR RECENTLY RETRAINED USAF ENLISTED

  3. Senior Leader Perspective on the Air Force Nuclear Enterprise: Todays Issues and the Future

    DTIC Science & Technology

    2016-09-15

    SENIOR LEADER PERSPECTIVE ON THE AIR FORCE NUCLEAR ENTERPRISE: TODAY’S ISSUES AND THE FUTURE GRADUATE RESEARCH PAPER Matthew D. Boone...States. AFIT-ENS-MS-16-S-028 SENIOR LEADER PERSPECTIVE ON THE AIR FORCE NUCLEAR ENTERPRISE: TODAY’S ISSUES AND THE FUTURE GRADUATE... ISSUES AND THE FUTURE Matthew D. Boone, BS, MA Major, USAF Committee Membership: Robert E. Overstreet, Lt Col, USAF, PhD

  4. National Positioning, Navigation, and Timing Architecture Study

    DTIC Science & Technology

    2008-09-01

    Ballooning • Trip Planning Environment • Tide / Current Measures • BLM Tract Management • Oil Spill Containment • Hazardous Waste Remediation...SMC/GPSW (Aerospace) Adde, Barbara GOVT NASA Alexander, Dexter LTC USA SMDC Alexander, Ken GOVT FAA Rep to NCO Allen, Leonard GOVT FRA...Shawn Lt Col USAF NSSO/PNT Brewer, Mike Col USAF OASD/NII Space Programs Brodsky, Beryl CTR NASA (Overlook) Broussard, Robert CTR AFSPC/A5

  5. Security Verification of Secure MANET Routing Protocols

    DTIC Science & Technology

    2012-03-22

    SECURITY VERIFICATION OF SECURE MANET ROUTING PROTOCOLS THESIS Matthew F. Steele, Captain, USAF AFIT/GCS/ ENG /12-03 DEPARTMENT OF THE AIR FORCE AIR...States AFIT/GCS/ ENG /12-03 SECURITY VERIFICATION OF SECURE MANET ROUTING PROTOCOLS THESIS Presented to the Faculty Department of Electrical and Computer...DISTRIBUTION UNLIMITED AFIT/GCS/ ENG /12-03 SECURITY VERIFICATION OF SECURE MANET ROUTING PROTOCOLS Matthew F. Steele, B.S.E.E. Captain, USAF

  6. A B-52H, tail number 61-0025, arrives at NASA's Dryden Flight Research Center after landing July 30,

    NASA Technical Reports Server (NTRS)

    2001-01-01

    NASA Dryden Flight Research Center, Edwards, California, received an 'H' model B-52 Stratofortress aircraft on July 30, 2001. The B-52H will be used as an air-launch aircraft supporting NASA's flight research and advanced technology demonstration efforts. Dryden received the B-52H from the U.S. Air Force's (USAF) 23rd Bomb Squadron, 5th Bombardment Wing (Air Combat Command), located at Minot AFB, N.D. A USAF crew flew the aircraft to Dryden. The aircraft, USAF tail number 61-0025, will be loaned initially, then later transferred from the USAF to NASA. The B-52H is scheduled to leave Dryden Aug. 2 for de-militarization and Programmed Depot Maintenance (PDM) at Tinker Air Force Base (AFB), Oklahoma. The depot-level maintenance is scheduled to last about six months and includes a thorough maintenance and inspection process. The newly arrived B-52H is slated to replace Dryden's famous B-52B '008,' in the 2003-2004 timeframe. It will take about one year for the B-52H to be ready for flight research duties. This time includes PDM, construction of the new pylon, installation of the flight research instrumentation equipment, and aircraft envelope clearance flights.

  7. A B-52H, on loan to NASA's Dryden Flight Research Center, makes a pass down the runway prior to land

    NASA Technical Reports Server (NTRS)

    2001-01-01

    NASA Dryden Flight Research Center, Edwards, California, received an 'H' model B-52 Stratofortress aircraft on July 30, 2001. The B-52H will be used as an air-launch aircraft supporting NASA's flight research and advanced technology demonstration efforts. Dryden received the B-52H from the U.S. Air Force's (USAF) 23rd Bomb Squadron, 5th Bombardment Wing (Air Combat Command), located at Minot AFB, N.D. A USAF crew flew the aircraft to Dryden. The aircraft, USAF tail number 61-0025, will be loaned initially, then later transferred from the USAF to NASA. The B-52H is scheduled to leave Dryden Aug. 2 for de-militarization and Programmed Depot Maintenance (PDM) at Tinker Air Force Base (AFB), Oklahoma. The depot-level maintenance is scheduled to last about six months and includes a thorough maintenance and inspection process. The newly arrived B-52H is slated to replace Dryden's famous B-52B '008,' in the 2003-2004 timeframe. It will take about one year for the B-52H to be ready for flight research duties. This time includes PDM, construction of the new pylon, installation of the flight research instrumentation equipment, and aircraft envelope clearance flights.

  8. Challenges for the aircraft structural integrity program

    NASA Technical Reports Server (NTRS)

    Lincoln, John W.

    1994-01-01

    Thirty-six years ago the United States Air Force established the USAF Aircraft Structural Integrity Program (ASIP) because flight safety had been degraded by fatigue failures of operational aircraft. This initial program evolved, but has been stable since the issuance of MIL-STD-1530A in 1975. Today, the program faces new challenges because of a need to maintain aircraft longer in an environment of reduced funding levels. Also, there is increased pressure to reduce cost of the acquisition of new aircraft. It is the purpose of this paper to discuss the challenges for the ASIP and identify the changes in the program that will meet these challenges in the future.

  9. An Environmental Evaluation of Acid Scrubbers; Building 628, McClellan AFB CA

    DTIC Science & Technology

    1975-08-01

    found collection efficiencies ranging from 42 to 80% for 1 pm particles in low energy scrubbers . High energy scrubbers , venturi and wet dynamic, had...collection elliciency ctyi be obtained but not with low energy wet scrubbers . High energy wet scrubbers ( venturi , wet dynamic, wet fabric nitrations, etc...ENVIRONMENTAL EVALUATION OF ACID SCRUBBERS Building 628. McClellan AFB CA Jerry W. Jackson. Capt, USAF, BSC William £. Normington. Capt, USAF August 1975

  10. A Case for Air Force Reorganization

    DTIC Science & Technology

    2013-04-01

    overstaffing problem exists, sev- eral theories lend insight into why and how this overgrowth occurs. Noted German sociologist Max Weber discusses...USAF Almanac, 1980,” May 1980; “2010 USAF Almanac”; and “Air Force Strength from FY 1948–2012.” 9. Max Weber , On Charisma and Institution Building...MA: Belknap Press of Harvard University Press, 1957), 67. 22. Max Weber , The Theory of Social and Economic Organization, trans. A. M. Henderson and

  11. Development and Employment of Fixed-Wing Gunships 1962-1972

    DTIC Science & Technology

    1982-01-01

    Carl Berger. Mr. Eugene P. Sagstetter, Mary F. Loughlin, and Vanessa D. Allen edited, proofread, and purged the manuscript of the typographical...General Coun.el. USAF Dr. Forrest C. Pogue Lt. General Charles G. Cleveland Smithsonian Institution USAF Commander. Air University. ATC Dr. Edward L...GiUNSHIP I (AC-47) Major Interdiction Areas (Southeast Asia) A NORTH VIETNAM Bar 1 LAOS Steel Tiger THAILAND ’ * Tiger Hound *~ ~T39 VAN DEVELOPMENT OF FIXED

  12. Pulse Coupled Neural Networks for the Segmentation of Magnetic Resonance Brain Images.

    DTIC Science & Technology

    1996-12-01

    PULSE COUPLED NEURAL NETWORKS FOR THE SEGMENTATION OF MAGNETIC RESONANCE BRAIN IMAGES THESIS Shane Lee Abrahamson First Lieutenant, USAF AFIT/GCS/ENG...COUPLED NEURAL NETWORKS FOR THE SEGMENTATION OF MAGNETIC RESONANCE BRAIN IMAGES THESIS Shane Lee Abrahamson First Lieutenant, USAF AFIT/GCS/ENG/96D-01...research develops an automated method for segmenting Magnetic Resonance (MR) brain images based on Pulse Coupled Neural Networks (PCNN). MR brain image

  13. Consideration of USAF (United States Air Force) Logistics Doctrine Principles in a Decision Making Framework.

    DTIC Science & Technology

    1987-09-01

    Henry Fayu.l: planning, organizing, commanding, coordinating, and controlling (Donnelly, Gibson, and Ivancevich , 1984:88). In 2 their text, Donnelly (et...al) describe the management function as "planning, organizing, and controlling (Donnelly, Gibson, and Ivancevich , 1984:5)." 3. Logistics Management...Air Force Weapon Systems. Washington DC: HQ USAF, 1 February 1985. Donnelly, James H., James L. Gibson, John M. Ivancevich , Fundamentals of Management

  14. Air-Sea Battle through Joint Training: Power Projection Sustainability

    DTIC Science & Technology

    2014-05-15

    9 generate our decisive advantage.” 39 An example of cross-domain operations employed by the USN and USAF was the release of an AGM-154C Joint...and Herzegovina. While employing a USAF GBU -15 “electro-optically guided” bomb within close range of a USN AGM-84 SLAM-ER, “electronic... 39 U.S. Office of the Chairman, Joint Chiefs of Staff. Capstone Concept for Joint Operations: Joint Force 2020

  15. Business Process Improvement Applied to Written Temporary Duty Travel Orders within the United States Air Force

    DTIC Science & Technology

    1993-12-01

    Generally Accepted Process While neither DoD Directives nor USAF Regulations specify exact mandatory TDY order processing methods, most USAF units...functional input. Finally, TDY order processing functional experts at Hanscom, Los Angeles and McClellan AFBs provided inputs based on their experiences...current electronic auditing capabilities. 81 DTPS Initiative. This DFAS-initiated action to standardize TDY order processing throughout DoD is currently

  16. Solar Cycle Effects on the Near-Earth Space Systems

    DTIC Science & Technology

    1990-08-06

    foreign nationals. This technical report has been reviewed and is approved for publication. Publication of this report does not constitute Air Force...approval of the report’s findings or conclusions. It is published only for the exchange and stimulation of ideas. RAFAEL A. RIVIERE, Capt, USAF ONATHAN...M. EMHES , MAJ, USAF MOIE Project Officer MOIE Project Manager SSD/CNL AFSTC/WCO OL-AB UNCLASSIFIED SECURITY CLASSIFICATION OF THIS PAGE REPORT

  17. Credit USAF. Original housed in the Muroc Flight Test Base, ...

    Library of Congress Historic Buildings Survey, Historic Engineering Record, Historic Landscapes Survey

    Credit USAF. Original housed in the Muroc Flight Test Base, Unit History, 1 September 1942 - 30 June 1945. Alfred F. Simpson Historical Research Agency. United States Air Force. Maxwell AFB, Alabama. View captioned as "7 Sept 1945, BH-5 Base Ordinance Motor Repair Shop" with gas station and gasoline pump. View looks roughly northwest - Edwards Air Force Base, North Base, Motor Repair Shop T-16, Third & C Streets, Boron, Kern County, CA

  18. Credit USAF, 7 September 1945. Original housed in the Muroc ...

    Library of Congress Historic Buildings Survey, Historic Engineering Record, Historic Landscapes Survey

    Credit USAF, 7 September 1945. Original housed in the Muroc Flight Test Base, Unit History, 1 September 1942 - 30 June 1945. Alfred F. Simpson Historical Research Agency. United States Air Force. Maxwell AFB, Alabama. View of the mess hall, looking to the north. Sign over door reads "MFTB Muroc Flight Test Base Base Mess." - Edwards Air Force Base, North Base, Base Mess Hall T-27, Third Street, Boron, Kern County, CA

  19. 7. Credit USAF, 1945. Original housed in the Muroc Flight ...

    Library of Congress Historic Buildings Survey, Historic Engineering Record, Historic Landscapes Survey

    7. Credit USAF, 1945. Original housed in the Muroc Flight Test Base, Unit History, 1 September 1942 30 June 1945. Alfred F. Simpson Historical Research Agency. United States Air Force. Maxwell AFB, Alabama. Interior view in shop wing on south side of hangar. Original caption reads "7 Sept. 1945, BH-10, Hangar No. 4 4505 Machine Shop." - Edwards Air Force Base, North Base, Hangar, End of North Base Road, Boron, Kern County, CA

  20. PLC Hardware Discrimination using RF-DNA fingerprinting

    DTIC Science & Technology

    2014-06-19

    PLC HARDWARE DISCRIMINATION USING RF-DNA FINGERPRINTING THESIS Bradley C. Wright, Civilian, USAF AFIT-ENG-T-14-J-12 DEPARTMENT OF THE AIR FORCE AIR...protection in the United States. AFIT-ENG-T-14-J-12 PLC HARDWARE DISCRIMINATION USING RF-DNA FINGERPRINTING THESIS Presented to the Faculty Department...DISCRIMINATION USING RF-DNA FINGERPRINTING Bradley C. Wright, B.S.E.E. Civilian, USAF Approved: /signed/ Maj Samuel J. Stone, PhD (Chairman) /signed/ Michael A

  1. Experimental and Theoretical Basis for a Closed-Form Spectral BRDF Model

    DTIC Science & Technology

    2015-09-17

    EXPERIMENTAL AND THEORETICAL BASIS FOR A CLOSED-FORM SPECTRAL BRDF MODEL DISSERTATION Samuel D. Butler, Major, USAF AFIT-ENP-DS-15-S-021 DEPARTMENT...SPECTRAL BRDF MODEL DISSERTATION Presented to the Faculty Graduate School of Engineering and Management Air Force Institute of Technology Air University Air...FOR A CLOSED-FORM SPECTRAL BRDF MODEL DISSERTATION Samuel D. Butler, BS, MS Major, USAF Committee Membership: Michael A. Marciniak, PhD Chairman Kevin

  2. United States Air Force Statistical Digest, Fiscal Year 1965, Twentieth Edition

    DTIC Science & Technology

    1965-09-30

    prOVided by the USAF under Military Assistance Program . MAP EMPLOYEES - Category of civilian personnel engaged in activities reqUired in carrying out the...92 - USAF CIVIUAN EMPLOYEES IN SALARIED AND WAGE BOARD GROUPS EMPLOYED UNDER MILITARY ASSISTANCE PROGRAM (MAP), WORLO-WIDE, AT END OF QUARTER - FY...statistical material for tary Assistance Program (MAP), and re- the digest. AFCHO will furnish a chronology lated studies and historical events. of

  3. A Study of Benefits Resulting from the AFIT (Air Force Institute of Technology) Education with Industry Program

    DTIC Science & Technology

    1989-09-01

    A STUDY OF BENEFITS RESULTING FROM THE AFIT EDUCATION WITH INDUSTRY PROGRAM THESIS Ed R. Hernandez Captain, USAF AFIT/G SM/LSR/ 8 9S- 18_...RESULTING FROM THE AFIT EDUCATION WITH INDUSTRY PROGRAM THESIS Ed R. Hernandez Captain, USAF AFIT/GSM/LSR/89S-18 Approved for public release...5 Discussion .. ............. ........ 6 Education versus Training .. .. ............. 7 Concept of Learning .. .. ............... 10 Active Learning

  4. Airborne Operations in World War II, European Theater

    DTIC Science & Technology

    1956-09-01

    GARDEN Gee Hamilcar HANDS UP Formation usually composed of two or more elements and roughly equivalent to a squadron Forward Visual Control Post Ground...USAF HISTORICAL STUDIES: NO. 97 AIRBORNE OPERATIONS IN WORLD WAR II, EUROPEAN THEATER By Dr. John C. Warren USAF Historical Division Research Studies...OMB control number. 1. REPORT DATE SEP 1956 2. REPORT TYPE 3. DATES COVERED - 4. TITLE AND SUBTITLE Airborne Operations in World War II 5a

  5. USAF Flight Surgeon Survey: Aircrew Mental Health Referrals and Satisfaction with Local Mental Health Providers Response

    DTIC Science & Technology

    2008-05-01

    Autogenic training exercise; A treatment for airsickness in military pilots. International Journal of Aviation Psychology, 2005; 15(4): 395-412...flying during training , humanitarian, and operational missions can be extremely taxing. Flight surgeons often observe or hear of changes in the...health care is to ease and resolve the emotional or behavioral difficulties of an aviator while attempting to preserve a highly trained USAF asset

  6. Missions and Mobility Configurations for RED HORSE

    DTIC Science & Technology

    1988-04-01

    use in other research reports or educational pursuits contingent upon the following stipulations: - Reproduction rights do not extend to any copyrighted...MOBILITY CONFIGURATIONS FOR RED HORSE AUTHOR(S) MAJOR JAMES T. RYBURN, USAF FACULTY ADVISOR LT COL ROBERT L. PETERS, ACSC/3823 STUS SPONSOR COL ROBERT J...Classification) MISSIONS AND MOBILITY CONFIGURATIONS FOR RED HORSE 12. PERSONAL AUTHOR(S) Ryburn, James T., Maj or, USAF 13a. TYPE OF REPORT J13b. TIME

  7. Fibrinogen Recovery in Two Methods of Cryoprecipitate Preparation

    DTIC Science & Technology

    1989-08-01

    ERNEST A. HAYGOOD, 1st Lt, USAF Executive Officer, Civilian Institution Programs 17. COSATI CODES 18. SUBJECT TERMS (Continue on reverse if necessary...NAME OF RESPONSIBLE INDIVIDUAL 22b. TELEPHONE (Include Area Code) 22c. OFFICE SYMBOL ERNEST A. HAYGOOD, 1st Lt, USAF (513) 255-2259 AFIT/CI DDForm...u I iv ACKNOWLEDGEMENTS I would like to extend sincerest appreciation to Dr. Lloyd Lippert , my research advisor. Without his continued guidance

  8. Corrective lens use and refractive error among United States Air Force aircrew.

    PubMed

    Wright, Steve T; Ivan, Douglas J; Clark, Patrick J; Gooch, John M; Thompson, William

    2010-03-01

    Corrective lens use by military aviators is an important consideration in the design of head-mounted equipment. The United States Air Force (USAF) has periodically monitored lens use by aviators; however, it has been over a decade since the last study. We provide an update on the prevalence of corrective lenses and refractive error among USAF aircrew based on eyeglass orders processed through the Spectacle Request Transmission System (SRTS). Currently, 41% of active duty USAF pilots and 54% of other aircrew require corrective lenses to perform flight duties. Refractive errors are characterized by low to moderate levels of myopia with a mean spherical equivalent power of -1.01 diopters (D) for pilots and -1.68 D for others. Contact lenses, and more recently refractive surgery, reduce the number of aircrew that must rely on spectacles when flying; however, spectacle compatibility remains an important consideration in the cockpit.

  9. USAF bioenvironmental noise data handbook. Volume 157: KC-10A in-flight crew noise

    NASA Astrophysics Data System (ADS)

    Hille, H. K.

    1982-09-01

    The KC-10A is a standard USAF tanker-transport aircraft with high-speed, high altitude refueling and long range transport capability. This report provides measured data defining the bioacoustic environments at flight crew/passenger locations inside this helicopter during normal flight operations. Data are reported for 24 locations in a wide variety of physical and psychoacoustic measures: overall and band sound pressure levels, C-weighted and A-weighted sound levels, preferred speech interference level, perceived noise level, and limiting times for total daily exposure of personnel with and without standard Air Force ear protectors. Refer to Volume 1 of this handbook, USAF Bioenvironmental Noise Data Handbook, Vol. 1: Organization, Content and Application, AMRL-TR-75-50(1) 1975, for discussion of the objective and design of the handbook, the types of data presented, measurement procedures, instrumentation, data processing, definitions of quantities, symbols, equations, applications, limitations, etc.

  10. Roseau River Subbasin, Red River of the North Reconnaissance Report.

    DTIC Science & Technology

    1980-12-01

    river. It was found that much of the area was used -,- .for agricultural purposes (cropland and pasture). A narrow corridor € .of woodlands, sometimes... corridor through disturbed (e.g. cropland) areas. The forested areas afford habitats for a greater variety of wildlife than any other major habitat type in...listing as a Federally protected species (U.S. Army Corps of Engineers, 1975; U.S. Fish and Wildife Service, 1980; International Roseau River Engineering

  11. MOUNT JEFFERSON PRIMITIVE AREA, OREGON.

    USGS Publications Warehouse

    Walker, George W.; Pattee, Eldon C.

    1984-01-01

    Mineral and reconnaissance geothermal surveys of the Mount Jefferson Primitive Area in the Cascade Range of Oregon indicate little likelihood that metallic or nonmetallic mineral or energy resources exist in the area. Several mining claims, presumably located for gold, are present, but analyses of samples from the claims failed to detect the presence of gold or other valuable metals. Rock for construction purposes is abundantly present, but better and more accessible deposits are available in adjacent areas.

  12. Transforming Airborne Command and Control and Intelligence, Surveillance, and Reconnaissance

    DTIC Science & Technology

    2012-06-01

    launched once and remains on station at high altitude for many years. The ISIS airship loiters at very slow speeds, but it can relocate to any theater...operate at considerable altitudes are too high to permit adequate radar resolution for MTI purposes. Additionally, even with improved radar resolution...provides a capability analysis on the AWACS, JSTARS, RPAs, and unmanned airships to determine which systems can best meet these requirements in the future

  13. Lean principles and defense information technology acquisition: An investigation of the determinants of successful application

    NASA Astrophysics Data System (ADS)

    Haley, M.

    The purpose of this study was to investigate whether or not there have been successful applications of lean manufacturing principles in highly variable defense IT environments. Specifically, the study assessed if implementation of the lean philosophies by a defense organization yielded repeatable, predictable results in software release schedules reductions. Additionally, the study set out to determine what potential critical success factors (CSF's) were documented in the secondary data captured for each release, and extracted the variables used in the decision making for acceptability of fielding. In evaluating lean applicability to the high variability environment of USAF IT acquisitions, the research was conducted using non-experimental quantitative methods of archival secondary data. The sample for this case study was compiled from a USAF office that had implemented these techniques in pre-development, development and testing, and fielding phases. Based on the research data, acquisitionists and lean practitioners are inherently interconnected. Therefore, an understanding that critical success factors (CSFs) are integral to successful lean application in DoD IT acquisitions is crucial. Through a combination of synergistic alignments, plyometric CSFs were discovered to maximize the effects of each single CSF to produce rapid results in defense IT acquisitions. These include: (1) Enterprise Incorporation, (2) Team Trust, (3) Transformational Leadership, (4) Recursive Improvement, (5) Integrated Synergy, (6) Customer-Centric Culture and (7) Heuristic Communication.

  14. Evaluation of Corrective Action Team (CAT) Leader Training in Aeronautical Systems Division

    DTIC Science & Technology

    1991-09-01

    00A DI EVALUATION OF CORRECTIVE ACTION TEAM ( CAT ) LEADER TRAINING IN AERONAUTICAL SYSTEMS DIVISION CA THESIS Kirk J. Streitrater, Captain, USAF AFIT...EVALUATION OF CORRECTIVE ACTION TEAM ( CAT ) LEADER TRAINING IN AERONAUTICAL SYSTEMS DIVISION THESIS Kirk J. Streitmater, Captain, USAF AFIT/GSM/LSR/91S-25...8217, , C- s :C AFIT/GSM/LSR/91S-25 EVALUATION OF CORRECTIVE ACTION TEAM ( CAT ) LEADER TRAINING IN AERONAUTICAL SYSTEMS DIVISION THESIS Presented to the

  15. Proceedings of the USAF Logistics Capability Assessment Symposium LOGCAS 82 Held at USAF Academy, Colorado on 15-19 March 1982

    DTIC Science & Technology

    1982-05-01

    Ohio. General Merkling , fZ" and graduated from Hamilton High School, Los Angeles. He has a bachelor of science degree in mechanical engineering...navigation, navigation radar and doppler radar systems on bomber, cargo , fighter, and drone aircraft. He also performed duties as maintenance debriefer...measure supply support for those items. ihe model will also project future performance and provide a cost/support relationship. 11-13

  16. Dental Electric Handengines: Test and Evaluation.

    DTIC Science & Technology

    1985-04-01

    ADRD5 066 A DENTAL ELECTRIC HANDENGINES: TEST AND EVALUATION(U) j/ij SCHOOL OF AEROSPACE MEDICINE BROOKS AFB TX C D FOSTER ET AL. APR 85 USAFSAM-TR... DENTAL ELECTRIC HANDENGINES o Test and Evaluation In -- I Cad D. Foster, Major, USAF, DC Paul M. Callison, Master Sergeant, USAF Gerald F. McKinley...AFSC) Brooks Air Force Base, TX 78235-5301 85 7 15 057 NOTICES This final report was submitted by personnel of the Dental Investigation Service

  17. Dollar Summary of Federal Supply Classification and Service Category by Company, FY83, Part 4 (AA92-N063).

    DTIC Science & Technology

    1983-01-01

    INTEGRATED SYSTEMS ANALYSTS INC VIRGINIA NAVY RDTE/ELECTRONICS AND COMMUNICATION EQUIP 964 INTERACTIVE SYSTEMS INC MICHIGAN USAF ROTE/ELECTRONICS AND...HARD GOODS INTERACTIVE SYSTEMS INC COLORADO ARMY RDTE/MISCELLANEOUS HARD GOODS LITTON SYSTEMS INC NEW JERSEY NAVY RDTE/MISCELLANEOUS HARD GOODS I...DEFENSE 88 INTELLIGENT SY STATE TOTAL 114 INTERACTIVE TE CO CALIFORNIA ARMY RDTE/OTHER DEFENSE 201 INTERNATIONAL I NAVY ROTE/OTHER DEFENSE 778 USAF RDTE

  18. Experimental Validation Techniques for the Heleeos Off-Axis Laser Propagation Model

    DTIC Science & Technology

    2010-03-01

    EXPERIMENTAL VALIDATION TECHNIQUES FOR THE HELEEOS OFF-AXIS LASER PROPAGATION MODEL THESIS John Haiducek, 1st Lt, USAF AFIT/GAP/ENP/10-M07 DEPARTMENT...Department of Defense, or the United States Government. AFIT/GAP/ENP/10-M07 EXPERIMENTAL VALIDATION TECHNIQUES FOR THE HELEEOS OFF-AXIS LASER ...BS, Physics 1st Lt, USAF March 2010 APPROVED FOR PUBLIC RELEASE; DISTRIBUTION UNLIMITED. AFIT/GAP/ENP/10-M07 Abstract The High Energy Laser End-to-End

  19. The United States Air Force in Korea: A Chronology, 1950-1953

    DTIC Science & Technology

    2000-01-01

    War , the U.S. Air Force (USAF) Historian commissioned the Research Division, Air Force His- torical Research Agency (AFHRA), Maxwell Air Force Base...and aces. Finally, it attempts to summarize those USAF events in Korea that best illustrate the air war and the application of air power in the...sources, usually to confirm the most signifi- cant events of the air war in Korea. AFHRA historians or archivists who researched and wrote the monthly and

  20. Leadership in Crisis: Service Chiefs in the Post-Vietnam World

    DTIC Science & Technology

    2012-06-01

    the Korean War offered numerous lessons for the Army and USAF based on the effectiveness of interdiction and the need to coordinate with the ground ...roles and missions.100 Attack capability in this discussion is a platform’s ability to attack targets on the ground . Both USAF and Army leaders had...States Government; Record Group 11; National Archives , 7 August 1964). AU/SAASS/MILLS/AY12 72 of war.8 Soon after Johnson signed the resolution

  1. Golden Legacy, Boundless Future: Essays on the United States Air Force and the Rise of Aerospace Power

    DTIC Science & Technology

    2000-01-01

    tactical support, and, to a lesser extent, bom- bardment. The American Army had to digest quickly the crucial lesson already absorbed by the...2. United States Air Force Statistical Digest , 1947, Director of Statistical Services, Comptroller, HQ USAF, Washington, D.C., 1948, 15-16, 72, 132...Statistical Digest , Director of Statistical Services, Deputy Chief of Staff, Comptroller, HQ USAF, Washington, D.C., Nov 1952, 162-164. 6. Sarah A

  2. United States Air Force Summer Research Program -- 1993 Summer Research Program Final Reports. Volume 12. Armstrong Laboratory

    DTIC Science & Technology

    1993-01-01

    Panasonic TLD . Panasonic Industrial Company; Secaucus, New Jersey. 5. Thurlow, Ronald M. "Neutron Dosimetry Using a Panasonic Thermoluminescent Dosimeter." A...steps 8-12. 29-15 THE BUILDING OF THE USAF PANASONIC UD-809AS ALGORITHM Katherine M. Arnold Research Associate Radiation Dosimetry Branch Brooks Air...Research August 1993 30-1 THE BUILDING OF THE USAF PANASONIC UD-809AS ALGORITHM Katherine M. Arnold Research Associate Radiation Dosimetry Branch

  3. Book Analysis: Challenger: A Major Malfunction.

    DTIC Science & Technology

    1988-04-01

    REPORT NUMBER 88-113S TITLE BOOK ANALYSIS: CHALLENGER : A MAJOR MALFUNCTION AUTHOR(S) MAJOR THOMAS M. HALL, USAF FACULTY ADVISOR LT COL JOhN R. GRELLMAN... CHALLENGER : A MAJOR MALFUNCTION 12. PERSONAL AUTHOR(S) Hall, Thomas M., Major, USAF 13a. TYPE OF REPORT 13b. TIME COVERED 14. DATE OF REPORT (Year, Month...identify by block number) FIELD GROUP SUB-GROUP 19. ABSTRACT Continue on reverse if necessary and identify by block number) This report analyzes Challenger

  4. Developing Cyberspace Data Understanding: Using CRISP-DM for Host-based IDS Feature Mining

    DTIC Science & Technology

    2010-03-01

    Developing Cyberspace Data Understanding: Using CRISP - DM for Host-based IDS Feature Mining THESIS Joseph R. Erskine, Captain, USAF AFIT/GCS/ENG/10-01...Air Force, Department of Defense, or the United States Government. AFIT/GCS/ENG/10-01 Developing Cyberspace Data Understanding: Using CRISP - DM for...Developing Cyberspace Data Understanding: Using CRISP - DM for Host-based IDS Feature Mining Joseph R. Erskine, B.S.C.S. Captain, USAF Approved: /signed/ 12

  5. A Graphics Environment Supporting the Rapid Prototyping of Pictorial Cockpit Displays

    DTIC Science & Technology

    1986-12-01

    0 - niDi cO 3 FIL .OF I A GRAPHICS ENVIRONMENT SUPPORTING THE RAPID PROTOTYPING OF PICTORIAL COCKPIT DISPLAYS THESIS Alan J. Braaten Captain, USAF...COCKPIT DISPLAYS THESIS Alan J. Braaten Captain, USAF AFIT/GCS/IA/86D- 1 Appram:ed for public release; distribution unlimited AFIT/GCS/MA/80- 1 A...GRAPHICS ENVIROWNT SUPPORTING THE RAPID PROTOTYPING OF PICTORIAL COCKPIT DISPLAYS THESIS Preented to the Faculty Of the School of Engineering of the Air

  6. An Analysis of Factors Influencing the Turnover of United States Air Force Pilots in the Six to Eleven Year Group

    DTIC Science & Technology

    1980-06-01

    1979. 16. Donnelly, James H., Jr., James L. Gibson, and JohnM. Ivancevich . Organizations--Structure, Processes, Behavior. Dallas TX: Business...Publications, Inc., 1973. 17. Ivancevich , John M., Andrew D. Szilagyi, Jr., and Marc J. Wallace, Jr. Organizational Behavior and Performance. Santa Monica CA...215. 102 Lyons , Colonel Billy S., USAF, and Colonel KZjnald L. Marks, USAF. "An Alternate Pilot Management Pro- gram for Future Strategic Weapon

  7. MAKING THE WEASELS WILD AGAIN: ENSURING FUTURE AIR DOMINANCE THROUGH EFFECTIVE SEAD TRAINING

    DTIC Science & Technology

    2016-06-01

    both multi-mission design series (MMDS) and joint SEAD training as well as improve the capabilities of its electronic warfare (EW) ranges in order...USAF units to train for multi-mission design series (MMDS) SEAD operations.14 MMDS training includes the use of multiple USAF airborne platforms...not provided SEAD aircrews with either the quantity or quality of training required to conduct effective operations.2 At that time , Major Jon Norman

  8. An Assessment of Software Safety as Applied to the Department of Defense Software Development Process

    DTIC Science & Technology

    1992-12-01

    provide program 5 managers some level of confidence that their software will operate at an acceptable level of risk. A number of structured safety...safety within the constraints of operational effectiveness, schedule, and cost through timely application of system safety management and engineering...Master of Science in Software Systems Management Peter W. Colan, B.S.E. Robert W. Prouhet, B.S. Captain, USAF Captain, USAF December 1992 Approved for

  9. Centralized Contractor Operated Initial Flight Screening Program at Pueblo, Colorado

    DTIC Science & Technology

    2006-03-23

    TAXI = Private/Corporate Jets Source:USAF IFT Preliminary Noise Impact Assessment, 22 July 2005 Current activity at the private airfield at Fowler...Airport Land use Source:USAF IFT Preliminary Noise Impact Assessment, 22 July 2005 3.8 Transportation Pueblo Memorial Airport is served by United...pumpage per day in 2003: 23.567 million gallons per day • All time record Peak Day: 62,930,000 on July 16th, 1997 • Treatment plant capacity: 84

  10. Band Gap Transition Studies of U:ThO2 Using Cathodoluminescence

    DTIC Science & Technology

    2014-03-27

    BAND GAP TRANSITION STUDIES OF U:THO2 USING CATHODOLUMINESCENCE THESIS Joshua D. Reding , Second Lieutenant, USAF AFIT-ENP-14-M-31 DEPARTMENT OF THE...Education and Training Command in Partial Fulfillment of the Requirements for the Degree of Master of Science in Applied Physics Joshua D. Reding , B.S...STUDIES OF U:THO2 USING CATHODOLUMINESCENCE Joshua D. Reding , B.S. Second Lieutenant, USAF Approved: //signed// Robert L. Hengehold, PhD (Chair) //signed

  11. Credit USAF, ca. 1943. Original housed in the Muroc Flight ...

    Library of Congress Historic Buildings Survey, Historic Engineering Record, Historic Landscapes Survey

    Credit USAF, ca. 1943. Original housed in the Muroc Flight Test Base, Unit History, 1 September 1942 - 30 June 1945. Alfred F. Simpson Historical Research Agency. United States Air Force. Maxwell AFB, Alabama. Historic view looking north across southwest end of swimming pool as army personnel work on finishing the pool bottom. View looks towards Mess Hall (T-10) on Second Street - Edwards Air Force Base, North Base, Swimming Pool, Second Street, Boron, Kern County, CA

  12. USAF Dental Service Mercury Hygiene Report, Calendar Year 1980.

    DTIC Science & Technology

    1981-12-01

    the floor. Mercury Vapor Analyzer Used No. calibration No. of clinics Percent reported MV2 - Bacharach 81 67.5 14 Hopcalite tubes 8 6.7 Jerome model...instruments which could determine TWA: hopcalite tubes (8), Jerome with dosimeter coils (5), and 3M monitor (3). All 16 of these surveys showed mercury...vapor levels. This quantification requires sampling using the Jerome with a dosimeter coil, hopcalite tubes, or the 3M monitor. The USAF Occupational

  13. Installation Restoration Program. Phase 2. Confirmation Quantification. Stage 2 for MacDill Air Force Base, Florida. Volume 2

    DTIC Science & Technology

    1988-07-22

    Inc. of Savannah, Georgia and Tallahassee, Florida provided analytical services. Michael Newberry, Captain USAF, and Jeff Mason, 2d LT., USAF, from...2803-19 AG AP6 ST;- ES Ci eit 2803-20 A? APC S -2 ES 23033-23 AG .AF6 SD-S 2803-22 AC AP6 SD-4 E.> PARAMIETER 280u- .y 2&u r 23-2: 2803-22 Bezo (g.h.1

  14. Legal Issues for the Commander,

    DTIC Science & Technology

    1983-01-01

    Frederick T. Kiley, USAF Deputy Director, Plans and Programs Major William A. Buckingham, Jr., USAF Deputy Director, Administration Lieutenant (Junior...Writer-Editors Editorial Clerks Evelyn Lakes Pat Williams , Janis L. Hietala Lead Clerk Rebecca W. Miller Dorothy M. Mack Albert C. Helder Carol Valentine...9 M.J. 575 (A.F.C.M.R. 1980). 41 AL .. ~ ~. .~ ~ i 42 References 28. United States v. Poundstone , 22 U.S.C.M.A. 277, 46 C.M.R. 277 (1973). 29. United

  15. Epidemoligic Investigation of Health Effects in Air Force Personnel Following Exposure to Herbicides: Baseline Questionnaires

    DTIC Science & Technology

    1982-11-01

    19M I Prepared for: The Surgeon General ~, United States Air Force Washington, D.C. 20314 USAF SCHOOL OF AEROSPACE MEDICINE Brooks Air Force Base...School of Aerospace Medicine , Aerospace Medical Division, AFSC, Brooks Air Force Base, Texas, under job order 2767-00-01. la When Government drawings...Wolfe. Ljeujenant; Colonel, USAF. M C S F. IlFONMING ORGANIZATION NAMS AND AODRESS 10. PROGRAM ELEMENT. PROJECT, TASKUSAF School of Aerospace Medicine

  16. What’s Wrong with the Survivor Benefit Plan?

    DTIC Science & Technology

    1986-04-01

    Found aspects of the program confusing. Most often mentioned were the benefit adjustment mechanism and the special tax advantage Features. Not...WHAT’S WRONG WITH THE SURVIVOR BENEFIT PLAN? AUTHOR(S) MAJOR RALPH A. BLA1ELOCK, USAF FACULTY ADVISOR MAJOR MACK FOSTER, ACSC/EDCM SPONSOR LT COLONEL...Include.ecurslty Ckwaaicationl WHAT’S WRONG WITH THE SURVIVOR BENEFIT , PERSONAL AUTHORST Blakelock, ph A., Major, USAF 13a. TYPE OF REPORT 13t. TIME

  17. Student Modeling in an Intelligent Tutoring System

    DTIC Science & Technology

    1996-12-17

    Multi-Agent Architecture." Advances in Artificial Intelligence : Proceedings of the 12 th Brazilian Symposium on Aritificial Intelligence , edited by...STUDENT MODELING IN AN INTELLIGENT TUTORING SYSTEM THESIS Jeremy E. Thompson Captain, USAF AFIT/GCS/ENG/96D-27 DIMTVMON* fCKAJWINT A Appr"v*d t=i...Air Force Base, Ohio AFIT/GCS/ENG/96D-27 STUDENT MODELING IN AN INTELLIGENT TUTORING SYSTEM THESIS Jeremy E. Thompson Captain, USAF AFIT/GCS/ENG/96D

  18. Air Force Basing Strategies in the Western Pacific in Response to Chinese Military Buildup during Fiscal Austerity

    DTIC Science & Technology

    2016-02-01

    CHINESE MILITARY BUILDUP DURING FISCAL AUSTERITY by Timothy M. Swierzbin, Major, USAF A Research Report Submitted to the Faculty In Partial...future of USAF operations in the Asia-Pacific such as drastic military budget austerity and the state of Chinese aggression in the region...around the world to impart various levels of austerity to tackle their national debts. The U.S. was also susceptible to the crisis and the Government

  19. Acoustic Evaluation and Recommended Controls for Runway Supervisory Units, Laughlin AFB, Texas.

    DTIC Science & Technology

    1980-02-01

    NR ), given in Table 2 and shown in Figures 8 through 12 , are the arithmetic differences between exterior and interior noise levels. No difference...ORG. REPORT MUM4MR , ,IT]VPARINACCI, Capt, USAF- BSC Consultant, Acoustics Evaluation Engr CAROLYN M. JONES, 2LT USAF, BSC Consultant, Industria ...Documents.,") Block 12 . Report Date. Enter here the day, month, and year or month and year as shown on the cover, Block 13. Number of Pages. Enter

  20. Distributed Localization of Active Transmitters in a Wireless Sensor Network

    DTIC Science & Technology

    2012-03-01

    Distributed Localization of Active Transmitters in a Wireless Sensor Network THESIS Oba L. Vincent, 2nd Lieutenant, USAF AFIT/GE/ENG/12-41 DEPARTMENT...protection in the United States. AFIT/GE/ENG/12-41 Distributed Localization of Active Transmitters in a Wireless Sensor Network THESIS Presented to the...Transmitters in a Wireless Sensor Network Oba L. Vincent, B.S.E.E. 2nd Lieutenant, USAF Approved: /signed/ 29 Feb 2012 Maj. Mark D. Silvius, Ph.D. (Chairman

  1. The Challenge To Tactical Reconnaissance: Timeliness Through Technology

    NASA Astrophysics Data System (ADS)

    Stromfors, Richard D.

    1984-12-01

    As you have no doubt gathered from Mr. Henkel's introduction, I have spent over 20 years of my Air Force career involved in the reconnaissance mission either as a tactical reconnaissance pilot, as a tactical reconnaissance inspector, as a writer and speaker on that subject while attending the Air Force Professional Military Education Schools, and currently as the Air Force's operational manager for reconnaissance aircraft. In all of those positions, I've been challenged many times over with what appeared, at first, to be insurmountable problems that upon closer examination weren't irresolvable after all. All of these problems pale, however, when viewed side-by-side with the one challenge that has faced me since I began my military career and, in fact, faces all of us as I talk with you today. That one challenge is the problem of timeliness. Better put: "Getting information to our customers firstest with the mostest." Together we must develop better platforms and sensors to cure this age-old "Achilles heel" in the reconnaissance cycle. Despite all of our best intentions, despite all of the emerging technologies that will be available, and despite all of the dollars that we've thrown at research and development, we in the reconnaissance business still haven't done a good job in this area. We must do better.

  2. Speech and gesture interfaces for squad-level human-robot teaming

    NASA Astrophysics Data System (ADS)

    Harris, Jonathan; Barber, Daniel

    2014-06-01

    As the military increasingly adopts semi-autonomous unmanned systems for military operations, utilizing redundant and intuitive interfaces for communication between Soldiers and robots is vital to mission success. Currently, Soldiers use a common lexicon to verbally and visually communicate maneuvers between teammates. In order for robots to be seamlessly integrated within mixed-initiative teams, they must be able to understand this lexicon. Recent innovations in gaming platforms have led to advancements in speech and gesture recognition technologies, but the reliability of these technologies for enabling communication in human robot teaming is unclear. The purpose for the present study is to investigate the performance of Commercial-Off-The-Shelf (COTS) speech and gesture recognition tools in classifying a Squad Level Vocabulary (SLV) for a spatial navigation reconnaissance and surveillance task. The SLV for this study was based on findings from a survey conducted with Soldiers at Fort Benning, GA. The items of the survey focused on the communication between the Soldier and the robot, specifically in regards to verbally instructing them to execute reconnaissance and surveillance tasks. Resulting commands, identified from the survey, were then converted to equivalent arm and hand gestures, leveraging existing visual signals (e.g. U.S. Army Field Manual for Visual Signaling). A study was then run to test the ability of commercially available automated speech recognition technologies and a gesture recognition glove to classify these commands in a simulated intelligence, surveillance, and reconnaissance task. This paper presents classification accuracy of these devices for both speech and gesture modalities independently.

  3. Water-quality reconnaissance of the north Dade County solid-waste facility, Florida

    USGS Publications Warehouse

    McKenzie, D.J.

    1982-01-01

    A water-quality sampling reconnaissance of the north Dade County solid-waste disposal facility (landfill) near Carol City, Florida, was conducted during 1977-78. The purpose of the reconnaissance was to determine selected quality characteristics of the surface- and ground-water of the landfill and contiguous area; and to assess, generally, if leachate produced by the decomposition of landfill wastes was adversely impacting the downgradient water quality. Sampling results indicated that several water-quality characteristics were present in landfill ground water at significantly higher levels than in ground water upgradient or downgradient from the landfill. Moreover, many of these water-quality characteristics were found at slightly higher levels at down gradient site 5 than at upgradient site 1 which suggested that some downgradient movement of landfill leachate had occurred. For example, chloride and alkalinity in ground water had average concentrations of 20 and 290 mg/L at background wells (site 1), 144 and 610 mg/L at landfill wells (sites 2 and 4), and 29 and 338 mg/L at downgradient wells (site 5). A comparison of the 1977-78 sampling results with the National Primary and Secondary Drinking Water Regulations indicated that levels of iron and color in ground water of the study area frequently exceeded national maximum contaminant levels, dissolved solids, turbidity, lead, and manganese occasionally exceeded regulations. Concentrations of iron and levels of color and turbidity in some surface water samples also exceeded National maximum contaminant levels. (USGS)

  4. Meteorological Support Interface Control Working Group (MSICWG) Instrumentation, Data Format, and Networks Document

    NASA Technical Reports Server (NTRS)

    Brenton, James; Roberts, Barry C.

    2017-01-01

    The purpose of this document is to provide an overview of instrumentation discussed at the Meteorological Interface Control Working Group (MSICWG), a reference for data formats currently used by members of the group, a summary of proposed formats for future use by the group, an overview of the data networks of the group's members. This document will be updated as new systems are introduced, old systems are retired, and when the MSICWG community necessitates a change to the formats. The MSICWG consists of personnel from the National Aeronautics and Space Administration (NASA) Kennedy Space Center (KSC), NASA Marshall Space Flight Center (MSFC), NASA Johnson Space Center (JSC), National Oceanic and Atmospheric Administration National Weather Service Spaceflight Meteorology Group (SMG), and the United States Air Force (USAF) 45th Space Wing and Weather Squadron. The purpose of the group is to coordinate the distribution of weather related data to support NASA space launch related activities.

  5. Hurricane Imaging Radiometer (HIRAD) Observations of Brightness Temperatures and Ocean Surface Wind Speed and Rain Rate During NASA's GRIP and HS3 Campaigns

    NASA Technical Reports Server (NTRS)

    Miller, Timothy L.; James, M. W.; Roberts, J. B.; Jones, W. L.; Biswas, S.; Ruf, C. S.; Uhlhorn, E. W.; Atlas, R.; Black, P.; Albers, C.

    2012-01-01

    HIRAD flew on high-altitude aircraft over Earl and Karl during NASA s GRIP (Genesis and Rapid Intensification Processes) campaign in August - September of 2010, and plans to fly over Atlantic tropical cyclones in September of 2012 as part of the Hurricane and Severe Storm Sentinel (HS3) mission. HIRAD is a new C-band radiometer using a synthetic thinned array radiometer (STAR) technology to obtain spatial resolution of approximately 2 km, out to roughly 30 km each side of nadir. By obtaining measurements of emissions at 4, 5, 6, and 6.6 GHz, observations of ocean surface wind speed and rain rate can be retrieved. The physical retrieval technique has been used for many years by precursor instruments, including the Stepped Frequency Microwave Radiometer (SFMR), which has been flying on the NOAA and USAF hurricane reconnaissance aircraft for several years to obtain observations within a single footprint at nadir angle. Results from the flights during the GRIP and HS3 campaigns will be shown, including images of brightness temperatures, wind speed, and rain rate. Comparisons will be made with observations from other instruments on the campaigns, for which HIRAD observations are either directly comparable or are complementary. Features such as storm eye and eye-wall, location of storm wind and rain maxima, and indications of dynamical features such as the merging of a weaker outer wind/rain maximum with the main vortex may be seen in the data. Potential impacts on operational ocean surface wind analyses and on numerical weather forecasts will also be discussed.

  6. Observations of C-band Brightness Temperatures and Ocean Surface Wind Speed and Rain Rate from the Hurricane Imaging Radiometer (HIRAD)

    NASA Technical Reports Server (NTRS)

    Miller, Timothy L.; James, M. W.; Roberts, J. B.; Jones, W. L.; May, C.; Ruf, C. S.; Uhlhorn, E. W.; Atlas, R.; Black, P.

    2012-01-01

    HIRAD flew on the WB-57 over Earl and Karl during NASA s GRIP (Genesis and Rapid Intensification Processes) campaign in August - September of 2010. HIRAD is a new Cband radiometer using a synthetic thinned array radiometer (STAR) technology to obtain cross-track resolution of approximately 3 degrees, out to approximately 60 degrees to each side of nadir. (The resulting swath width for a platform at 60,000 feet is roughly 60 km, and resolution for most of the swath is around 2 km.) By obtaining measurements of emissions at 4, 5, 6, and 6.6 GHz, observations of ocean surface wind speed and rain rate can be retrieved. This technique has been used for many years by precursor instruments, including the Stepped Frequency Microwave Radiometer (SFMR), which has been flying on the NOAA and USAF hurricane reconnaissance aircraft for several years to obtain observations within a single footprint at nadir angle. Results from the flights during the GRIP campaign will be shown, including images of brightness temperatures, wind speed, and rain rate. Comparisons will be made with observations from other instruments on the GRIP campaign, for which HIRAD observations are either directly comparable or are complementary. Features such as storm eye and eyewall, location of storm wind and rain maxima, and indications of dynamical features such as the merging of a weaker outer wind/rain maximum with the main vortex may be seen in the data. Potential impacts on operational ocean surface wind analyses and on numerical weather forecasts will also be discussed.

  7. Observations During GRIP from HIRAD: Images of C-Band Brightness Temperatures and Ocean Surface Wind Speed and Rain Rate

    NASA Technical Reports Server (NTRS)

    Miller, Timothy L.; James, M. W.; Jones, W. L.; Ruf, C. S.; Uhlhorn, E. W.; Biswas, S.; May, C.; Shah, G.; Black, P.; Buckley, C. D.

    2012-01-01

    HIRAD (Hurricane Imaging Radiometer) flew on the WB-57 during NASA s GRIP (Genesis and Rapid Intensification Processes) campaign in August - September of 2010. HIRAD is a new C-band radiometer using a synthetic thinned array radiometer (STAR) technology to obtain cross-track resolution of approximately 3 degrees, out to approximately 60 degrees to each side of nadir. By obtaining measurements of emissions at 4, 5, 6, and 6.6 GHz, observations of ocean surface wind speed and rain rate can be inferred. This technique has been used for many years by precursor instruments, including the Stepped Frequency Microwave Radiometer (SFMR), which has been flying on the NOAA and USAF hurricane reconnaissance aircraft for several years. The advantage of HIRAD over SFMR is that HIRAD can observe a +/- 60-degree swath, rather than a single footprint at nadir angle. Results from the flights during the GRIP campaign will be shown, including images of brightness temperatures, wind speed, and rain rate. To the extent possible, comparisons will be made with observations from other instruments on the GRIP campaign, for which HIRAD observations are either directly comparable or are complementary. Features such as storm eye and eyewall, location of vortex wind and rain maxima, and indications of dynamical features such as the merging of a weaker outer wind/rain maximum with the main vortex may be seen in the data. Potential impacts on operational ocean surface wind analyses and on numerical weather forecasts will also be discussed.

  8. Transforming Mechanized Reconnaissance: How the Armored Brigade Combat Team (ABCT) Cavalry Squadron Should be Structured for Reconnaissance and Security Operations in the Near Future

    DTIC Science & Technology

    2014-06-13

    Squadron ( BFV /HMMWV, Current) .................................................. 93 Description...Evaluation Criteria ........................................................ 106 Comparison to Validation Criteria: ABCT Cavalry Squadron ( BFV /HMMWV...Brigade Combat Team BFV Bradley Fighting Vehicle BRT Brigade Reconnaissance Troop CAB Combined Arms Battalion CFV Cavalry Fighting Vehicle FM

  9. Study on the shipboard radar reconnaissance equipment azimuth benchmark method

    NASA Astrophysics Data System (ADS)

    Liu, Zhenxing; Jiang, Ning; Ma, Qian; Liu, Songtao; Wang, Longtao

    2015-10-01

    The future naval battle will take place in a complex electromagnetic environment. Therefore, seizing the electromagnetic superiority has become the major actions of the navy. Radar reconnaissance equipment is an important part of the system to obtain and master battlefield electromagnetic radiation source information. Azimuth measurement function is one of the main function radar reconnaissance equipments. Whether the accuracy of direction finding meets the requirements, determines the vessels successful or not active jamming, passive jamming, guided missile attack and other combat missions, having a direct bearing on the vessels combat capabilities . How to test the performance of radar reconnaissance equipment, while affecting the task as little as possible is a problem. This paper, based on radar signal simulator and GPS positioning equipment, researches and experiments on one new method, which povides the azimuth benchmark required by the direction-finding precision test anytime anywhere, for the ships at jetty to test radar reconnaissance equipment performance in direction-finding. It provides a powerful means for the naval radar reconnaissance equipments daily maintenance and repair work[1].

  10. Reconnaissance Of The Year 2000 And Beyond

    NASA Astrophysics Data System (ADS)

    Dresser, M. M.

    1981-12-01

    The reconnaissance systems of the year 2000 and beyond may be merely an extension of current technology or may utilize bold new technology and concepts still in the embryonic stages. The five basic reconnaissance mission stages: collection, processing, interpretation, reporting, and dissemination, are reviewed in terms of the potential application of new and emerging technology such as high density multispectral focal plane arrays, new radar techniques, VLSI/VHSIC computational resources, artificial intelligence, multisensor integration, pattern and target recognition, image compression, advanced display and targeting techniques, and even new fields not thought of as exact sciences today. The application of these technologies is viewed in the context of the reconnaissance missions: targeting, damage assessment, order of battle assessment, terrain evaluation and planning. The traditional neeos for varying levels of detail and timeliness of reconnaissance data are shown to be largely removed by the use of the most advanced and highest development risk systems. Lower development risk systems show excellent capabilities with the potential for high capability at low cost. New fields may totally change or even eliminate reconnaissance as we know it today.

  11. The United States Air Force and the Culture of Innovation, 1945-1965

    DTIC Science & Technology

    2002-01-01

    US Dept of Transportation; typically they hover between 85 and 95 percent. 16. Kent C. Redmond and Thomas M. Smith, Project Whirlwind: A Case Histo...Washing- ton, D.C.: AF Hist and Museums Prog, 1994). 14. Thomas A . Sturm, The USAF SAB: Its First Twenty Years 1944–1964 (Washington, D.C.: USAF...allegations at Ramo-Wooldridge and the Air Force’s approach. Schriever answered them in a letter to Lt. Gen. Thomas Power, the commander of ARDC, in

  12. The Death of Superman: The Case Against Specialized Tanker Aircraft in the USAF

    DTIC Science & Technology

    2002-06-01

    tanker and receiver aircraft were de Havilland DH -4Bs. The DH -4B was a single engine biplane with a gross weight of 3,557 pounds. Its cruising speed...including transport, air ambulance, photographic plane, trainer, target tug, forest fire patroller, and air racer. “De Havilland DH -4: Air Service... Havilland DH -4: Air Service Workhorse.” USAF Museum, WPAFB. On-line. Internet, 6 June 2002. Available from http://www.wpafb.af.mil/ museum

  13. Status Report on Medical Materiel Items Tested and Evaluated for Use in the USAF Aeromedical Evacuation System

    DTIC Science & Technology

    1990-12-01

    Volumetric Infusion Pump is conditionally acceptable for use. The Air -In- Line detector does not sense air bubbles 0.95 cm (3/8 inch) or smaller...been fitted with an improved brushless air circulation motor, Brailsford model T- 2NFR. Using the new motor, the 185 passed EMI and is acceptable for...USAF School of Aerospace Medicine, Human Systems Division, Air Force Systems Command, Brooks Air Force Base, Texas, under job order 7930-16- 12. This

  14. An Annotated Bibliography of Hypobaric Decompression Sickness Research Conducted at the Crew Technology Division, USAF School of Aerospace Medicine, Brooks AFB, Texas from 1983 to 1988

    DTIC Science & Technology

    1990-06-01

    AN ANNOTATED BIBLIOGRAPHY OF HYPOBARIC DECOMPRESSION SICKNESS RESEARCH CONDUCTED AT THE CREW TECHNOLOGY DIVISION, USAF SCHOOL OF AEROSPACE MEDICINE...190 man-flights to four selected altitudes (30000, 27500, 25000, and 22500 ft pressure equivalent) in a hypobaric chamber. The subjects’ ages ranged...conditions and two of these developed delayed sy~rtcms. Three of these five subjects underwent hyperbaric oxygen treatment. Conclusion. Female subjects

  15. Report of the Defense Science Board Task Force on Tactical Battlefield Communications,

    DTIC Science & Technology

    2000-02-01

    Communications, in and Intelligence (ASD/C3I); and LTG John Woodward, J6. The Task Force comprised fourteen experts from government, industry, and academe. The...O’Berry (USAF-Retired) Col Bobby Smart (USAF) Professor Stewart Personick Mr. Mark Rich Mr. Peter D. Steensma DSB Staff Assistant Mr. John ...were: The Honorable Dr. Jacques Gansler, USD/AT&L, the Honorable Art Money, ASD/C3I and LTG John Woodward, JCS-J6. The Task Force membership (Figure

  16. 6. Credit USAF, ca. 1947. Original housed in the Photograph ...

    Library of Congress Historic Buildings Survey, Historic Engineering Record, Historic Landscapes Survey

    6. Credit USAF, ca. 1947. Original housed in the Photograph Files, AFFTC/HO, Edwards AFB, California. Interior of Building 4401 (or possibly 4402) looking east at hangar doors with a North American Aviation XB-45 Tornado jet aircraft in the foreground. This view illustrates why the series of sliding doors and wide, high interior clearances were necessary to accommodate large aircraft. Note configuration of wooden trusses supporting the roof. - Edwards Air Force Base, North Base, Hangar No. 1, First & B Streets, Boron, Kern County, CA

  17. Development and Implementation of a Comprehensive Risk Management Program at the USAF Academy Hospital, USAF Academy, Colorado

    DTIC Science & Technology

    1980-04-01

    injuries annually of which some 700,000 appeared to involve some form of medically negligent conduct. 6 Similarly, the number of malpractice claims brought...only three (3) claims of medical malpractice were filed against the Air Force. That same year, a total of $12(!) was paid by the Air Force in...1976.26 The department of Health, Education and Welfare’s Commission on Medical Malpractice estimated that 12,000 medical malpractice claims 27 were filed

  18. Total Quality Management in the Department of Defense

    DTIC Science & Technology

    1989-09-01

    DTI ELECT SDu TOTAL QUALITY MANAGEMENT IN THE DEPARTMENT OF DEFENSE THESIS BRUCE E. SPRINGS, B.S. CAPTAIN, USAF AFIT/GLN/LSR/ 89S -57 I1- DEPARTMENT...13 0 3 AFIT/GLM/LSR/89S-57 TOTAL QUALITY MANAGEMENT IN THE DEPARTMENT OF DEFENSE THESIS BRUCE E. SPRINGS, B.S. CAPTAIN, USAF AFIT/GLH/LSR/89S-57...Defense. # AFIT/GLM/LSR/89S-57 TOTAL QUALITY MANAGEMENT IN THE DEPARTMENT OF DEFENSE THESIS Presented to the Faculty of the School of Systems and Logistics

  19. Project CHECO Southeast Asia Report. Forward Airfields for Tactical Airlift in SEA

    DTIC Science & Technology

    1970-06-15

    publications, this is an authen- tic s-sment of the effectiveness of USAF airpower in PACOM. ef /o a , Major General, USAF I/ m i ii l UNCLASSIFIED...Australian Air Force (RAAF) crews were airborne 35,569 times in 1969, with cargo that ranged from troops to chickens, cement , rice, ammunition, cattle...Runway surfaces--clay, laterite , limestone, light steel matting (M8Al), or sod, depending on the aircraft involved-- were expected to sustain 700 traffic

  20. Randolph AFB, San Antonio, Texas. Revised Uniform Summary of Surface Weather Observations (RUSSWO)

    DTIC Science & Technology

    1976-03-19

    FoRM ARE oUsoIII ’, " ’ . . . " " -,, ’:,,,:t."," *4 -- ".°" "- . . . " ’ * "- : ; Ir , ( DATA PROCESSING BRANCH EtAC/USAF SURFACE WINDS AIR" WATHER ...FORM ARI OS$Oitlt_ ___ _zT z __ __ ___......- ___ _ _ _ .4. .. . II DATA PROCESSIN G BRASFCH FTAC/USAF SURFACE WINDS AiR WATHER SERVICE/MAC PERCENTAGE...SURFACE WINDS 1 A/R WATHER SERVICE/MAC PERCENTAGE FREQUENCY OF WIND DIRECTION AND SPEED (FROM HOURLY OBSERVATIONS) ( 12911- RANDOLPH AFBJTEXAS/SAN

  1. Engineering Test and Evaluation During High G. Volume III, Anti-G Suits.

    DTIC Science & Technology

    1978-06-01

    items are: 3 inservice units from USAF and IJSN; an RAF unit; and 2 experimental units (lower body full pressure, and capstan). The study of the capstan...inspections are performed by life-support techni- cians whose training and expertise best enable them to evaluate the anti-G suit condition. The TEHG...of testing in one minute." At some installations this test has been waived by USAF Air Training Command (ATC) to "l psig drop from 5 psig in 20 sec

  2. Development and Implementation of a Comprehensive Risk Management Program at the USAF Academy Hospital.

    DTIC Science & Technology

    1980-04-01

    much less con - cerned about malpractice problems. As a result of the program, they began to view the risk management program as their own and to recog...that con - tributes to better patient care. 131 Implementing Risk Management According to Donovan and Bader, an action plan for the systems approach might...Al87 344 DEVELOPMENT AND IMPLEMENTATION OF A COMPREHENSIVE RISK 1 MANAGEMENT PROGRAM AT THE USAF ACADEMY HOSPITAL(U) ARMY HEALTH CARE STUDIES AND

  3. A Study to Determine Patient Waiting Time at the Outpatient Pharmacy at Wilford Hall USAF Medical Center

    DTIC Science & Technology

    1988-06-01

    at Wilford Hall USAF Medical Center significantly reduced the patient wait time at the main outpatient pharmacy. Satellite pharmacies have been ).’l...PRESENTING TO WINDOW 1, 19 MAR 88. 47 C:. A’.’E-:A: -ESCRIRTIONS PER PATIENT ...........48 H. WILFORD HALL MEDICAL CENTER OUTPATIENT QUESTIONNAIRE...that wait times at tne outpatient pharmacy were excessive. It was this concern that motivated the Medical Center Administrator to request that patient

  4. The ’Irreversibility’ of Israel’s Annexation of the West Bank and Gaza Strip: A Critical Evaluation.

    DTIC Science & Technology

    1985-10-01

    to the West Bank - 22 - and Gaza Strip warrant the conclusion that political initiatives based on the presumption that Israeli withdrawal is feasible...with the possible and important exception of East Jerusalem, the second, psycho-cultural threshold, has not yet been crossed. An ingrained presumption ...HQ USAF/IN Washington, D.C. 20330 AFSAC/ INOC Fort Belvoir, VA 22060-5788 Commandant USAF Academy Colorado Springs, CO 80914 AFIS/DPT Fort Belvoir, VA

  5. Retaining U.S. Air Force Pilots When the Civilian Demand for Pilots Is Growing

    DTIC Science & Technology

    2016-01-01

    pilot retention and determine the changes in ARP and AP that could offset those effects. It also simulates the effects of eliminating AP for pilots...array of compensation policies for pilots, thereby providing the USAF with an empirically based analytical platform to determine the special and...greatly from the input and support of our project monitor, Maj Ryan Theiss, Chief, Rated Force Policy-Mobility Forces (HQ USAF/A1PPR), as well as Lt

  6. Refrigeration and Cryogenics Career Ladder, AFSc 54530, 54550, and 54570.

    DTIC Science & Technology

    1983-07-01

    STATES AIR FORCE D cl e 00l REFRIGERATION AND CRYOGENICS CAREER LADDER AFSCs 54530, 54550, AND 54570 AFPT 90-545-461 JULY 1983 ,-. 71983 - OCCUPATIONAL...been reviewed and is approved. PAUL T. RINGENBACH, Colonel, USAF WALTER E . DRISKILL, Ph.D. Commander Chief, Occupational Analysis Branch USAF...ASSIGNED SAMPLE AIRMAN 35 35 E -4 22 23 E -5 27 26 E -6 11 12 E -7 5 4 E -8 * E -9 * TOTALS 100 100 DENOTES LESS THAN ONE PERCENT TABLE 3 TAFHS

  7. 9. Credit USAF, ca. 1945. Original housed in the Muroc ...

    Library of Congress Historic Buildings Survey, Historic Engineering Record, Historic Landscapes Survey

    9. Credit USAF, ca. 1945. Original housed in the Muroc Flight Test Base, Unit History, 1 September 1942 - 30 June 1945. Alfred F. Simpson Historical Research Agency. United States Air Force. Maxwell AFB, Alabama. View of concrete base and brackets of jet engine rotor balancing machine. Location where photograph was taken not determined, but presumed to be in shops of Building 4505. - Edwards Air Force Base, North Base, Hangar, End of North Base Road, Boron, Kern County, CA

  8. 8. Credit USAF, ca. 1945. Original housed in the Muroc ...

    Library of Congress Historic Buildings Survey, Historic Engineering Record, Historic Landscapes Survey

    8. Credit USAF, ca. 1945. Original housed in the Muroc Flight Test Base, Unit History, 1 September 1942 - 30 June 1945. Alfred F. Simpson Historical Research Agency. United States Air Force. Maxwell AFB, Alabama. View of concrete base for jet engine rotor balancing machine. Location where photograph was taken not determined, but presumed to be in shops of Building 4505 which had a sizeable machine shop. - Edwards Air Force Base, North Base, Hangar, End of North Base Road, Boron, Kern County, CA

  9. Analysis of Minuteman Missile Crew Member Attitudes Toward Present Minuteman Education Program and Possible Alternatives.

    DTIC Science & Technology

    1980-06-01

    TO0WARD PRESLT NUE N - DUCATION PROGRADF AND T0SMBLE 6. PERFORMING GIG. 0114:00RT NUMneRt 11. CONTRACT ORt GRANT NuUSERf(s1 t~ Donald L. i emp Captain...USAF, M4SC *Andrew T.//Rybacr Captain, USAF 9. PERFORMING ORGANIZATION NAME AND AOORES~r10 PROGRAM ELEMENT. PROJECT. TASK School of Systems and...106 38. MMEP IMPROVES DUTY PERFORMANCE (X2 One Sample Test) .. .......... . 107 39. MMEP IMPROVES DUTY PERFORMANCE (Questionnaire Data

  10. Is the USAF Officer Corps a Fighting Force?

    DTIC Science & Technology

    1988-05-01

    quottin)j analysis, and operational audit . Following work moasurent and 14 computAtions, th., standards 4uro staffed and approved by NQ USAF *rnl...occupation group in the Air Force. 9 Most recently# Senator John Glenn has asked the GAO to conduct an audit of pilot requirements.1 9 This information...AlIocdtion System," Air Force Times, 14 September 1987, p. 6. 9. Pat )alton, " Audit Pilot Requirements, Glenn Asks GAO," Air Forte Times, 18 January 1988

  11. Mission Emphasis and the Determination of Needs for New Weapon Systems

    DTIC Science & Technology

    2009-05-01

    Loveland, CO: Prosci, 2006). 61. Richard R. Nelson and Sidney G. Winter, An Evolutionary Theory of Economic Change (Cambridge, MA: The Belknap Press...of Gen Hunter Harris, USAF, (Ret.), by Col John E. Van Duyn and Maj Richard B. Clement, 7 July 1971. Typed transcript p. 32, K239.0512-403 Iris No...C. Jones, USAF, (Ret.) by Dr. Lt Col Maurice Maryanow and Dr. Richard H. Kohn, 5 August, 15-17 October 1985; 20-21 January, 13-14 March 1986

  12. Practical Applications of Math and Science in Junior High Schools

    DTIC Science & Technology

    1984-04-01

    APPLICATIONS OF MATH AND SCIENCE IN JUNIOR HIGH SCHOOLS AUTHOR(S) MAJOR LAWRENCE N. HYLAND, USAF FACULTY ADVISOR mAJoR JAMM WILSON, ACSC/EDDP SPONSOR LT COL...JUNIOR HIGH SCHOOLS 6 PERFORMING O1G. REPORT NUMBER "ś, Au THORrs) 8. CON’RACT OR GRANT NUMBER(.,) Lawrence N. Hyland, Major, USAF 9. PERFORMING...materials aimed at the jumior high school level. Material exposes target group to the mathematical and scientific skills required of Air Force

  13. Desert Express: An Analysis on Improved Customer Service

    DTIC Science & Technology

    1991-09-01

    Nt MARQ 3,199 Of. DESERT EXPRESS: AN ANALYSIS ON IMPROVED CUSTOMER SERVICE THESIS Thomas C Thaiheim, Majo-,r USAF AFTT/GLM/LSM,/91S-64 ?Z; W...Astq vt.: tyc a l AFIT/GLM/,LSM/91S-64 DESERT EXPRESS: AN ANALYSIS ON IMPROVED CUSTOMER SERVICE THESIS Thomas C. Thalheim, Major, USAF AFIT/GLM/LSM...91S-64 Approved for public release; distribution unlimited AFIT/GLM/LSM/91S-64 DESERT EXPRESS: AN ANALYSIS ON IMPROVED CUSTOMER SERVICE THESIS

  14. Air & Space Power Journal. Volume 22, Number 1, Spring 2008

    DTIC Science & Technology

    2008-01-01

    Braganca, USAF Naval Air Station Patuxent River, Maryland Dr. Kendall K. Brown NASA Marshall Space Flight Center Col Steven D. Carey, USAF...bunch of ‘Bs’ I’ve ever heard of.” At first there was no reaction to my remarks, but then the entire room erupted in shouts and cheers! All I had...present itself. Being in Our Profession Is All about Service to Others I am reminded of the photograph of the chief master sergeant stationed in Iraq

  15. Effect of Prior Exposure at Elevated Temperatures on Tensile Properties and Stress-Strain Behavior of Three Oxide/Oxide Ceramic Matrix Composites

    DTIC Science & Technology

    2015-03-26

    OF THREE OXIDE/OXIDE CERAMIC MATRIX COMPOSITES THESIS Christopher J. Hull, Captain, USAF AFIT- ENY -MS-15-M-228 DEPARTMENT OF THE AIR FORCE...Government and is not subject to copyright protection in the United States. AFIT- ENY -MS-15-M-228 EFFECT OF PRIOR EXPOSURE AT ELEVATED TEMPERATURES ON...BS Captain, USAF March 2015 DISTRIBUTION STATEMENT A: APPROVED FOR PUBLIC RELEASE; DISTRIBUTION UNLIMITED AFIT- ENY - MS-15-M-228 EFFECT OF

  16. Fatigue and Workload in Four-Man C-5A Cockpit Crews (Volant Galaxy).

    DTIC Science & Technology

    1980-08-01

    AD-AO91. 1.9 SCI400L OF AEROSPACE MEDICINE BROOKS AFB TX F/6 S/9 FATIGUE AND WORKLOAD ZN FOUR-NAN C-SA COCKPIT CREWS (VOLANT *AL--ETC(U$ AUG 80 W F...release; distribution unlimited. USAF SCHOOL OF ALROSPACE MEDICINE Aerospace Medical Division (AFSC) Brooks Air Force Base, Texas 78235 81 2 NOTICES...This final report was submitted by personnel of the Crew Performance Branch, Crew Technology Division, USAF School of Aerospace Medicine , Aerospace

  17. Project CHECO Southeast Asia Report. USAF Search and Rescue in Southeast Asia, 1 July 1969 - 31 December 1970

    DTIC Science & Technology

    1971-04-23

    airpower to meet a multitude of requirements. The varied applications of airpower have involved the full spectrum of USAF aerospace vehicles, support...shield of the sky proper, a sphere azure , rimmed and gridded or, superimposed in the southwest areas of the sphere a cross and three lightning bolt...Plan 69-1 to provide two full squadrons of HH-53 Super Jolly Greens or BUFFs as they were known in SEA--for Big Ugly Friendly Fellows, as one

  18. Practical question-and-answer guide on VDTS (video display terminals) for BEES (base bioenvironmental engineer). Final report

    DOE Office of Scientific and Technical Information (OSTI.GOV)

    Olson, B.M.

    1985-01-01

    The USAF OEHL conducted an extensive literature review of Video Display Terminals (VDTs) and the health problems commonly associated with them. The report is presented in a question-and-answer format in an attempt to paraphrase the most commonly asked questions about VDTs that are forwarded to USAF OEHL/RZN. The questions and answers have been divided into several topic areas: Ionizing Radiation; Nonionizing Radiation; Optical Radiation; Ultrasound; Static Electricity; Health Complaints/Ergonomics; Pregnancy.

  19. Project CHECO Southeast Asia Report. USAF Civic Action in Thailand

    DTIC Science & Technology

    1969-03-22

    SECOND CLASS HEALTH CENTERS MIDWIFERY CENTER MOBILE MEDICAL TEAMS , I SPECIAL 7AF/l3AF FORCES I I I I t I i ! L------·-. 56 ACW -t I i 1 I i...direct treatment of patients by U.S. personnel and the wide variety of drugs offered by the Americans were considered to be contrary to the stated...while diminishing the sophistication 10/ of drugs .-- The variety of drugs supplied by the USAF created a dual problem: (1) Thai resources were

  20. Demographic Shifts in the United States Air Force: 1994-2007

    DTIC Science & Technology

    2008-02-15

    experience includes F-15C, F-15E, A-10, F-16, RC-135, RQ-4 “Global Hawk”, MQ-9 “Predator” and U-2. He is married to the former Deanna Pacansky of...manpower is relied upon to keep this operational tempo, the retention of personnel in whom the USAF invested heavily through training and equipping will...continue to examine the demographics of both the US and USAF population to be alert to possible changes as they affect recruitment, retention , and

  1. Defense AT&L (Volume 36, Number 2, March-April 2007)

    DTIC Science & Technology

    2007-04-01

    87 28 The Pursuit of Courage, Judg- ment, and Luck Maj. Dan Ward, USAF Maj. Chris Quaid, USAF Conventional wisdom states that a closed risk is a good...example) that could be as much as 50 percent dirt. Many agencies were buying adobe bricks that were not kiln -fired, so within two or three seasons of...all too many PMs think a good risk management process simply identifies and mitigates the bad things that can happen. Conventional risk manage- ment

  2. Testing and Evaluation of the Bear Medical Systems, Inc. Bear 33 Volume Ventilator System

    DTIC Science & Technology

    1990-12-01

    approved for publication. RICHARD J. KNECHT, Lt Col, USAF, NC ROGER L STORK , Col, USAF, BSC Project Scientist Chief, Crew Systems Branch EORCHENDER...no problems. After the vibration tests, a visual inspection of the humidifier revealed that a screw and metal clip from a terminal on the incoming...hexagonal J-bolt nuts, which secure the sled to the litter, with larger wing nuts. This modification will allow the sled to be adequately secured by

  3. Testing and Evaluation of the International Biomedical Inc. Neonatal Transport System.

    DTIC Science & Technology

    1990-12-01

    nationals. This report has been reviewed and is approved for publication. RICHARD J. KNECHT, Lt Col, USAF, NC ROGER L. STORK , Colonel, USAF, BSC Project...required by the 375th Aeromedical Airlift Wing surgeon (375 AAW/SG); a process that can consume precious time. (NOTE: The 375 AAW was later redesignated...the 375th Military Airlift Wing , and the SG components were integrated with HQ MAC/SG.) The life and death nature of most newborn referrals to Level

  4. Project CHECO Southeast Asia Report. USAF Civic Action in Republic of Vietnam

    DTIC Science & Technology

    1968-04-01

    peace in SEA." 1 The Commander, 7AF, told his staff the "capabilities and energies of the USAF would be used to implement a positive Civic Action...Civic Action Division took the position that Community Relations was not a function of a Military Civic Action Program and properly belonged in the...considered an assignment of convenience, since the position more properly called for a Special Air Warfare Officer, AFSC 0316. Efforts were being made to

  5. Sensor Control And Film Annotation For Long Range, Standoff Reconnaissance

    NASA Astrophysics Data System (ADS)

    Schmidt, Thomas G.; Peters, Owen L.; Post, Lawrence H.

    1984-12-01

    This paper describes a Reconnaissance Data Annotation System that incorporates off-the-shelf technology and system designs providing a high degree of adaptability and interoperability to satisfy future reconnaissance data requirements. The history of data annotation for reconnaissance is reviewed in order to provide the base from which future developments can be assessed and technical risks minimized. The system described will accommodate new developments in recording head assemblies and the incorporation of advanced cameras of both the film and electro-optical type. Use of microprocessor control and digital bus inter-face form the central design philosophy. For long range, high altitude, standoff missions, the Data Annotation System computes the projected latitude and longitude of central target position from aircraft position and attitude. This complements the use of longer ranges and high altitudes for reconnaissance missions.

  6. Hydrologic reconnaissance of the Blue Creek Valley area, Box Elder County, Utah

    USGS Publications Warehouse

    Bolke, E.L.; Price, Don

    1972-01-01

    This report is the tenth in a series of reports prepared by the U. S. Geological Survey in cooperation with the Utah Department of Natural Resources, Division of Water Rights, that describe the water resources of selected areas in northwestern Utah. The purpose of this report is to present available hydrologic data for the Blue Creek Valley area and to provide a quantitative evaluation of the potential water-resources development of the area.

  7. Hydrologic reconnaissance of Rush Valley, Tooele County, Utah

    USGS Publications Warehouse

    Hood, James W.; Price, Don; Waddell, K.M.

    1969-01-01

    This report is the third in a series by the U. S. Geological Survey in cooperation with the Utah Department of Natural Resources, Division of Water Rights, which describes the water resources of the western basins of Utah. Its purpose is to present available hydrologic data for Rush Valley, to provide an evaluation of the potential water-resources development of the valley, and to identify needed studies that would help provide an understanding of the valley's water supply.

  8. Pulling Teeth: Why Humans Are More Important Than Hardware in Airborne Intelligence, Surveillance, and Reconnaissance

    DTIC Science & Technology

    2015-06-12

    soldiers aloft in tethered hot air balloons to observe enemy positions on the battlefield. The Union Army even established a separate Balloon Corps from...December 20, 2014). 1 describe man-lifting kites in the Far East while eighteenth and nineteenth century manned balloons and piloted fixed wing aircraft...in the twentieth and twenty-first centuries provided this capability. One of the first recorded Western uses of manned balloons for ISR purposes

  9. Reconnaissance Waccamaw River Basin North Carolina and South Carolina. Flood Control and Related Purposes.

    DTIC Science & Technology

    1981-09-01

    livestock are relatively minor as compared to cultivated crops. The production of timber, pulpwood, and veneer logs is also an important land use. Timber... Minor channel and bridge improvements would be required for commercial navigation up to this point. According to local residents, durinq periods of...people expressed a desire that no changes be made in the river’s present characteristics other than minor clearinq and snagging and some dredging of

  10. Red River of the North, Reconnaissance Report: Wild Rice River.

    DTIC Science & Technology

    1980-12-01

    2 lists the waste treatment facilities and needs of fifteen coumnities within the subbasin. Hydropower There are three dams located on the Wild Rice...potential hydroelectric sites. The dams were built primarily for flood control purposes and are classified as small-scale facilities. The main obstacles...drain a combined total area of 2,233 square miles. Several small low-water dams and a few larger impoundments have been constructed on the river and its

  11. Hydrologic reconnaissance of Skull Valley, Tooele County, Utah

    USGS Publications Warehouse

    Hood, James W.; Waddell, K.M.

    1968-01-01

    This report is the second in a series by the U.S. Geological Survey in cooperation with the Utah Department of Natural Resources, Division of Water Rights, which describes the water resources of the western basins of Utah. Its purpose is to present available hydrologic data on Skull Valley, to provide an evaluation of the potential water-resource development of the valley, and to identify needed studies that would help provide an understandingof the valley's water supply.

  12. When Military Fitness Standards No Longer Apply: The High Prevalence of Metabolic Syndrome in Recent Air Force Retirees.

    PubMed

    Cranston, Marcus M; True, Mark W; Wardian, Jana L; Carriere, Rishawn M; Sauerwein, Tom J

    2017-07-01

    Metabolic syndrome (MetS) is strongly associated with cardiovascular disease. With MetS prevalence rates increasing in the U.S. population, prevention efforts have largely focused on diet and exercise interventions. Before retirement, military service members have met fitness requirements for at least 20 years, and have lower MetS rates compared to age-matched U.S. population controls (23.4% vs. 39.0%), which suggests a protective effect of the lifestyle associated with military service. However, MetS rates in military retirees have not been previously reported, so it is unknown whether this protective effect extends beyond military service. The purpose of this study was to examine the prevalence of MetS and individual diagnostic criteria in a population of recent U.S. Air Force (USAF) retirees. We obtained institutional review board approval for all participating sites at Wilford Hall Ambulatory Surgical Center. From December 2011 to May 2013, USAF retirees within 8 years of their date of retirement were recruited at five USAF bases. Consenting subjects underwent examination and laboratory studies to assess the five diagnostic criteria measures for MetS. We used binary logistic regression to examine the relationship between various factors and the presence of MetS. The study population (n = 381) was primarily male (81.9%), enlisted (71.1%) and had a mean age of 48.2 years. When applying the American Heart Association MetS diagnostic criteria to this population, the MetS prevalence was 37.2%. When using alternative diagnostic criteria found in other published studies that did not include the use of cholesterol medications, the MetS prevalence was 33.6%. Per American Heart Association criteria, the prevalence of each of the MetS diagnostic criteria was as follows: central obesity, 39.8%; elevated fasting glucose, 32.4%; high blood pressure, 56.8%; low-high-density lipoproteins cholesterol, 33.3%; and elevated triglycerides, 42.7%. MetS was more common among males (odds ratio [OR] = 4.05; confidence interval [CI] = 1.94, 8.48) and enlisted (OR = 2.23; CI = 1.24, 4.01). It was also strongly associated with a history of participating in the Air Force Weight Management Program (OR = 2.82; CI = 1.41, 5.63) and increased weight since retirement (OR = 4.00; CI = 1.84, 8.70). However, the study did not find an association between the presence of MetS and time since retirement or self-reported diet and exercise changes since retirement. The MetS prevalence among recent USAF retirees represents a shift from age-matched active duty rates toward higher rates described in the overall U.S. This finding suggests the protective health effects of fitness standards may be reduced shortly after retirement. This is true despite activities such as screening before and during military service and exposure to USAF health promotion efforts and fitness standards throughout a period of active duty service lasting at least 20 years. In general, military members should be counseled that on retirement, efforts to maintain a healthy weight have continued benefit and should not be forgotten. The risk of MetS after retirement is particularly increased for those identified as being overweight during their active duty careers. Interventions that prevent and reduce unhealthy weight gain may be an appropriate investment of resources and should be studied further. Reprint & Copyright © 2017 Association of Military Surgeons of the U.S.

  13. Deployable reconnaissance from a VTOL UAS in urban environments

    NASA Astrophysics Data System (ADS)

    Barnett, Shane; Bird, John; Culhane, Andrew; Sharkasi, Adam; Reinholtz, Charles

    2007-04-01

    Reconnaissance collection in unknown or hostile environments can be a dangerous and life threatening task. To reduce this risk, the Unmanned Systems Group at Virginia Tech has produced a fully autonomous reconnaissance system able to provide live video reconnaissance from outside and inside unknown structures. This system consists of an autonomous helicopter which launches a small reconnaissance pod inside a building and an operator control unit (OCU) on a ground station. The helicopter is a modified Bergen Industrial Twin using a Rotomotion flight controller and can fly missions of up to one half hour. The mission planning OCU can control the helicopter remotely through teleoperation or fully autonomously by GPS waypoints. A forward facing camera and template matching aid in navigation by identifying the target building. Once the target structure is identified, vision algorithms will center the UAS adjacent to open windows or doorways. Tunable parameters in the vision algorithm account for varying launch distances and opening sizes. Launch of the reconnaissance pod may be initiated remotely through a human in the loop or autonomously. Compressed air propels the half pound stationary pod or the larger mobile pod into the open portals. Once inside the building, the reconnaissance pod will then transmit live video back to the helicopter. The helicopter acts as a repeater node for increased video range and simplification of communication back to the ground station.

  14. Cooperative Autonomous Robots for Reconnaissance

    DTIC Science & Technology

    2009-03-06

    REPORT Cooperative Autonomous Robots for Reconnaissance 14. ABSTRACT 16. SECURITY CLASSIFICATION OF: Collaborating mobile robots equipped with WiFi ...Cooperative Autonomous Robots for Reconnaissance Report Title ABSTRACT Collaborating mobile robots equipped with WiFi transceivers are configured as a mobile...equipped with WiFi transceivers are configured as a mobile ad-hoc network. Algorithms are developed to take advantage of the distributed processing

  15. Hydrologic reconnaissance of Grouse Creek valley, Box Elder County, Utah

    USGS Publications Warehouse

    Hood, J.W.; Price, Don

    1970-01-01

    This report is the seventh in a series by the U. S. Geological Survey in cooperation with the Utah Department of Natural Resources, Division of Water Rights, which describes water resources of the western basins of Utah. Its purpose is to present available hydrologic data on Grouse Creek valley, to provide an evaluation of the potential water-resource development of the valley, and to identify studies that would help provide a better understanding of the valley's water supply

  16. Work Domain Analysis of Australia’s Air Power System: Purpose-related Functions of Combat; Transport; and Intelligence, Surveillance, and Reconnaissance Subsystems

    DTIC Science & Technology

    2015-03-01

    of nature (e.g., flooding, drought, cyclone, earthquake, volcanic eruption , disease epidemic) or an act of man (e.g., riots, civil unrest, war...e.g., volcanic eruption ). To militate against these potential dangers, assets contributing to People Rescue (e.g., fixed-wing aircraft, rotary-wing...operating altitude of an aircraft to avoid strong winds or volcanic ash). UNCLASSIFIED DSTO-TR-3085 UNCLASSIFIED 69  “…rescue helicopters and

  17. United States Air Force Summary (Consolidation of Statistical Digest and USAF Summary), Ninth Edition

    DTIC Science & Technology

    1983-01-01

    MARIANA ISLS ,..•o 8 GUAM .. o ANDERSEN AFB ,. BONIN ISLSo o o I) . o • ... .... t gO 6 ~,... ()0 KAitENA AB i"r o EAST CHINA SEA • ~. USAF MAJOR... Dave (OK) Hertel, Denni s M. (MI) Price, Melvin (IL) Bennett, Charles E. (FL) Military Personnel & Compensation Mitche 11 , Donal d J. (NY) Holt...Schroeder, Patricia (CO) Stump, Bob (AZ) Skelton, Ike (MO) Leath, James M. (TX) McCurdy, Dave (OK) Smith, Joseph F. (PA) TABLE 81 (Cont I d

  18. Myrtle Beach AFB South Carolina. Revised Uniform Summary of Surface Weather Observations. Parts A-F

    DTIC Science & Technology

    1975-07-03

    DATA PROCESSING BRNCm2 TAC/USAF SURFACE WINDS AIP wATHER SERVIC/?AL PERCENTAGE FREQUENCY OF WIND DIRECTION AND SPEED (FROM HOURLY OBSERVATIONS...TRANS MONI, ALL WATHER 1200-1400 CLAM MUES (L.$,t.) ( CONDITION SPEED MEAN (KNTS) i’ 4-6 7. 10 11. 16 17.21 22 .27 28 . 33 34.40 41 .47 48 • !5 ;t56...PRUCESSING BRANCH 2ETAC/USAF SURFACE WINDSAIR wATHER SERVICE/MAC PERCENTAGE FREQUENCY OF WIND DIRECTION AND SPEED (FROM HOURLY OBSERVATIONS) 13717

  19. A Qualitative Study of the European Trucking Industry and Logistics Strategies Using the United States Motor Carrier Industry as a Guide

    DTIC Science & Technology

    1992-09-01

    UNITED STATES MOTOR CARRIER INDUSTRY AS A GUIDE THESIS David W. Butler Andrew P. Wilhelm Captain, USAF Captain, USAF AFIT/GLM/LSM/92S-7 Approved for...UNITED STATES MOTOR CARRIER INDUSTRY AS A GUIDE THESIS Presented to the Faculty of the School of Systems and Logistics of the Air Force Institute of...THE EUROPEAN TRUCKING INDUSTRY AND LOGISTICS STRATEGIES USING THE UNITED STATES MOTOR CARRIER INDUSTRY AS A GUIDE I. Introduction General Issue The

  20. 1. Credit USAF, 1943. Original housed in the Photograph Files, ...

    Library of Congress Historic Buildings Survey, Historic Engineering Record, Historic Landscapes Survey

    1. Credit USAF, 1943. Original housed in the Photograph Files, AFFTC/HO, Edwards AFB, California. View west showing eastern elevation of wooden hangar while under construction. Building 4401 was also historically designated Hangar No. 1. The north side of the Unicon Portable Hangar (Building 4305) appears at the extreme left of the view. Concrete apron is under construction in the foreground. Building 4402 is same design and construction as Building 4401. - Edwards Air Force Base, North Base, Hangar No. 1, First & B Streets, Boron, Kern County, CA

  1. Credit USAF, 7 September 1945. Original housed in the Muroc ...

    Library of Congress Historic Buildings Survey, Historic Engineering Record, Historic Landscapes Survey

    Credit USAF, 7 September 1945. Original housed in the Muroc Flight Test Base, Unit History, 1 September 1942 - 30 June 1945. Alfred F. Simpson Historical Research Agency. United States Air Force. Maxwell AFB, Alabama. Photo captioned "Oblique view of Recreation Hall/Chapel Bldg. T73." Movies on marquee were "Why Girls Leave Home" and "Blazing the Western Trail." View looks west from camera position across E Street - Edwards Air Force Base, North Base, Recreation Hall & Chapel T-73, E Street near North Base Road, Boron, Kern County, CA

  2. Credit USAF, ca. 1945. Original housed in the Muroc Flight ...

    Library of Congress Historic Buildings Survey, Historic Engineering Record, Historic Landscapes Survey

    Credit USAF, ca. 1945. Original housed in the Muroc Flight Test Base, Unit History, 1 September 1942 - 30 June 1945. Alfred F. Simpson Historical Research Agency. United States Air Force. Maxwell AFB, Alabama. View looks north at a hutment typical of several structures erected at the Muroc Flight Test Base (North Base) ca. 1943-1945. Similar structures, Buildings T-61, T-62 and T-63, lie in the distance behind T-40 - Edwards Air Force Base, North Base, Barracks T-40, Second & A Streets, Boron, Kern County, CA

  3. Credit USAF, ca. 1943. Original housed in the Muroc Flight ...

    Library of Congress Historic Buildings Survey, Historic Engineering Record, Historic Landscapes Survey

    Credit USAF, ca. 1943. Original housed in the Muroc Flight Test Base, Unit History, 1 September 1942 - 30 June 1945. Alfred F. Simpson Historical Research Agency. United States Air Force. Maxwell AFB, Alabama. Historic view looking northeast along southeast edge of swimming pool during construction. The wavy edge of the pool visible here remains as a ground surface feature in 1995. Building in the background is the second Bachelor Officers' Quarters (T-15) built in 1943 - Edwards Air Force Base, North Base, Swimming Pool, Second Street, Boron, Kern County, CA

  4. USAF bioenvironmental noise data handbook. Volume 148. T-37B in-flight crew noise

    NASA Astrophysics Data System (ADS)

    Hille, H. K.

    1981-11-01

    The T-37B is a USAF two-seat primary trainer aircraft. This report provides measured data defining the bioacoustic environments at flight crew/passenger locations inside this aircraft during normal flight operations. Data are reported at one location for 19 different flight conditions and psychoacoustic measures: overall and band sound pressure levels, C-weighted and A-weighted sound levels, preferred speech interference level, perceived noise level, and limiting times for total daily exposure of personnel with and without standard Air Force ear protectors.

  5. 8. Credit USAF, ca. 1952. Original housed in the Photograph ...

    Library of Congress Historic Buildings Survey, Historic Engineering Record, Historic Landscapes Survey

    8. Credit USAF, ca. 1952. Original housed in the Photograph Files, AFFTC/HO, Edwards AFB, California. Oblique low-level aerial view of North Base looking northeast. Based on positions and types of aircraft and automobiles, this photo taken same day as HAER photo CA-170-7. Most temporary structures in this view have been demolished with the exception of the hangars. The concrete foundations remain of many structures, while no trace was found of others. - Edwards Air Force Base, North Base, North Base Road, Boron, Kern County, CA

  6. A Study of the Relationship between Years of Commissioned Service and the Perceived Importance of the Military Compensation Package to Air Force Officers.

    DTIC Science & Technology

    1984-09-01

    OF’ COMMISSIONED SERVICE AND THE PERCEIVED IMPORTANCE OF THE MILITARY COMPENSATION PACKAGE TO AIR FORCE OFFICERS THESIS Daniel A. Ovelbar Captain, USAF... THESIS Daniel A. Cvelbar Captain, USAF AFI T/GSM/LSY/84S-8 DTICSLECTE3 Approved for public release; distribution unlimited The contents of the document...OF THE MILITARY COMPENSATION PACKAGE TO AIR FORCE OFFICERS THESIS Presented to the Faculty of the School of Systems and Logistics of the Air Force

  7. The Continued Need for USAF Light Attack post OEF/OIF: A Survey of West African Infrastructure to Support Tactical Air Operations

    DTIC Science & Technology

    2013-04-01

    Mauritania’s two main airfields, at Nouakchott and Atar , have 9,800 foot runways that A-10s could operate from. In addition to those airfields...running road passes through Atar , Zouerat and Bir Moghrein on the way to Algeria. Without the use of the bases at Zouerat and Bir Moghrein the highway...runs almost 400 miles beyond extended duration air support from Atar . With the legacy platforms currently available, the USAF could provide air

  8. A New Facility Design and Work Method for the Quantitative Fit Testing Laboratory

    DTIC Science & Technology

    1989-05-01

    AtRV=’Uk kUB C RELEASEIW R190 I ERNEST A. HAYGOOD, 1st Lt, USAF Executive Officer, Civilian Institution Proarams 17. COSATI CODES 18. SUBJECT TERMS...22. NAME O RESPONSIBLE INDIVIDUAL 22b. TELEPHONE (Mdud. e Cd) 22c. OFFICE SYMBOL ERNEST A. HAYGOOD, lst Lt, USAF (513) 255-2259 A AFIT/CI DO Form 1473...Morgan et al. C1963) define a link as "any connection between a man and a machine or between one man and another" (p. 322). Lippert [1971) studied the

  9. The Oliktok Point Arctic Research Facility (OPARF)

    NASA Astrophysics Data System (ADS)

    Zak, B. D.; Ivey, M.

    2011-12-01

    For the past year, the US Department of Energy, through Sandia National Laboratories, has operated a Designated User Facility at Oliktok Point Alaska, on the Arctic Ocean coast near the western end of the Prudhoe Bay oil fields. The primary purpose of this user facility is to accommodate and support manned and unmanned airborne measurement platforms over the Arctic Ocean and adjacent coastline as the arctic sea ice recedes. The speed at which the sea ice is receding exceeds model-projected speeds considerably for reasons that are not fully understood. The ultimate objective is to incorporate improved understanding of the radiative and other processes impacting sea ice recession into the relevant climate models. OPARF is based at a USAF Long Range Radar Station, an old Distant Early Warning (DEW) radar station built during the height of the Cold War, but continuing to be operated to track air traffic over the pole. The USAF has graciously granted Sandia and DOE use of selected facilities at Oliktok on a non-interference basis. DOE also maintains FAA-granted Restricted Airspace over Oliktok Point and adjacent ocean. In addition, DOE has also requested that the FAA establish a Warning Area over international waters 30 miles wide and 700 miles long stretching from near Oliktok towards the North Pole. That request is currently being processed by the FAA, with the public comment period now closed. This paper will update OPARF developments for potential users of the Oliktok user facility and other interested researchers.

  10. Kvichak River RISEC Project Resource Reconnaissance and Physical Characterization

    DOE Data Explorer

    Jarlath McEntee

    2015-10-01

    During the summer and fall of 2011 TerraSond Ltd. (TerraSond) completed a bathymetric survey and hydrokinetic energy assessment of the Kvichak River at Igiugig, Alaska. The purpose of this work was to characterize the initial site conditions for the design and installation of a hydrokinetic turbine to provide electric power for the village. There were six distinct phases of work for this project. The first was a literature review and investigation of prior surveys and hydrologic studies done in the area. The second, third, fourth, and fifth phases consisted of four field expeditions conducted over the summer and fall of 2011. These expeditions consisted of an initial reconnaissance, multi beam bathymetric surveys, flow velocity and discharge measurements, a survey of water levels, and detailed flow velocity studies. The final phase of the project was complete data reduction, and preparation of the final report with its accompanying map sheets and data packages. This submission contains the final report for the Kvichak River RiISEC Project in addition to weather data for Igiugig, AK, Summer 2015.

  11. Design and simulation of flight control system for man-portable micro reconnaissance quadcopter

    NASA Astrophysics Data System (ADS)

    Yin, Xinfan; Zhang, Daibing; Fang, Qiang; Shen, Lincheng

    2017-10-01

    The quadcopter has been widely used in the field of aerial photography and environmental detection, because of its advantages of VTOL, simple structure, and easy-control. In the field of urban anti-terrorism or special operations, micro reconnaissance quadcpter has its unique advantages such as all-weather taking off and landing, small noise and so on, and it is very popular with special forces and riot police. This paper aims at the flight control problem of the micro quadcopter, for the purposes of attitude stabilization control and trajectory tracking control of the micro quadcopter, first, the modeling of the micro quadcopter is presented. And using the MATLAB/SIMULINK toolbox to build the flight controller of the micro quadcopter, and then simulation analysis and real flight test are given. The results of the experiment show that the designed PID controller can correct the flight attitude shift effectively and track the planned tracks well, and can achieve the goal of stable and reliable flight of the quadcopter. It can be a useful reference for the flight control system design of future special operations micro UAV.

  12. Blinding the Eyes of the Corps: Foresight at Last?

    DTIC Science & Technology

    1992-06-01

    Figure 2: RF-4B ADAS Code Matrix Block ..................... 69 vii TABLE OF ABBREVIATIONS AGL above ground level ATARS Advanced Air Reconnaissance...prior to 1995, the currently projected year for initial operational capability (IOC) of the Advanced Tactical Air Reconnaissance System ( ATARS ). 59...made a conscious commitment to participate in the development of the Advanced Tactical Airborne Reconnaissance System ( ATARS ), a CCD-based, "electro

  13. Multiple Autonomous Vehicles for Minefield Reconnaissance and Mapping

    DTIC Science & Technology

    1997-12-01

    NPS-ME-97-008 NAVAL POSTGRADUATE SCHOOL Monterey, California ItC A D- 19980421 131 =C QUALTY Ui Ji.CTEJ) THESIS MULTIPLE AUTONOMOUS VEHICLES FOR...MULTIPLE AUTONOMOUS VEHICLES FOR MINEFIELD 5. FUNDING NUMBERS RECONNAISSANCE AND MAPPING N0001497WX30039 6. AUTHOR(S) Jack A. Starr 7. PERFORMING... AUTONOMOUS VEHICLES FOR MINEFIELD RECONNAISSANCE AND MAPPING Jack A. Starr Lieutenant, United States Navy B.S., Oregon State University, 1991 Submitted in

  14. Improving Air Force Imagery Reconnaissance Support to Ground Commanders.

    DTIC Science & Technology

    1983-06-03

    reconnaissance support in Southeast Asia due to the long response times of film recovery and 26 processing capabilities and inadequate command and control...reconnaissance is an integral part of the C31 information explosion. Traditional silver halide film products, chemically processed and manually distributed are...being replaced with electronic near-real-time (NRT) imaging sensors. The term "imagery" now includes not only conventional film based products (black

  15. Increased flight surgeon role in military aeromedical evacuation.

    PubMed

    Lyons, T J; Connor, S B

    1995-10-01

    Physicians were involved in the development of aeromedical evacuation (medevac) and flight surgeons flew as crewmembers on the first U.S. military medevac flights. However, since World War II flight surgeons have not been routinely assigned to operational medevac units. The aeromedical literature addressing the role of physicians in medevac is controversial. Recent contingencies involving the U.S. Air Force (USAF) have required the augmentation of medevac units with flight surgeons. Beginning in 1992, the United States Air Forces Europe (USAFE) assigned three flight surgeons to the medevac squadron. Between 2 February 1993 and 24 March 1994 USAFE moved 241 patients on 29 missions out of the former Yugoslavia--most of these missions had a flight surgeon on the crew. Because advance medical information on the status of these patients is often nonexistent, the presence of a physician on the crew proved life-saving in some instances. In peacetime operations, there has been a recent trend in the European theater for the USAF to move more unstable patients. Dedicated medevac flight surgeons have proven to have the specific experience and training to perform effectively in the role of in-flight medical attendant. In addition, they are effective in negotiating with referring physicians about the urgency of movement, required equipment, the need for medical attendants, etc. These flight surgeons also provide medical coverage of transiting patients in the Aeromedical Staging Flight (ASF), thus providing needed continuity in the medevac system. Dedicated medevac flight surgeons fill a unique and valuable role in medevac systems. Agencies with medevac units should consider assigning flight surgeons to these units.

  16. Twenty-Seven-Year Follow-Up of Vietnam Air War USAF POWs and Matched Controls Not Captured: A Qualitative Study.

    PubMed

    Sledge, William; Rozanova, Julia; Dorset, Julianne

    2018-01-01

    To provide a follow up of a 1976 study of the impact of captivity on U.S. Air Force (USAF) POWs and USAF Controls matched for time in Southeast Asia, military rank and aircraft crew position. Qualitative study of replies to open ended questions of positive and negative changes due to their captivity/combat experiences made by participants (POWs and Controls) who replied in both 1976 and in 2003. Both groups acknowledged positive and negative effects of the experiences in 1976. In 1976 and 2003 the POWs mainly reported negative effects on career and family domains but positive effects of individual development and growth. Controls reported mild negative effects on family in 1976, and benefits to their careers and sense of self in both 1976 and 2003. Captivity during the Vietnam War for USAF included two types of extreme duress which were the incarceration itself; and the repatriation experience which entailed re-assimilation despite loss of occupation and disrupted families. Despite these obstacles, POWs exhibited substantial resilience in achieving self-growth and how they regarded themselves psychologically in comparison to their matched control fellow aviators who while also suffering a lesser separation from family, tended to prosper in their careers and were proud of their accomplishments. Long term separation from work, family and friends and the inability to return to their families and careers with the effectiveness demanded by their ambition were a more devastating ongoing consequence of their captivity than the immediate suffering of their imprisonment.

  17. Urinary Polycyclic Aromatic Hydrocarbon (OH-PAH) Metabolite Concentrations and the Effect of GST Polymorphisms Among US Air Force Personnel Exposed to Jet Fuel

    PubMed Central

    Rodrigues, Ema G.; Smith, Kristen; Maule, Alexis L.; Sjodin, Andreas; Li, Zheng; Romanoff, Lovisa; Kelsey, Karl; Proctor, Susan; McClean, Michael D.

    2016-01-01

    Objective To evaluate the association between inhalation exposure to jet propulsion fuel 8 (JP-8) and urinary metabolites among US Air Force (USAF) personnel, and investigate the role of glutathione S-transferase polymorphisms. Methods Personal air samples were collected from 37 full-time USAF personnel during 4 consecutive workdays and analyzed for JP-8 constituents and total hydrocarbons. Pre- and postshift urine samples were collected each day and analyzed for polycyclic aromatic hydrocarbon urinary metabolites. Results Work shift exposure to total hydrocarbons was significantly associated with postshift urinary 1-naphthol (β = 0.17; P = <0.0001), 2-naphthol (β = 0.09; P = 0.005), and 2-hydroxyfluorene concentrations (β = 0.08; P = 0.006), and a significant gene-environment interaction was observed with glutathione S-transferase mu-1. Conclusions USAF personnel experience inhalation exposure to JP-8, which is associated with absorption of JP-8 constituents while performing typical job-related tasks, and in our data the glutathione S-transferase mu-1 polymorphism was associated with differential metabolism of naphthalene. PMID:24806557

  18. Urinary polycyclic aromatic hydrocarbon (OH-PAH) metabolite concentrations and the effect of GST polymorphisms among US Air Force personnel exposed to jet fuel.

    PubMed

    Rodrigues, Ema G; Smith, Kristen; Maule, Alexis L; Sjodin, Andreas; Li, Zheng; Romanoff, Lovisa; Kelsey, Karl; Proctor, Susan; McClean, Michael D

    2014-05-01

    To evaluate the association between inhalation exposure to jet propulsion fuel 8 (JP-8) and urinary metabolites among US Air Force (USAF) personnel, and investigate the role of glutathione S-transferase polymorphisms. Personal air samples were collected from 37 full-time USAF personnel during 4 consecutive workdays and analyzed for JP-8 constituents and total hydrocarbons. Pre- and postshift urine samples were collected each day and analyzed for polycyclic aromatic hydrocarbon urinary metabolites. Work shift exposure to total hydrocarbons was significantly associated with postshift urinary 1-naphthol (β = 0.17; P = <0.0001), 2-naphthol (β = 0.09; P = 0.005), and 2-hydroxyfluorene concentrations (β = 0.08; P = 0.006), and a significant gene-environment interaction was observed with glutathione S-transferase mu-1. USAF personnel experience inhalation exposure to JP-8, which is associated with absorption of JP-8 constituents while performing typical job-related tasks, and in our data the glutathione S-transferase mu-1 polymorphism was associated with differential metabolism of naphthalene.

  19. Soil runway friction evaluation in support of USAF C-17 transport aircraft operations

    NASA Technical Reports Server (NTRS)

    Yager, Thomas J.

    1995-01-01

    A series of NASA Diagonal-Braked Vehicle (DBV) test runs were performed on the soil runway 7/25 at Holland landing zone, Fort Bragg, North Carolina, near Pope Air Force Base in March 1995 at the request of the Air Force C-17 System Program Office. These ground vehicle test results indicated that the dry runway friction level was suitable for planned C-17 transport aircraft landing and take-off operations at various gross weights. These aircraft operations were successfully carried out. On-board aircraft deceleration measurements were comparable to NASA DBV measurements. Additional tests conducted with an Army High Mobility Multi-Purpose Wheeled Vehicle equipped with a portable decelerometer, showed good agreement with NASA DBV data.

  20. Observations of C-Band Brightness Temperatures and Ocean Surface Wind Speed and Rain Rate from the Hurricane Imaging Radiometer (HIRAD) during GRIP and HS3

    NASA Technical Reports Server (NTRS)

    Miller, Timothy L.; James, M. W.; Roberts, J. B.; Jones, W. L.; Biswas, S.; Ruf, C. S.; Uhlhorn, E. W.; Atlas, R.; Black, P.; Albers, C.

    2013-01-01

    HIRAD flew on high-altitude aircraft over Earl and Karl during NASA s GRIP (Genesis and Rapid Intensification Processes) campaign in August - September of 2010, and at the time of this writing plans to fly over Atlantic tropical cyclones in September of 2012 as part of the Hurricane and Severe Storm Sentinel (HS3) mission. HIRAD is a new C-band radiometer using a synthetic thinned array radiometer (STAR) technology to obtain cross-track resolution of approximately 3 degrees, out to approximately 60 degrees to each side of nadir. By obtaining measurements of emissions at 4, 5, 6, and 6.6 GHz, observations of ocean surface wind speed and rain rate can be retrieved. This technique has been used for many years by precursor instruments, including the Stepped Frequency Microwave Radiometer (SFMR), which has been flying on the NOAA and USAF hurricane reconnaissance aircraft for several years to obtain observations within a single footprint at nadir angle. Results from the flights during the GRIP and HS3 campaigns will be shown, including images of brightness temperatures, wind speed, and rain rate. Comparisons will be made with observations from other instruments on the campaigns, for which HIRAD observations are either directly comparable or are complementary. Features such as storm eye and eye-wall, location of storm wind and rain maxima, and indications of dynamical features such as the merging of a weaker outer wind/rain maximum with the main vortex may be seen in the data. Potential impacts on operational ocean surface wind analyses and on numerical weather forecasts will also be discussed.

  1. White Paper - A Study of the Maneuver Battalion Reconnaissance or Scout Platoon

    DTIC Science & Technology

    1989-09-18

    of buzzwords may have sufficed, but battalions, compan -s, arid platoons in the field suffered. A issic example was the tank and mechanized infantry...commander’s Intelligence Preparation of the Battlefield (IPB). Later in the reconnaissance chapter, dismounting is stressed. Reconnaissance by fire...cavalry assets or even benefit from their collateral employment. They also cited artificialities in that OPFOR sco ts are given much more time to recon

  2. Tropical Cyclone Reconnaissance with the Global Hawk: Operational Thresholds and Characteristics of Convective Systems Over the Tropical Western North Pacific

    DTIC Science & Technology

    2013-12-01

    Tropical cyclone research is an intense ongoing science that has acquired even greater importance in this era of global climate change . Increased study of...RECONNAISSANCE WITH THE GLOBAL HAWK: OPERATIONAL THRESHOLDS AND CHARACTERISTICS OF CONVECTIVE SYSTEMS OVER THE TROPICAL WESTERN NORTH PACIFIC by...TROPICAL CYCLONE RECONNAISSANCE WITH THE GLOBAL HAWK: OPERATIONAL THRESHOLDS AND CHARACTERISTICS OF CONVECTIVE SYSTEMS OVER THE TROPICAL WESTERN

  3. Women in Combat Pros and Cons

    DTIC Science & Technology

    1988-04-01

    and Cons . Major Thomas H. Cecil 88-0490 "--"insights into tomorrou,"’ ..v- A A 0 PtY-i f(.> i’I,-:::x:’~ --pcr~ j.~ ~~* --. -- iiV • DISCLAIMER The...k. r- r,’ I’. REPORT NUMBER 88-0490 TITLE WOMEN IN COMBAT-PROS AND CONS AUTHOR(S) MAJOR THOMAS H. CEC-IL, USAF -% FACULTY ADVISOR CH, LT COL DAVID W...NUMBERS 11 TITLE (include Security Classification) WOMEN IN COMBAT--PROS AND CONS 12. PERSON4AL AUTHOR(S) Cecil, Thomas H1., Major, USAF 9a YýOF REPORT

  4. Anthropometric accommodation in USAF cockpits

    NASA Technical Reports Server (NTRS)

    Zehner, Gregory F.

    1994-01-01

    Over the past three years, a new set of methodologies has been developed to specify and evaluate anthropometric accommodation in USAF crewstation designs. These techniques are used to improve the ability of the pilot to reach controls, to safely escape the aircraft, to achieve adequate mobility and comfort, and to assure full access to the visual field both inside and outside the aircraft. This paper summarized commonly encountered aircraft accommodation problems, explains the failure of the traditional 'percentile man' design concept to resolve these difficulties, and suggests an alternative approach for improving cockpit design to better accommodate today's more heterogeneous flying population.

  5. 10. Credit USAF, 1945. Original housed in the Muroc Flight ...

    Library of Congress Historic Buildings Survey, Historic Engineering Record, Historic Landscapes Survey

    10. Credit USAF, 1945. Original housed in the Muroc Flight Test Base, Unit History, 1 September 1942 30 June 1945. Alfred F. Simpson Historical Research Agency. United States Air Force. Maxwell AFB, Alabama. View of jet engine rotor balancing machine with engine rotor in place for balancing operations. Original caption reads "Balancing bucket wheel of jet engine, Muroc Flight Test Base, Oct. 1945"; personnel not identified. Location where photograph was taken not determined, but presumed to be in shops of Building 4505. - Edwards Air Force Base, North Base, Hangar, End of North Base Road, Boron, Kern County, CA

  6. 4. Credit USAF, ca. 1945. Original housed in the Photograph ...

    Library of Congress Historic Buildings Survey, Historic Engineering Record, Historic Landscapes Survey

    4. Credit USAF, ca. 1945. Original housed in the Photograph Files, AFFTC/HO, Edwards AFB, California. Low level oblique aerial view of Muroc Flight Test Base (North Base), looking southwest along flightline. HANG-P-A hangar (Building 4505) is in the right foreground. A Bell XP-59A Airacomet, the United States military's first jet propelled aircraft, is being towed on the apron toward the control tower. Other aircraft in the foreground include Douglas DC-3s, North American Aviation P-51 Mustangs, and Lockheed P-38 Lightnings. - Edwards Air Force Base, North Base, North Base Road, Boron, Kern County, CA

  7. United States Air Force F-35A Operational Basing Environmental Impact Statement. Appendix E: Comments

    DTIC Science & Technology

    2013-09-01

    Germanos, Nicholas M Civ USAF HQ ACC/A7NS From: Sent: To: Subject: Hi Leo Ioannou Wednesday, July 10, 2013 11:28 AM Germanos, Nicholas M Civ USAF HQ...we have them here . And the F35s, even if they are louder, I would not mind them either. Remember . Keep the F35s coming. SOUND OF FREEDOM Leo ...34 Explaining further, Reuters reported that: uThose a re the dates that Loc kheed Martin’s F-35 will achieve <http://articles.chicagotribune.com/2013-05

  8. YF-12 Lockalloy ventral fin program, volume 1. [design analysis, fabrication, and manufacturing of aircraft structures using aluminum and beryllium alloys for the lockheed YF-12 aircraft

    NASA Technical Reports Server (NTRS)

    Duba, R. J.; Haramis, A. C.; Marks, R. F.; Payne, L.; Sessing, R. C.

    1976-01-01

    Results are presented of the YF-12 Lockalloy Ventral Fin Program which was carried out by Lockheed Aircraft Corporation - Advanced Development Projects for the joint NASA/USAF YF-12 Project. The primary purpose of the program was to redesign and fabricate the ventral fin of the YF-12 research airplane (to reduce flutter) using Lockalloy, and alloy of beryllium and aluminum, as a major structural material. A secondary purpose, was to make a material characterization study (thermodynamic properties, corrosion; fatigue tests, mechanical properties) of Lockalloy to validate the design of the ventral fin and expand the existing data base on this material. All significant information pertinent to the design and fabrication of the ventral fin is covered. Emphasis throughout is given to Lockalloy fabrication and machining techniques and attendant personnel safety precautions. Costs are also examined. Photographs of tested alloy specimens are shown along with the test equipment used.

  9. Reconnaissance of Water Quality at Four Swine Farms in Jackson County, Florida, 1993

    DTIC Science & Technology

    1996-01-01

    applications on agricultural land. (Krider, 1987). Since the estimated annual wet manure product in pounds per animal is: 3,407 for breeding swine , and...Reconnaissance of Water Quality at Four Swine Farms in Jackson County, Florida, 1993 By Jerilyn J. Collins U.S. Geological Survey Open File Report...COVERED - 4. TITLE AND SUBTITLE Reconnaissance of Water Quality at Four Swine Farms in Jackson County, Florida, 1993 5a. CONTRACT NUMBER 5b. GRANT

  10. Objectives for Mars Orbital Missions in the 2020s: Report from a MEPAG Science Analysis Group

    NASA Astrophysics Data System (ADS)

    Zurek, R. W.; Campbell, B. A.; Diniega, S.; Lock, R. E.

    2015-12-01

    NASA Headquarters is looking at possible missions to Mars to follow the proposed 2020 Mars rover mission currently in development. One option being considered is a multi-functional orbiter, launched in the early 2020's, whose capabilities could address objectives in the following areas: • Replenishment of the telecommunications and reconnaissance infrastructure presently provided by the aging Mars Odyssey and Mars Reconnaissance Orbiters; • Scientific and technical progress on the NRC Planetary Science Decadal Survey priorities, updated MEPAG Goals, and/or follow-up of new discoveries; • Location and quantification of in situ resources for utilization by future robotic and human surface-based missions; and • Data needed to address Strategic Knowledge Gaps (SKGs), again for possible human missions. The Mars Exploration Program Analysis Group (MEPAG) was asked to prepare an analysis of possible science objectives and remote sensing capabilities that could be implemented by such a multi-purpose Mars orbiter launched in the 2022/24 timeframe. MEPAG conducted this analysis through formation of a Next Orbiter Science Analysis Group (NEX-SAG), which was chartered jointly by the NASA Science and Human Exploration Directorates. The SAG was asked to conduct this study within a range of mission capabilities, including the possible first use of Solar Electric Propulsion (SEP) in the Mars system. SEP could provide additional power enabling new payload components and possible changes in orbit (e.g., orbital inclination change) that permit different mission observational campaigns (e.g., polar and non-polar). Special attention was paid towards identifying synergies between science investigations, reconnaissance, and resource/SKG needs. We will present the findings and conclusions of this NEX-SAG regarding possible objectives for the next NASA Orbiter to Mars.

  11. Demographic, Lifestyle Factors, and Reasons for Use of Dietary Supplements by Air Force Personnel.

    PubMed

    Austin, Krista G; Price, Lori Lyn; McGraw, Susan M; Leahy, Guy; Lieberman, Harris R

    2016-07-01

    Dietary supplement (DS) use is common among U.S. Army personnel to purportedly improve health, provide energy, and increase strength. However, a comprehensive analysis of DS use among U.S. Air Force (USAF) personnel has not been conducted using the same survey instrument, which would permit direct comparisons to DS use by Army personnel. A standardized questionnaire was used to assess DS use, demographic factors, and reasons for use of DS by USAF personnel (N = 1750). Logistic regression models adjusted for age, sex, and rank were used to determine relationships among categories of DS (multivitamin and multimineral, individual vitamins and minerals, protein/amino acid supplements, combination products, herbal supplements, purported steroid analogs, and other) and demographic factors. Findings were compared to reports from other military services and civilian populations. DS were used by 68% of USAF personnel: 35% used 1-2 DS ≥ 1 time/wk, 13% 3-4 DS ≥ 1 time/wk, and 20% ≥ 5 DS ≥ 1 time/wk. There were 45% of personnel who used a multivitamin and mineral, 33% protein supplements, 22% individual vitamins/minerals, 22% combination products, and 7% herbals. Logistic regression demonstrated aerobic exercise duration and strength training were associated with increased DS use. Individuals who previously deployed were more likely to use DS. Like Army personnel, college students and athletes, USAF personnel use more DS than the general population and are more likely to use purported performance enhancing DS, such as protein supplements, and concurrently consume multiple DS. Austin KG, Price LL, McGraw SM, Leahy G, Lieberman HR. Demographic, lifestyle factors, and reasons for use of dietary supplements by Air Force personnel. Aerosp Med Hum Perform. 2016; 87(7):628-637.

  12. Using the Freiburg Acuity and Contrast Test to measure visual performance in USAF personnel after PRK.

    PubMed

    Dennis, Richard J; Beer, Jeremy M A; Baldwin, J Bruce; Ivan, Douglas J; Lorusso, Frank J; Thompson, William T

    2004-07-01

    Photorefractive keratectomy (PRK) may be an alternative to spectacle and contact lens wear for United States Air Force (USAF) aircrew and may offer some distinct advantages in operational situations. However, any residual corneal haze or scar formation from PRK could exacerbate the disabling effects of a bright glare source on a complex visual task. The USAF recently completed a longitudinal clinical evaluation of the long-term effects of PRK on visual performance, including the experiment described herein. After baseline data were collected, 20 nonflying active duty USAF personnel underwent PRK. Visual performance was then measured at 6, 12, and 24 months after PRK. Visual acuity (VA) and contrast sensitivity (CS) data were collected by using the Freiburg Acuity and Contrast Test (FrACT), with the subject viewing half of the runs through a polycarbonate windscreen. Experimental runs were completed under 3 glare conditions: no glare source and with either a broadband or a green laser (532-nm) glare annulus (luminance approximately 6090 cd/m) surrounding the Landolt C stimulus. Systematic effects of PRK on VA relative to baseline were not identified. However, VA was almost 2 full Snellen lines worse with the laser glare source in place versus the broadband glare source. A significant drop-off was observed in CS performance after PRK under conditions of no glare and broadband glare; this was the case both with and without the windscreen. As with VA, laser glare disrupted CS performance significantly and more than broadband glare did. PRK does not appear to have affected VA, but the changes in CS might represent a true decline in visual performance. The greater disruptive effects from laser versus broadband glare may be a result of increased masking from coherent spatial noise (speckle) surrounding the laser stimulus.

  13. X-43C Flight Demonstrator Project Overview

    NASA Technical Reports Server (NTRS)

    Moses, Paul L.

    2003-01-01

    The X-43C Flight Demonstrator Project is a joint NASA-USAF hypersonic propulsion technology flight demonstration project that will expand the hypersonic flight envelope for air-breathing engines. The Project will demonstrate sustained accelerating flight through three flights of expendable X-43C Demonstrator Vehicles (DVs). The approximately 16-foot long X-43C DV will be boosted to the starting test conditions, separate from the booster, and accelerate from Mach 5 to Mach 7 under its own power and autonomous control. The DVs will be powered by a liquid hydrocarbon-fueled, fuel-cooled, dual-mode, airframe integrated scramjet engine system developed under the USAF HyTech Program. The Project is managed by NASA Langley Research Center as part of NASA's Next Generation Launch Technology Program. Flight tests will be conducted by NASA Dryden Flight Research Center off the coast of California over water in the Pacific Test Range. The NASA/USAF/industry project is a natural extension of the Hyper-X Program (X-43A), which will demonstrate short duration (approximately 10 seconds) gaseous hydrogen-fueled scramjet powered flight at Mach 7 and Mach 10 using a heavy-weight, largely heat sink construction, experimental engine. The X-43C Project will demonstrate sustained accelerating flight from Mach 5 to Mach 7 (approximately 4 minutes) using a flight-weight, fuel-cooled, scramjet engine powered by much denser liquid hydrocarbon fuel. The X-43C DV design flows from integrating USAF HyTech developed engine technologies with a NASA Air-Breathing Launch Vehicle accelerator-class configuration and Hyper-X heritage vehicle systems designs. This paper describes the X-43C Project and provides the background for NASA's current hypersonic flight demonstration efforts.

  14. Atmospheric Profiles, Clouds and the Evolution of Sea Ice Cover in the Beaufort and Chukchi Seas: Atmospheric Observations and Modeling as Part of the Seasonal Ice Zone Reconnaissance Surveys

    DTIC Science & Technology

    2017-06-04

    Ice Zone Reconnai ssance Survey project (SIZRS). Combined with oceanographic and sea ice components of the SIZRS project. The projects i dentified...with clear , warm advection events . 1S. SUBJECT TERMS Sea i ce, atmosphere , sea ice retreat , Seasonal Ice Zone Reconnaissance Survey , SIZRS , model...Reconnaissance Surveys Axel Schweiger Applied Physics Laboratory, University of Washington, 1013 NE 40th St., Seattle, Wa. 98105 phone: (206) 543

  15. Atmospheric Profiles, Clouds and the Evolution of Sea Ice Cover in the Beaufort and Chukchi Seas: Atmospheric Observations and Modeling as Part of the Seasonal Ice Zone Reconnaissance Surveys

    DTIC Science & Technology

    2017-06-04

    Cover in the Beaufort and Chukchi Seas: Atmospheric Observations and Modeling as Part of the Seasonal Ice Zone Reconnaissance Surveys Axel...of the atmospheric component of the Seasonal Ice Zone Reconnaissance Survey project (SIZRS). Combined with oceanographic and sea ice components of...indicate cumulative probabilities. Vertical lines show median errors for forecast and climatology, respectively Figure 7 Correlation coefficient

  16. Fighting blind: why US Army Divisions Need a Dedicated Reconnaissance and Security Force

    DTIC Science & Technology

    2017-05-25

    dedicated reconnaissance and security force. By the 2003 invasion of Iraq, 3d Infantry Division employed a division cavalry squadron that integrated...26 1 Introduction 3-7 Cavalry conducted reconnaissance and security tasks ahead of and on the flank of 3d Infantry Division as the...division led Vth Corp’s attack from Kuwait to Baghdad in 2003. 3-7 Cavalry’s movements confused the enemy about 3d Infantry Division’s location and intent

  17. Red River of the North Reconnaissance Report: Pembina River.

    DTIC Science & Technology

    1980-12-01

    the mallard, blue -winged teal, pintail, gadwall, northern shoveler, green -winged teal, American wigeon, and redhead. [ Rush Lake receives heavy use...r.D-Ri4. 787 RED RIVER OF THE NORTH RECONNAISSANCE REPORT: PEMBINA 1/2 RIVER(IJ) GULF SOUTH RESEAPRCH INST BATON ROUGE LA DEC 9 DACU77-8@-C-e8i7B...ii% ---. :w: U ;r u --- ’w AD-A140 787 RED RIVER OF THE NORTH RECONNAISSANCE , %h,%! iREPORT , _ PEMBINA ; RIVER CD j- - D FINAL RMPORT ’ December

  18. The Need For and Benefits of the Creation of the Light Armored Reconnaissance Regiment

    DTIC Science & Technology

    2010-04-14

    instead of the 8 battalions reporting straight to a commanding general provides significant advantages . When asked about the benefits of the recent...The Need For and Benefits of the Creation of the Light Armored N/A Reconnaissance Regiment 5b. GRANT NUMBER N/A 5c. PROGRAM ELEMENT NUMBER N/A 6...MASTER OF MILITARY STUDIES THE NEED FOR AND BENEFITS OF THECREATION OF THE LIGHT ARMORED RECONNAISSANCE REGIMENT SUBMITTED IN PARTIAL FULFILLMENT OF

  19. Mars Reconnaissance Orbiter Taking Shape

    NASA Image and Video Library

    2004-08-09

    Lockheed Martin Space Systems engineer Terry Kampmann left and lead technician Jack Farmerie work on assembly and test of NASA Mars Reconnaissance Orbiter spacecraft bus in a cleanroom at the company Denver facility.

  20. Material Excavated by a Fresh Impact and Identified as Water Ice

    NASA Image and Video Library

    2009-09-24

    The Compact Reconnaissance Imaging Spectrometer for Mars, an instrument on NASA Mars Reconnaissance Orbiter, obtained information confirming material excavated by a fresh impact and Identified as water ice.

  1. Seventh Annual Workshop on Space Operations Applications and Research (SOAR 1993), volume 2

    NASA Technical Reports Server (NTRS)

    Krishen, Kumar (Editor)

    1994-01-01

    This document contains papers presented at the Space Operations, Applications and Research Symposium (SOAR) Symposium hosted by NASA/Johnson Space Center (JSC) and cosponsored by NASA/JSC and U.S. Air Force Materiel Command. SOAR included NASA and USAF programmatic overviews, plenary session, panel discussions, panel sessions, and exhibits. It invited technical papers in support of U.S. Army, U.S. Navy, Department of Energy, NASA, and USAF programs in the following areas: robotics and telepresence, automation and intelligent systems, human factors, life support, and space maintenance and servicing. SOAR was concerned with Government-sponsored research and development relevant to aerospace operations.

  2. United States Air Force Statistical Digest, Fiscal Year 1964, Nineteenth Edition

    DTIC Science & Technology

    1964-09-30

    opera- tions, materiel, personnel, training, medical serv- ices, finance, security and law enforcement, fa- cilities, transportation , Military...RTER. AND HOUR. FI..OWN DURING QU"’RTER. By COMM"’ND, WORL.D-WIOE - FY 1964 AGE (IN MONTHlJ) D,.TRIBUTION 0.- USAF A,RCR...FT By MI •• ION, DE . ION. AHD...WOfl ....D_wIOE - 30 JUN 1964 • • • • • • • • • • • • • • • • • • • • • •••••• USAF AND COMPONENT A,RCR.....T G...,NS AND LoasEs By MI •• roN. DES

  3. TRASANA. Force Stratification System User Handbook.

    DTIC Science & Technology

    1977-09-01

    n - 4 u m W CL a 0-C C COCOc:11 7 k., 0 =. t.4 c-Ac( ~ lqa . U~ ~~~~~ p. c A? W 0=0 ’. 0 a - 0 - EO U=ON~.S4’ o S .0 p. . 0 0 0 ’ ft 0 LO Cl O.CCL. . k...ADGRU, USAF Institute of Technology I Chief, ADGRU, US Naval War College 1 Chief, US Elm, USAF Air-Ground Operations School 1 USA Rep, USMC Educ Cen...Marine Corps Dev and Educ Command I USA Rep, Comb Svc Spt Prog School, Atlantic I Commandant, USA Element, School of Music 1 Liaison Offices/Officers

  4. 5. Credit USAF, ca. 1944. Original housed in the Muroc ...

    Library of Congress Historic Buildings Survey, Historic Engineering Record, Historic Landscapes Survey

    5. Credit USAF, ca. 1944. Original housed in the Muroc Flight Test Base, Unit History, 1 September 1942 - 30 June 1945. Alfred F. Simpson Historical Research Agency. United States Air Force. Maxwell AFB, Alabama. Interior view of hangar, looking north northwest. Note exposed wooden construction. Two jet engines lie partially concealed by tarpaulins in the background, along with a combustion chamber assembly (horizontal cylinders in a circular array). On the workbench in the foreground lie an engine rotor hub and what appears to be an engine fuel line assembly. - Edwards Air Force Base, North Base, Hangar No. 1, First & B Streets, Boron, Kern County, CA

  5. 7. Credit USAF, ca. 1952. Original housed in the Photograph ...

    Library of Congress Historic Buildings Survey, Historic Engineering Record, Historic Landscapes Survey

    7. Credit USAF, ca. 1952. Original housed in the Photograph Files, AFFTC/HO, Edwards AFB, California. Oblique aerial view of North Base AFFTC (Air Force Flight Test Center) looking west northwest. The flight line at the edge of Rogers Dry Lake appears in the foreground, served by the facility's four hangars. Temporary structures beyond the hangars were demolished later in the 1950s. The fence that formerly surrounded the swimming pool in earlier photos has been taken down. In the distance lies the Jet Propulsion Laboratory Edwards Test Station, in its pre-1953 configuration. - Edwards Air Force Base, North Base, North Base Road, Boron, Kern County, CA

  6. Sixth Annual Workshop on Space Operations Applications and Research (SOAR 1992), volume 2

    NASA Technical Reports Server (NTRS)

    Krishen, Kumar (Editor)

    1993-01-01

    This document contains papers presented at the Space Operations, Applications, and Research Symposium (SOAR) hosted by the U.S. Air Force (USAF) on 4-6 Aug. 1992. The symposium was cosponsored by the Air Force Material Command and by NASA/JSC. Key technical areas covered during the symposium were robotics and telepresence, automation and intelligent systems, human factors, life sciences, and space maintenance and servicing. The SOAR differed from most other conferences in that it was concerned with Government-sponsored research and development relevant to aerospace operations. Symposium proceedings include papers covering various disciplines presented by experts from NASA, the USAF, universities, and industry.

  7. X-15 test pilots - in a lighter mood

    NASA Technical Reports Server (NTRS)

    1966-01-01

    The X-15 pilots clown around in front of the #2 aircraft.From left to right: USAF Capt. Joseph Engle, USAF Maj. Robert Rushworth, NASA test pilot John 'Jack' McKay, USAF Maj. William 'Pete' Knight, NASA test pilot Milton Thompson, and NASA test pilot William Dana. First flown in 1959 from the NASA High Speed Flight Station (later renamed the Dryden Flight Research Center), the rocket powered X-15 was developed to provide data on aerodynamics, structures, flight controls and the physiological aspects of high speed, high altitude flight. Three were built by North American Aviation for NASA and the U.S. Air Force. They made a total of 199 flights during a highly successful research program lasting almost ten years, following which its speed and altitude records for winged aircraft remained unbroken until the Space Shuttle first returned from earth orbit in 1981. The X-15's main rocket engine provided thrust for the first 80 to 120 seconds of a 10 to 11 minute flight; the aircraft then glided to a 200 mph landing. The X-15 reached altitudes of 354,200 feet (67.08 miles) and a speed of 4,520 mph (Mach 6.7).

  8. Aircraft and related factors in crashes involving spatial disorientation: 15 years of U.S. Air Force data.

    PubMed

    Lyons, Terence J; Ercoline, William; O'Toole, Kevin; Grayson, Kevin

    2006-07-01

    Previous studies have determined that spatial disorientation (SD) causes 0.5-23% of aircraft crashes, but SD-related crash and fatality rates in different aircraft types have not been systematically studied. SD crashes for the fiscal years 1990 to 2004 and aircraft sortie numbers for all U.S. Air Force (USAF) aircraft were obtained from the USAF Safety Center. Contingency table analysis and Chi-squared tests were used to evaluate differences in SD rates. SD accounted for 11% of USAF crashes with an overall rate of 2.9 per million sorties and a crash fatality rate of 69%. The SD rate was higher in fighter/attack aircraft and helicopters than in training and transport aircraft. The risk of SD was increased at night with 23% of night crashes being caused by SD. But the SD rate and crash fatality rate were not higher in single-crewmember aircraft. SD risk is significantly increased in helicopters and fighter/attack aircraft and at night. The data suggest that a second crewmember does not protect against SD. Further study of specific SD scenarios could lead to focused interventions for SD prevention.

  9. USAF Bioenvironmental Noise Data Handbook. Volume 160: KC-10A aircraft, near and far-field noise

    NASA Astrophysics Data System (ADS)

    Powell, R. G.

    1982-09-01

    The USAF KC-10A aircraft is an advanced tanker/cargo aircraft powered by three CF6-50C2 turbofan engines. This report provides measured and extrapolated data defining the bioacoustic environments produced by this aircraft operating on a concrete runup pad for eight engine/power configurations. Near-field data are reported for one location in a wide variety of physical and psychoacoustic measures: overall and band sound pressure levels, C-weighted and A-weighted sound levels, preferred speech interference levels, perceived noise levels, and limiting times for total daily exposure of personnel with and without standard Air Force ear protectors. Far-field data measured at 15 locations are normalized to standard meteorological conditions and extrapolated from 75-8000 meters to derive sets of equal-value contours for these same seven acoustic measures as functions of angle and distance from the source. Refer to Volume 1 of this handbook, USAF Bioenvironmental Noise Data Handbook, Vol 1: Organization, Content and Application, AMRL-TR-75-50(1) 1975, for discussion of the objective and design of the handbook, the types of data presented, measurement procedures, instrumentation, data processing, definitions of quantities, symbols, equations, applications, limitations, etc.

  10. PEER - January 12, 2010 Haiti Earthquake - Related Events

    Science.gov Websites

    Related Events Related Events Preliminary Reconnaissance Presentation about Chile Earthquake Tuesday Topic: Chile EERI/PEER Reconnaissance Briefing Date: Tuesday, March 30, 2010 Time: 3:00 PM to 5PM

  11. Overview of the Mars Reconnaissance Orbiter mission

    NASA Technical Reports Server (NTRS)

    Mateer, B.; Graf, J.; Zurek, R.; Jones, R.; Eisen, H.; Johnston, M.; Jai, D. B.

    2002-01-01

    The Mars Reconnaissance Orbiter will deliver to Mars orbit a payload to conduct remote sensing science observations, characterize sites for future landers, and provide critical telecom/navigation relay capability for follow-on missions.

  12. Physiological and Selective Attention Demands during an International Rally Motor Sport Event

    PubMed Central

    Turner, Anthony P.; Richards, Hugh

    2015-01-01

    Purpose. To monitor physiological and attention responses of drivers and codrivers during a World Rally Championship (WRC) event. Methods. Observational data were collected from ten male drivers/codrivers on heart rate (HR), core body (T core) and skin temperature (T sk), hydration status (urine osmolality), fluid intake (self-report), and visual and auditory selective attention (performance tests). Measures were taken pre-, mid-, and postcompetition day and also during the precompetition reconnaissance. Results. In ambient temperatures of 20.1°C (in-car peak 33.9°C) mean (SD) peak HR and T core were significantly elevated (P < 0.05) during rally compared to reconnaissance (166 (17) versus 111 (16) beats·min−1 and 38.5 (0.4) versus 37.6 (0.2)°C, resp.). Values during competitive stages were substantially higher in drivers. High urine osmolality was indicated in some drivers within competition. Attention was maintained during the event but was significantly lower prerally, though with considerable individual variation. Conclusions. Environmental and physical demands during rally competition produced significant physiological responses. Challenges to thermoregulation, hydration status, and cognitive function need to be addressed to minimise potentially negative effects on performance and safety. PMID:25866799

  13. Evaluation of sinkhole occurrence in the Valley and Ridge Province, East Tennessee: Phase 3

    DOE Office of Scientific and Technical Information (OSTI.GOV)

    Newton, J.G.; Tanner, J.M.

    1987-11-01

    Data from a reconnaissance-type inventory of sinkhole occurrence and from more detailed inventories in selected areas were used to determine regional density and frequency of sinkhole occurrence in the Valley and Ridge Province, Tennessee. The overall database consisted of 333 sinkholes of which 211, or 63 percent of the total, were classified as induced. Almost all induced sinkholes resulted from construction activities, such as grading, ditching, and impoundment of water. Extrapolation of data to provide estimates of regional sinkhole density necessitated adjustment of the reconnaissance inventory. Adjustment factors were calculated by comparing reconnaissance inventories from selected areas with those obtainedmore » from detailed inventories in the same areas. The number of sinkholes in the detailed inventories was 5 and 8.5 times greater than the number in the reconnaissance inventories.« less

  14. Atmospheric Profiles, Clouds, and the Evolution of Sea Ice Cover in the Beaufort and Chukchi Seas Atmospheric Observations and Modeling as Part of the Seasonal Ice Zone Reconnaissance Surveys

    DTIC Science & Technology

    2012-09-30

    Ice Cover in the Beaufort and Chukchi Seas Atmospheric Observations and Modeling as Part of the Seasonal Ice Zone Reconnaissance Surveys Axel...temperatures. These changes in turn will affect the evolution of the SIZ. An appropriate representation of this feedback loop in models is critical if we... modeling experiments as part of the atmospheric component of the Seasonal Ice Zone Reconnaissance Survey project (SIZRS). We will • Determine the role

  15. Tactical Reconnaissance and Security for the Armor Battalion Commander: Is the Scout Platoon Combat Capable or Combat Ineffective?

    DTIC Science & Technology

    1990-12-27

    reconnaissance force back to a heavy ele ,._.it capable of security missions and limited 10 reconnaissance. Vletnam continued the platoon’s emphasis on...College, Fort Leavenworth, KS, 30 November 1988 (CARL Ref. AOR215860). JouroaI ~ el Bacevich, LTC A. J. "Training Scouts." Armor, September 1987, pp. 37...Swanson, Major Steven G. " Bronco Nine Speaks His Mind." MIlitaryInteigence, April-June 1990, pp. 8- 10, 12. "The Bustle Rack." Armo,; March-April 1990

  16. Geotechnical effects of the 2015 magnitude 7.8 Gorkha, Nepal, earthquake and aftershocks

    USGS Publications Warehouse

    Moss, Robb E. S.; Thompson, Eric M.; Kieffer, D Scott; Tiwari, Binod; Hashash, Youssef M A; Acharya, Indra; Adhikari, Basanta; Asimaki, Domniki; Clahan, Kevin B.; Collins, Brian D.; Dahal, Sachindra; Jibson, Randall W.; Khadka, Diwakar; Macdonald, Amy; Madugo, Chris L M; Mason, H Benjamin; Pehlivan, Menzer; Rayamajhi, Deepak; Uprety, Sital

    2015-01-01

    This article summarizes the geotechnical effects of the 25 April 2015 M 7.8 Gorkha, Nepal, earthquake and aftershocks, as documented by a reconnaissance team that undertook a broad engineering and scientific assessment of the damage and collected perishable data for future analysis. Brief descriptions are provided of ground shaking, surface fault rupture, landsliding, soil failure, and infrastructure performance. The goal of this reconnaissance effort, led by Geotechnical Extreme Events Reconnaissance, is to learn from earthquakes and mitigate hazards in future earthquakes.

  17. Camera Ready to Install on Mars Reconnaissance Orbiter

    NASA Image and Video Library

    2005-01-07

    A telescopic camera called the High Resolution Imaging Science Experiment, or HiRISE, right was installed onto the main structure of NASA Mars Reconnaissance Orbiter left on Dec. 11, 2004 at Lockheed Martin Space Systems, Denver.

  18. PERSONNEL PROTECTION THROUGH RECONNAISSANCE ROBOTICS AT SUPERFUND REMEDIAL SITES

    EPA Science Inventory

    Investigation, mitigation, and clean-up of hazardous materials at Superfund sites normally require on-site workers to perform hazardous and sometimes potentially dangerous functions. uch functions include site surveys and the reconnaissance for airborne and buried toxic environme...

  19. Advanced U.S. military aircraft battery systems

    NASA Astrophysics Data System (ADS)

    Flake, Richard A.; Eskra, Michael D.

    1990-04-01

    While most USAF aircraft currently use vented Ni-Cd for dc electrical power and emergency power, as well as the powering of lights and instruments prior to engine starting, these batteries have high maintenance requirements, low reliability, and no built-in testing capability with which to check battery health prior to flight. The USAF Wright R&D Center accordingly initiated its Advanced Maintenance-Free NiCd Battery System development program in 1986, in order to develop a sealed Ni-Cd battery which would remain maintenance-free over a period of three years. Attention is being given to a high power bipolar battery design in which there are no individual cell cases or cell interconnects.

  20. Injuries and Illnesses of Vietnam War POWs Revisited. 5. Combined Service Group Risk Factors

    DTIC Science & Technology

    2017-11-08

    provide the decision was made report both the standard F test using the Tukey post-hoc test, as well as the Welch test using the Games -Howell test for...USAF USN - USA USAF - USA Torture Mann-Whitney U < 0.001 < 0.001 0.170 Tukey HSD < 0.001 < 0.001 0.325 Games -Howell < 0.001 < 0.001 0.270 LOC months...Mann-Whitney U 0.185 < 0.001 < 0.001 Tukey HSD 0.015 0.013 0.578 Games -Howell 0.013 < 0.001 0.390 LOS weeks Mann-Whitney U < 0.001 < 0.001 0.541 Tukey

  1. A Study of the Perceptions of Roles, Responsibilities, and Problem Areas during Facility Transition in the Military Construction Program.

    DTIC Science & Technology

    1987-09-01

    priority based on the r sul-s of the rank order analysis of the combined USAF/COE Sa a jrouo n1 or :v.e USA’ dana qrouo. The COE data group sablisn...between the Resident Engineer and the DEEC is needed. O&M Manuals. The USAF conmnents anI concerns a bo,1t -ie &M M4ani’L3 4ere: 1. Som etnes g-ttinj the...teR-2sidJent Engineer- .ini tn- Chieff oDf Contract Man age-!n-enit ( DEEC is needed. Along the same line , onie COE comnmen t statedI that thne

  2. 3. Credit USAF, ca. 1945. Original housed in the Records ...

    Library of Congress Historic Buildings Survey, Historic Engineering Record, Historic Landscapes Survey

    3. Credit USAF, ca. 1945. Original housed in the Records of the Defense Intelligence Agency. Record Group 373. National Archives. Cartographic and Architectural Branch. Washington, D.C. Aerial orthophoto map 16PS5M79-IV23 of Muroc Flight Test Base (North Base), north faces up with runway at the top and Rogers Dry Lake at the lower right. Ammunition huts (not extant in 1995) appear in a cluster just south of the west end of the runway. Note runway markings on lakebed. Linear feature at very top of image is rocket sled test track designed and built 1944-1945. - Edwards Air Force Base, North Base, North Base Road, Boron, Kern County, CA

  3. The Sixth Annual Workshop on Space Operations Applications and Research (SOAR 1992)

    NASA Technical Reports Server (NTRS)

    Krishen, Kumar (Editor)

    1993-01-01

    This document contains papers presented at the Space Operations, Applications, and Research Symposium (SOAR) hosted by the U.S. Air Force (USAF) on 4-6 Aug. 1992 and held at the JSC Gilruth Recreation Center. The symposium was cosponsored by the Air Force Material Command and by NASA/JSC. Key technical areas covered during the symposium were robotic and telepresence, automation and intelligent systems, human factors, life sciences, and space maintenance and servicing. The SOAR differed from most other conferences in that it was concerned with Government-sponsored research and development relevant to aerospace operations. The symposium's proceedings include papers covering various disciplines presented by experts from NASA, the USAF, universities, and industry.

  4. 6. Credit USAF, April, 1945. Original in the possession of ...

    Library of Congress Historic Buildings Survey, Historic Engineering Record, Historic Landscapes Survey

    6. Credit USAF, April, 1945. Original in the possession of Ken G. Oldfield, Laguna Hills, California. View looking west across North Base flightline of XP-80s Shooting Stars undergoing accelerated service tests. HANG-N-A hangars No. 1 (Building 4401) and No. 2 (Building 4402) appear at left of view, with runway control tower (T-65, or Building 4500) at far right. Flight operations offices were in T-42 (Building 4502) at base of control tower; this structure was not extant in 1995. In the background between the control tower and Building 4402 lies T-15, officer's quarters. - Edwards Air Force Base, North Base, North Base Road, Boron, Kern County, CA

  5. Multi-Dimensional Signal Processing Research Program

    DTIC Science & Technology

    1981-09-30

    applications to real-time image processing and analysis. A specific long-range application is the automated processing of aerial reconnaissance imagery...Non-supervised image segmentation is a potentially im- portant operation in the automated processing of aerial reconnaissance pho- tographs since it

  6. Fuel property effects on USAF gas turbine engine combustors and afterburners

    NASA Technical Reports Server (NTRS)

    Reeves, C. M.

    1984-01-01

    Since the early 1970s, the cost and availability of aircraft fuel have changed drastically. These problems prompted a program to evaluate the effects of broadened specification fuels on current and future aircraft engine combustors employed by the USAF. Phase 1 of this program was to test a set of fuels having a broad range of chemical and physical properties in a select group of gas turbine engine combustors currently in use by the USAF. The fuels ranged from JP4 to Diesel Fuel number two (DF2) with hydrogen content ranging from 14.5 percent down to 12 percent by weight, density ranging from 752 kg/sq m to 837 kg/sq m, and viscosity ranging from 0.830 sq mm/s to 3.245 sq mm/s. In addition, there was a broad range of aromatic content and physical properties attained by using Gulf Mineral Seal Oil, Xylene Bottoms, and 2040 Solvent as blending agents in JP4, JP5, JP8, and DF2. The objective of Phase 2 was to develop simple correlations and models of fuel effects on combustor performance and durability. The major variables of concern were fuel chemical and physical properties, combustor design factors, and combustor operating conditions.

  7. Characterization of microbial contamination in United States Air Force aviation fuel tanks.

    PubMed

    Rauch, Michelle E; Graef, Harold W; Rozenzhak, Sophie M; Jones, Sharon E; Bleckmann, Charles A; Kruger, Randell L; Naik, Rajesh R; Stone, Morley O

    2006-01-01

    Bacteria and fungi, isolated from United States Air Force (USAF) aviation fuel samples, were identified by gas chromatograph fatty acid methyl ester (GC-FAME) profiling and 16S or 18S rRNA gene sequencing. Thirty-six samples from 11 geographically separated USAF bases were collected. At each base, an above-ground storage tank, a refueling truck, and an aircraft wing tank were sampled at the lowest sample point, or sump, to investigate microbial diversity and dispersion within the fuel distribution chain. Twelve genera, including four Bacillus species and two Staphylococcus species, were isolated and identified. Bacillus licheniformis, the most prevalent organism isolated, was found at seven of the 11 bases. Of the organisms identified, Bacillus sp., Micrococcus luteus, Sphinogmonas sp., Staphylococcus sp., and the fungus Aureobasidium pullulans have previously been isolated from aviation fuel samples. The bacteria Pantoea ananatis, Arthrobacter sp., Alcaligenes sp., Kocuria rhizophilia, Leucobacter komagatae, Dietza sp., and the fungus Discophaerina fagi have not been previously reported in USAF aviation fuel. Only at two bases were the same organisms isolated from all three sample points in the fuel supply distribution chain. Isolation of previously undocumented organisms suggests either, changes in aviation fuel microbial community in response to changes in aviation fuel composition, additives and biocide use, or simply, improvements in isolation and identification techniques.

  8. 4. July 1971. AERIAL RECONNAISSANCE II, ERIE RAILWAY SURVEY. ...

    Library of Congress Historic Buildings Survey, Historic Engineering Record, Historic Landscapes Survey

    4. July 1971. AERIAL RECONNAISSANCE II, ERIE RAILWAY SURVEY. - Erie Railway, Parallel French Creek Bridges, 100 feet South of Millers Station Road, 0.4 mile Northeast of State Route 408, 0.9 mile East of Cambridge Springs, Cambridge Springs, Crawford County, PA

  9. 2. July 1971. AERIAL RECONNAISSANCE II, ERIE RAILWAY SURVEY. ...

    Library of Congress Historic Buildings Survey, Historic Engineering Record, Historic Landscapes Survey

    2. July 1971. AERIAL RECONNAISSANCE II, ERIE RAILWAY SURVEY. - Erie Railway, Parallel French Creek Bridges, 100 feet South of Millers Station Road, 0.4 mile Northeast of State Route 408, 0.9 mile East of Cambridge Springs, Cambridge Springs, Crawford County, PA

  10. 3. July 1971. AERIAL RECONNAISSANCE II, ERIE RAILWAY SURVEY. ...

    Library of Congress Historic Buildings Survey, Historic Engineering Record, Historic Landscapes Survey

    3. July 1971. AERIAL RECONNAISSANCE II, ERIE RAILWAY SURVEY. - Erie Railway, Parallel French Creek Bridges, 100 feet South of Millers Station Road, 0.4 mile Northeast of State Route 408, 0.9 mile East of Cambridge Springs, Cambridge Springs, Crawford County, PA

  11. 1. July 1971. AERIAL RECONNAISSANCE II, ERIE RAILWAY SURVEY. ...

    Library of Congress Historic Buildings Survey, Historic Engineering Record, Historic Landscapes Survey

    1. July 1971. AERIAL RECONNAISSANCE II, ERIE RAILWAY SURVEY. - Erie Railway, Parallel French Creek Bridges, 100 feet South of Millers Station Road, 0.4 mile Northeast of State Route 408, 0.9 mile East of Cambridge Springs, Cambridge Springs, Crawford County, PA

  12. 15 CFR 270.101 - Preliminary reconnaissance.

    Code of Federal Regulations, 2013 CFR

    2013-01-01

    ... INSTITUTE OF STANDARDS AND TECHNOLOGY, DEPARTMENT OF COMMERCE NATIONAL CONSTRUCTION SAFETY TEAMS NATIONAL CONSTRUCTION SAFETY TEAMS Establishment and Deployment of Teams § 270.101 Preliminary reconnaissance. (a) To... the site of a building failure. The Director may establish and deploy a Team to conduct the...

  13. 15 CFR 270.101 - Preliminary reconnaissance.

    Code of Federal Regulations, 2010 CFR

    2010-01-01

    ... INSTITUTE OF STANDARDS AND TECHNOLOGY, DEPARTMENT OF COMMERCE NATIONAL CONSTRUCTION SAFETY TEAMS NATIONAL CONSTRUCTION SAFETY TEAMS Establishment and Deployment of Teams § 270.101 Preliminary reconnaissance. (a) To... the site of a building failure. The Director may establish and deploy a Team to conduct the...

  14. 15 CFR 270.101 - Preliminary reconnaissance.

    Code of Federal Regulations, 2012 CFR

    2012-01-01

    ... INSTITUTE OF STANDARDS AND TECHNOLOGY, DEPARTMENT OF COMMERCE NATIONAL CONSTRUCTION SAFETY TEAMS NATIONAL CONSTRUCTION SAFETY TEAMS Establishment and Deployment of Teams § 270.101 Preliminary reconnaissance. (a) To... the site of a building failure. The Director may establish and deploy a Team to conduct the...

  15. 15 CFR 270.101 - Preliminary reconnaissance.

    Code of Federal Regulations, 2014 CFR

    2014-01-01

    ... INSTITUTE OF STANDARDS AND TECHNOLOGY, DEPARTMENT OF COMMERCE NATIONAL CONSTRUCTION SAFETY TEAMS NATIONAL CONSTRUCTION SAFETY TEAMS Establishment and Deployment of Teams § 270.101 Preliminary reconnaissance. (a) To... the site of a building failure. The Director may establish and deploy a Team to conduct the...

  16. 15 CFR 270.101 - Preliminary reconnaissance.

    Code of Federal Regulations, 2011 CFR

    2011-01-01

    ... INSTITUTE OF STANDARDS AND TECHNOLOGY, DEPARTMENT OF COMMERCE NATIONAL CONSTRUCTION SAFETY TEAMS NATIONAL CONSTRUCTION SAFETY TEAMS Establishment and Deployment of Teams § 270.101 Preliminary reconnaissance. (a) To... the site of a building failure. The Director may establish and deploy a Team to conduct the...

  17. Resilience, Stress, Stigma, and Barriers to Mental Healthcare in U.S. Air Force Nursing Personnel.

    PubMed

    Hernandez, Stephen H A; Morgan, Brenda J; Parshall, Mark B

    Stigma may deter military service members from seeking mental health (MH) services. Previously, substantial proportions of U.S. Air Force (USAF) registered nurses and medical technicians reported concerns about stigma with accessing MH services; in particular, that unit members might lose confidence in them or perceive them as weak, unit leadership might treat them differently, or accessing care might affect career advancement. This study assessed the extent to which stigma and barriers to accessing MH services as perceived by USAF nursing personnel are associated with resilience, stress, previous deployment, or demographic characteristics. An anonymous, online survey was administered to active-duty USAF registered nurses and medical technicians at three locations (N = 250). The survey included demographic items, the Stigma and Barriers to Care scales, Conner-Davidson Resilience Scale, and Perceived Stress Questionnaire. Mean resilience was high, and perceived stress was moderate. About half of participants agreed that unit members might have less confidence in me (54%) or unit leadership might treat me differently (58%). Many also had concerns that it would harm my career (47%), I would be seen as weak (47%), or there would be difficulty getting time off work for treatment (45%). Stigma was positively correlated with perceived stress (r = .40, p < .01) and negatively correlated with resilience (r = -.24, p < .01). Officers had significantly higher stigma and resilience scores and lower stress scores compared with enlisted personnel, but those differences were small. This study validated previous findings that substantial percentages of USAF nursing personnel have concerns that accessing MH services may adversely affect their careers and how they are viewed by unit leaders and peers. In addition, higher levels of concern about stigma were associated with higher levels of stress and lower levels of resilience. Limitations included a low response rate (18%) and self-selection biases.

  18. X-43C Plans and Status

    NASA Technical Reports Server (NTRS)

    Moses, Paul L.

    2003-01-01

    X-43C Project is a hypersonic flight demonstration being executed as a collaboration between the National Aeronautics and Space Administration (NASA) and the United States Air Force (USAF). X-43C will expand the hypersonic flight envelope for air breathing engines beyond the history making efforts of the Hyper-X Program (X-43A). X-43C will demonstrate sustained accelerating flight during three flight tests of expendable X-43C Demonstrator Vehicles (DVs). The approximately 16-foot long X-43C DV will be boosted to the starting test conditions, separate from the booster, and accelerate from Mach 5 to Mach 7 under its own power and autonomous control. The DVs are to be powered by a liquid hydrocarbon-fueled, fuel-cooled, dual-mode, airframe integrated scramjet engine system developed under the USAF HyTech Program. The Project is managed by NASA Langley Research Center as part of NASA s Next Generation Launch Technology Program. Flight tests will be conducted by NASA Dryden Flight Research Center over water off the coast of California in the Pacific Test Range. The NASA/USAF/industry project is a natural extension of the Hyper-X Program (X-43A), which will demonstrate short duration ( 10 seconds) gaseous hydrogen-fueled scramjet powered flight at Mach 7 and Mach 10 using a heavyweight, largely heat sink construction, experimental engine. The X-43C Project will demonstrate sustained accelerating flight from Mach 5 to Mach 7 ( 4 minutes) using a flight-weight, fuel-cooled, scramjet engine powered by much denser liquid hydrocarbon fuel. The X-43C DV design flows from integrating USAF HyTech developed engine technologies with a NASA Air Breathing Launch Vehicle accelerator-class configuration and Hyper-X heritage vehicle systems designs. This paper describes the X-43C Project and provides background for NASA s current hypersonic flight demonstration efforts.

  19. Ranking the risk of wildlife species hazardous to military aircraft

    USGS Publications Warehouse

    Zakrajsek, E.J.; Bissonette, J.A.

    2005-01-01

    Collisions between birds and aircraft (birdstrikes) pose a major threat to aviation safety. Different species pose different levels of threat; thus, identification of the most hazardous species can help managers identify the level of hazard and prioritize mitigation efforts. Dolbeer et al. (2000) assessed the hazard posed by birds to civilian aircraft by analyzing data from the Federal Aviation Administration's (FAA) Wildlife Strike Database to rank the hazardous species and species groups. A similar analysis has not been done for the military but would be useful and necessary. Military flight characteristics differ from those of civilian flights. During the period 1985-1998, birdstrikes cost the United States Air Force (USAF) an average of $35 million/year in damage. Using the USAF Birdstrike Database, we selected and evaluated each species or species group by the number of strikes recorded in each of 3 damage categories. We weighted damage categories to reflect extent and cost of damage. The USAF Birdstrike Database contained 25,519 records of wildlife strikes in the United States. During the period 1985-1998, 22 (mean = 1.6/year) Class-A birdstrikes (>$1,000,000 damage, loss of aircraft, loss of life, or permanent total disability) were sustained, accounting for 80% of total monetary losses caused by birds. Vultures (Cathartes aura, Coragyps atratus, Caracara cheriway) were ranked the most hazardous species group (Hazard Index Rank [HIR] = 127) to USAF aircraft, followed by geese (Branta canadensis, Chen caerulescens, HIR = 76), pelicans (Pelecanus erythrorhynchos, P. occidentalis, HIR = 47), and buteos (Buteo sp., HIR = 30). Of the smaller flocking birds, blackbirds and starlings (mostly Agelaius phoeniceus, Euphagus cyanocephalus, Molothrus ater, Sturnus vulgaris, HIR = 46), horned larks (Eremophila alpestris, HIR = 24), and swallows (Families Hirundinidae, Apodidae, HIR = 23) were species groups ranked highest. Coupling these results with local bird census data to adjust hazard rank indices to specific locations can facilitate hazard management and lead to meaningful reductions in hazards and costs associated with birdstrikes.

  20. Design optimization of space launch vehicles using a genetic algorithm

    NASA Astrophysics Data System (ADS)

    Bayley, Douglas James

    The United States Air Force (USAF) continues to have a need for assured access to space. In addition to flexible and responsive spacelift, a reduction in the cost per launch of space launch vehicles is also desirable. For this purpose, an investigation of the design optimization of space launch vehicles has been conducted. Using a suite of custom codes, the performance aspects of an entire space launch vehicle were analyzed. A genetic algorithm (GA) was employed to optimize the design of the space launch vehicle. A cost model was incorporated into the optimization process with the goal of minimizing the overall vehicle cost. The other goals of the design optimization included obtaining the proper altitude and velocity to achieve a low-Earth orbit. Specific mission parameters that are particular to USAF space endeavors were specified at the start of the design optimization process. Solid propellant motors, liquid fueled rockets, and air-launched systems in various configurations provided the propulsion systems for two, three and four-stage launch vehicles. Mass properties models, an aerodynamics model, and a six-degree-of-freedom (6DOF) flight dynamics simulator were all used to model the system. The results show the feasibility of this method in designing launch vehicles that meet mission requirements. Comparisons to existing real world systems provide the validation for the physical system models. However, the ability to obtain a truly minimized cost was elusive. The cost model uses an industry standard approach, however, validation of this portion of the model was challenging due to the proprietary nature of cost figures and due to the dependence of many existing systems on surplus hardware.

  1. Next Generation Munitions Handler: Human-Machine Interface and Preliminary Performance Evaluation

    DOE Office of Scientific and Technical Information (OSTI.GOV)

    Draper, J.V.; Jansen, J.F.; Pin, F.G.

    1999-04-25

    The Next Generation Munitions Handler/Advanced Technology Demonstrator (NGMI-VATTD) is a technology demonstrator for the application of an advanced robotic device for re-arming U.S. Air Force (USAF) and U.S. Navy (USN) tactical fighters. It comprises two key hardware components: a heavy-lift dexterous manipulator (HDM) and a nonholonomic mobility platform. The NGMWATTD is capable of lifting weapons up to 4400 kg (2000 lb) and placing them on any weapons rack on existing fighters (including the F-22 Raptor). This report describes the NGMH mission with particular reference to human-machine interfaces. It also describes preliminary testing to garner feedback about the heavy-lift manipulator armmore » from experienced fighter load crewmen. The purpose of the testing was to provide preliminary information about control system parameters and to gather feed- back from users about manipulator arm functionality. To that end, the Air Force load crewmen interacted with the NGMWATTD in an informal testing session and provided feedback about the performance of the system. Certain con- trol system parameters were changed during the course of the testing and feedback from the participants was used to make a rough estimate of "good" initial operating parameters. Later, formal testing will concentrate within this range to identify optimal operating parameters. User reactions to the HDM were generally positive, All of the USAF personnel were favorably impressed with the capabilities of the system. Fine-tuning operating parameters created a system even more favorably regarded by the load crews. Further adjustment to control system parameters will result in a system that is operationally efficient, easy to use, and well accepted by users.« less

  2. Delegation of clinical dietetic tasks in military and civilian hospitals: implications for practice.

    PubMed

    Myers, M E; Gregoire, M B; Spears, M C

    1991-12-01

    The purposes of our research were two-fold: to determine perceptions of the quality of task performance and to identify dietetic personnel currently performing clinical dietetic tasks in military and civilian hospitals. Questionnaires were returned from 309 dietitians and 208 dietetic support personnel at 151 military and civilian hospitals (73% response overall). For tasks completed by support personnel, no task was rated as having optimum quality, 1 was rated as highly acceptable, 6 as acceptable, 19 as somewhat unacceptable, and 4 as unacceptable. Current performance ratings indicated that 1 task was performed solely by dietitians, 21 were completed by dietitians with assistance, 6 were completed jointly by dietitians and support personnel, 2 were completed by support personnel with supervision by dietitians, and no task was completed independently by support personnel. Tasks were grouped into four categories: basic clinical dietetics (11 tasks), intermediate and in-depth clinical dietetics (12 tasks), outpatient nutrition clinic (5 tasks), and nutrition education (community) (4 tasks). Quality scores for the US Air Force (USAF) hospitals were higher for all task categories except intermediate and in-depth clinical dietetic tasks. The quality scores of support personnel were higher than those of dietitians for all task categories. The USAF performance scores indicated significantly more involvement of support personnel. Generally, the performance scores of dietitians increased with experience; the scores of support personnel decreased with experience. Correlations between quality and performance ratings for individual tasks revealed low to moderate relationships. Our results suggest that additional delegation of tasks to dietetic support personnel may be possible without negatively affecting perceptions of the quality of task outcome.(ABSTRACT TRUNCATED AT 250 WORDS)

  3. 75 FR 43943 - Defense Science Board; Task Force on Counter Insurgency (COIN) Intelligence, Surveillance and...

    Federal Register 2010, 2011, 2012, 2013, 2014

    2010-07-27

    ... Insurgency (COIN) Intelligence, Surveillance and Reconnaissance (ISR) Operations AGENCY: Department of... Force on Counter Insurgency (COIN) Intelligence, Surveillance and Reconnaissance (ISR) Operations will... Defense. These meetings will identify how DoD intelligence can most effectively support COIN operations...

  4. Out of the Blue: NATO SOF Air Wing

    DTIC Science & Technology

    2012-03-01

    surveillance, targeting, and reconnaissance aircraft . This research also examines NSHQ’s training and readiness organizational structure, and proposes...mix contains rotary-wing and fixed-wing aviation platforms, as well as intelligence, surveillance, targeting, and reconnaissance aircraft . This...METHODOLOGY ..........................................................................................9  II.  AIRCRAFT CATEGORIZATION

  5. Audio-magnetotelluric methods in reconnaissance geothermal exploration

    USGS Publications Warehouse

    Hoover, D.B.; Long, C.L.

    1976-01-01

    and 18 600 Hz where artificial VLF sources are available. As a reconnaissance technique we use AMT surveys in conjunction with regional gravity, magnetic, and telluric surveys. The exploration depth is a function of the resistivities of the lithologic section, but typically ranges from the surface to 0.2 km in low-resistivity areas and to greater than 2 km in high-resistivity regions. Results of the initial reconnaissance AMT surveys provide a rational basis for deciding on the extent of costlier follow-up surveys. As part of the U.S. Geological Survey geothermal program, surveys were conducted in Long Valley and Surprise Valley, California; the Vale, Ore-Weiser, Idaho region; and Bruneau-Grand View, Raft River, and Island Park regions of Idaho. AMT surveys in five additional known geothermal resource areas (KGRA's) have been scheduled for completion by May 1975. In the Raft River and Bruneau-Grand View regions and Long Valley, follow-up electrical surveys substantiated the effectiveness of the AMT technique for reconnaissance surveying.

  6. Reconnaissance invariante d'objets 3-D et correlation SONG

    NASA Astrophysics Data System (ADS)

    Roy, Sebastien

    Cette these propose des solutions a deux problemes de la reconnaissance automatique de formes: la reconnaissance invariante d'objets tridimensionnels a partir d'images d'intensite et la reconnaissance robuste a la presence de bruit disjoint. Un systeme utilisant le balayage angulaire des images et un classificateur par trajectoires d'espace des caracteristiques permet d'obtenir la reconnaissance invariante d'objets tridimensionnels. La reconnaissance robuste a la presence de bruit disjoint est realisee au moyen de la correlation SONG. Nous avons realise la reconnaissance invariante aux translations, rotations et changements d'echelle d'objets tridimensionnels a partir d'images d'intensite segmentees. Nous utilisons le balayage angulaire et un classificateur a trajectoires d'espace des caracteris tiques. Afin d'obtenir l'invariance aux translations, le centre de balayage angulaire coincide avec le centre geometrique de l'image. Le balayage angulaire produit un vecteur de caracteristiques invariant aux changements d'echelle de l'image et il transforme en translations du signal les rotations autour d'un axe parallele a la ligne de visee. Le classificateur par trajectoires d'espace des caracteristiques represente une rotation autour d'un axe perpendiculaire a la ligne de visee par une courbe dans l'espace. La classification se fait par la mesure de la distance du vecteur de caracteristiques de l'image a reconnaitre aux trajectoires stockees dans l'espace. Nos resultats numeriques montrent un taux de classement atteignant 98% sur une banque d'images composee de 5 vehicules militaires. La correlation non-lineaire generalisee en tranches orthogonales (SONG) traite independamment les niveaux de gris presents dans une image. Elle somme les correlations lineaires des images binaires ayant le meme niveau de gris. Cette correlation est equivalente a compter le nombre de pixels situes aux memes positions relatives et ayant les memes intensites sur deux images. Nous presentons une realisation opto-electronique de la correlation SONG. Cette realisation utilise le correlateur a transformees conjointes. Les resultats des experiences numeriques et optiques montrent que le bruit disjoint ne nuit pas a la correlation SONG.

  7. Mines, prospects, and mineral sites, wilderness and RARE II areas, White Mountain National Forest, New Hampshire

    USGS Publications Warehouse

    Gazdik, G. C.; Harris, Gazdik; Welsh, R. A.; Girol, V. P.

    1988-01-01

    The areas investigated are located in the White Mountain National Forest in Coos, Grafton, and Carroll Counties, New Hampshire. Personnel from the U.S. Bureau of Mines conducted field reconnaissance of the westernmost areas, Kinsman Mountain, Mt. Wolf-Gordon Pond, Jobildunk, and Carr Mountain, in the fall of 1980. Field reconnaissance of the eastern areas, Great Gulf, Presidential Range-Dry River, Dartmouth Range, Pemigewasset and Wild River was conducted in the spring of 1981. A total of 237 rock and 103 panned-concentrate samples were collected during the investigations. Reconnaissance radiometric ground surveys were conducted at selected locations.

  8. 10. Credit USAF, 7 September 1945. Original housed in the ...

    Library of Congress Historic Buildings Survey, Historic Engineering Record, Historic Landscapes Survey

    10. Credit USAF, 7 September 1945. Original housed in the Muroc Flight Test Base, Unit History, 1 September 1942 - 30 June 1945. Alfred F. Simpson Historical Research Agency. United States Air Force. Maxwell AFB, Alabama. View looks northwest into jet engine test cell located on aircraft apron southeast of Building 4305. In background of photo can be seen doors of Unicon Portable Hangar on left, and southeast end of Building T-l Bachelor Officers' Quarters ("Desert Rat Hotel"). This view emphasizes the hangar's role as a test facility for developing and testing aircraft and aircraft systems, not simply as a "garage" for aircraft. - Edwards Air Force Base, North Base, Unicon Portable Hangar, First & C Streets, Boron, Kern County, CA

  9. Application Of Optical Techniques To Command, Control, And Communications (C3) Systems

    NASA Astrophysics Data System (ADS)

    Weinberg, M.; Steensma, P. D.

    1981-02-01

    This paper identifies and discusses specific applications of the optical transmission technology to various Command Control and Communications (C3) systems. Candidate C3 systems will first be identified and discussed briefly. These will include: 407L/485L Tactical Air Defense Systems (USAF) TAOC-85 Tactical Air Operations Central (USMC) SACDIN Strategic Air Command Digital Integrated Network (USAF) MX-C3 Missile "X" Command Control Communications Network The first tr are classified as tactical C3 systems while the latter two are classified as strategic C systems. Potential optical applications will be identified along with the benefits derived. Each application will be discussed with key parameters, cost performance benefits, potential problem areas, time frame for development identified.

  10. Military Transformation: Intelligence, Surveillance and Reconnaissance

    DTIC Science & Technology

    2003-01-17

    http:// ww2 .pstripes.osd.mil/01/research1.html]. The Air Force is the largest military provider of surveillance and reconnaissance as it operates most... Infrared System both had funding requests reduced. The cuts were due primarily to seriously escalating costs and program management issues.101 The DOD

  11. RECONNAISSANCE FOR ARSENIC, ESTRADIOL, ANTIBIOTICS, AND MICROBIAL RESISTANCE IN POULTRY-DOMINATED CHESAPEAKE BAY WATERSHEDS

    EPA Science Inventory

    There are concerns about the effects from the high density of poultry feeding operations and the extensive use of feed amendments on water quality in the Shenandoah Valley in Virginia and Delmarva Peninsula. Therefore, we conducted reconnaissance investigations in two Shenandoah ...

  12. Roads and Airfields I (Programed Instruction). Engineer Subcourse 64-9.

    ERIC Educational Resources Information Center

    Army Engineer School, Fort Belvoir, VA.

    The document is a programed text for a correspondence course in the planning, construction, and maintenance of military roads and airfields. There are seven lessons: construction requirements and design criteria; road reconnaissance and site selection; airfield reconnaissance and site selection; layout procedures, construction staking, and field…

  13. Recent Geological and Hydrological Activity in Amazonis and Elysium Basins and Their Link, Marte Valles (AME): Prime Target for Future Reconnaissance

    NASA Astrophysics Data System (ADS)

    Dohm, J. M.; Robbins, S. J.; Hynek, B. M.

    2012-03-01

    Amazonis and Elysium basins and their link, Marte Vallis (AME), uniquely point to a geologically and hydrologically active Mars. We will present evidence for why AME reconnaissance can help address whether Mars is geologically, hydrologically, and biologically active.

  14. Operational Space Weather in USAF Education

    NASA Astrophysics Data System (ADS)

    Smithtro, C.; Quigley, S.

    2006-12-01

    Most education programs offering space weather courses are understandably and traditionally heavily weighted with theoretical space physics that is the basis for most of what is researched and modeled. While understanding the theory is a good and necessary grounding for anyone working the field of space weather, few military or commercial jobs employ such theory in real-time operations. The operations sites/centers are much more geared toward use of applied theory-resultant models, tools and products. To ensure its operations centers personnel, commanders, real-time system operators and other customers affected by the space environment are educated on available and soon-to-be operational space weather models and products, the USAF has developed applicable course/lecture material taught at various institutions to include the Air Force Institute of Technology (AFIT) and the Joint Weather Training Complex (335th/TRS/OUA). Less frequent training of operational space weather is available via other venues that will be discussed, and associated course material is also being developed for potential use at the National Security Space Institute (NSSI). This presentation provides an overview of the programs, locations, courses and material developed and/or taught by or for USAF personnel dealing with operational space weather. It also provides general information on student research project results that may be used in operational support, along with observations regarding logistical and professional benefits of teaching such non-theoretical/non-traditional material.

  15. Standard of care of erectile dysfunction in U.S. Air Force aircrew and active duty not on flying status.

    PubMed

    Nast, Justin B

    2014-11-01

    In 2011, over 3,000 active duty U.S. Air Force (USAF) members were prescribed a phosphodiesterase inhibitor (PDEI). PDEIs are first-line therapy for treating erectile dysfunction and can have significant side effects that could impact aircrew performance. In total, 200 eligible subject records were randomly sampled from the active duty USAF population of those males filling a prescription for a PDEI in June 2011; 100 of those records were from aviators. The electronic records were reviewed and scored to determine if USAF aeromedical standards for prescribing PDEIs were followed, with a minimum score of 0 for no standards met and a maximum of 3 for all standards met. The average score for both groups was 1, with no significant difference between the group scores. A proper aeromedical disposition was documented in 67% of the aviator records. Although there was no significant difference in standard of care for aviators and nonaviators, the overall documented standard of care was poor. Lack of documentation was the primary reason for the low scores and the low percentage of properly rendered aeromedical dispositions. Proper medical record documentation is important for evaluating quality of care and ensuring compliance with regulations in an Air Force aviator population. Reprint & Copyright © 2014 Association of Military Surgeons of the U.S.

  16. Ecological risk assessment for Mather Air Force Base, California: Phase 1, screening assessment

    DOE Office of Scientific and Technical Information (OSTI.GOV)

    Meyers-Schoene, L.; Fischer, N.T.; Rabe, J.J.

    Mather Air Force Base (AFB) is among the numerous facilities scheduled for closure under the US Air Force (USAF) Installation Restoration Program (IRP). A component of the Mather AFB IRP is to prepare risk assessments for each of the chemically contaminated sites. Because no previous ecological risk related studies have been conducted on Mather AFB, the authors proposed a phased approach to assessing ecological risks at the base. Phase 1 consisted of baseline ecological surveys that collected data over a 12-month period. In addition, benchmark screening criteria were used in conjunction with modeling results that utilized measured concentrations of chemicalmore » analytes in abiotic samples. Phase 2 may consist of the collection of more site-specific data and toxicity testing, if warranted by the Phase 1 screening analysis. This approach was in agreement with the USAF`s ecological risk assessment guidance and met the approval of the Air Force and USEPA Region 9. The authors found the use of established and derived screening values to effectively aid in the focusing of the ecological risk assessment on those chemicals most likely to be hazardous to ecological receptors at the base. Disadvantages in the use of screening values include the uncertainties associated with the conservative assumptions inherent in the derivation of benchmark values and the difficulty in extrapolating from laboratory determined benchmark values to impacts in the field.« less

  17. Lunar Reconnaissance Orbiter Camera (LROC) instrument overview

    USGS Publications Warehouse

    Robinson, M.S.; Brylow, S.M.; Tschimmel, M.; Humm, D.; Lawrence, S.J.; Thomas, P.C.; Denevi, B.W.; Bowman-Cisneros, E.; Zerr, J.; Ravine, M.A.; Caplinger, M.A.; Ghaemi, F.T.; Schaffner, J.A.; Malin, M.C.; Mahanti, P.; Bartels, A.; Anderson, J.; Tran, T.N.; Eliason, E.M.; McEwen, A.S.; Turtle, E.; Jolliff, B.L.; Hiesinger, H.

    2010-01-01

    The Lunar Reconnaissance Orbiter Camera (LROC) Wide Angle Camera (WAC) and Narrow Angle Cameras (NACs) are on the NASA Lunar Reconnaissance Orbiter (LRO). The WAC is a 7-color push-frame camera (100 and 400 m/pixel visible and UV, respectively), while the two NACs are monochrome narrow-angle linescan imagers (0.5 m/pixel). The primary mission of LRO is to obtain measurements of the Moon that will enable future lunar human exploration. The overarching goals of the LROC investigation include landing site identification and certification, mapping of permanently polar shadowed and sunlit regions, meter-scale mapping of polar regions, global multispectral imaging, a global morphology base map, characterization of regolith properties, and determination of current impact hazards.

  18. Human exploration of Mars - The role of a Mars outpost laboratory

    NASA Technical Reports Server (NTRS)

    Duke, Michael B.

    1992-01-01

    Consideration is given to a Martian exploration strategy which includes intensive robotic reconnaissance to characterize features of Mars' geology that are important to the solution of major problems of Mars history, including the possible past presence of life. A human reconnaissance phase may follow the robotic reconnaissance phase, guided to the most productive sites by the results of the robotic missions. The strategy also involves an intensive human phase of investigation, with interactive field geology/laboratory investigation at the Mars outpost. The laboratory investigations, as well as the field work, should be highly interactive with a broad scientific community on earth. The most detailed analyses would be performed on samples returned to earth.

  19. Further ecological and shoreline stability reconnaissance surveys of Back Island, Behm Canal, Southeast Alaska

    DOE Office of Scientific and Technical Information (OSTI.GOV)

    Young, J.S.; Strand, J.A.; Ecker, R.M.

    1987-09-01

    A diver reconnaissance of the intertidal and subtidal zones of Back Island was performed to catalog potentially vulnerable shellfish, other invertebrates, and marine plant resources occurring at three proposed alternate pier sites on the west side of Back Island. Additionally, a limited survey of terrestrial vegetation was conducted in the vicinity of one of the proposed alternate pier sites to describe the littoral community and to list the dominant plant species found there. Finally, a reconnaissance survey of the shoreline of Back Island was conducted to evaluate potential changes in shoreline stability resulting from construction of onshore portions of themore » Southeast Alaska Acoustic Measurement Facility (SEAFAC).« less

  20. Hydrology reconnaissance of the Sink Valley area, Tooele and Box Elder Counties, Utah

    USGS Publications Warehouse

    Price, Don; Bolke, E.L.

    1970-01-01

    This is the sixth in a series of reports by the U.S. Geological Survey in cooperation with the Utah Department of Natural Resources, Division of Water Rights, which describe the water resources of selected basins in western Utah. Areas covered by previously published reports in this series are shown in figure 1 and are listed on page 29. The purpose of this report is to present available hydrologic data on the Sink Valley (Puddle Valley) area, to provide an evaluation of the potential for water-resource development in the area, and to serve as a basis for planning possible later detailed investigations.

  1. Hydrologic reconnaissance of Curlew Valley, Utah and Idaho

    USGS Publications Warehouse

    Bolke, E.L.; Price, Don

    1969-01-01

    This report is the fifth in a series of reports prepared by the U. S. Geological Survey in cooperation with the Utah Department of Natural Resources, Division of Water Rights, that describe the water resources of selected basins in western Utah. Previously published reports in this series are listed on page 35 and the areas covered by them are shown in figure 1. The purpose of this report is to present available hydrologic data on the Utah part of Curlew Valley, to provide an evaluation of the potential water-resource development of the valley, and to identify needed studies that would help provide an understanding of the valley's water supply.

  2. Texture, Carbonate Content, and Preliminary Maps of Surficial Sediments of the Flower Garden Banks Area, Northwestern Gulf of Mexico Outer Shelf

    USGS Publications Warehouse

    Scanlon, Kathryn M.; Ackerman, Seth D.; Rozycki, Jill E.

    2003-01-01

    The purpose of this report is to release texture and carbonate content analyses of 107 seafloor sediments collected within and near the East and West Flower Garden Banks areas of the Sanctuary and to show relationships between these data and existing bathymetric data. The sediment data, in conjunction with previously collected geological, geophysical and biological data were used to construct a reconnaissance-scale map of the distribution of seafloor sediment types. This map will be useful for resource managers and can be used, with additional data, as a basis for future habitat mapping.

  3. Notes on the geology of northeastern New Mexico

    USGS Publications Warehouse

    St. John, O.

    1876-01-01

    During the season of 1869, in the progress of his extended reconnaissance of the Rocky Mountains, Dr. Hayden visited this region, from whom we have authentic account of its general geological features, and their intimate relation to those prevailing in other and similar districts to the north and south. A few months' residence in this part of the country in 1874-'75* afforded the writer opportunity to become somewhat familiar with its geological features; and the purpose of the present communication is to present such facts as may tend to contribute something toward a similar knowledge of remote and perhaps hitherto rarely-visited localities, and their connection with already examined districts.

  4. Utilization of ERTS-1 data in geological evaluation, regional planning, forest management, and water management in North Carolina

    NASA Technical Reports Server (NTRS)

    Welby, C. W. (Principal Investigator); Lammi, J. O.; Carson, R. J., III

    1974-01-01

    The author has identified the following significant results. ERTS-1 imagery has been evaluated for use in resource planning and management in North Carolina, and found to be useful for general reconnaissance purposes in forestry, geology, and water resources work. It has also been used for studying large-scale transient phenomena such as river plumes and movement of sediment in the sounds. ERTS-1 imagery has been an aid to geologic and land-use mapping. Stereoscopes, projectors of various kinds, and microscopes have proved useful instruments for the kinds of data acquisition needed by resource planners and managers.

  5. 32 CFR 806.1 - Summary of revisions.

    Code of Federal Regulations, 2010 CFR

    2010-07-01

    ... Headquarters United States Air Force (HQ USAF/SC) and Headquarters Air Force Communications and Information Center/Corporate Information Division (HQ AFCIC/ITC); contains significant changes and additions to...

  6. 32 CFR 644.26 - Required clearances.

    Code of Federal Regulations, 2010 CFR

    2010-07-01

    ... Director of Engineering and Services (AF/PRE) and the Director of Planning, Programming and Analysis (AF/RDXI), as to industrial installations, of Headquarters, USAF, are responsible for initiating all...

  7. 32 CFR 644.26 - Required clearances.

    Code of Federal Regulations, 2012 CFR

    2012-07-01

    ... Director of Engineering and Services (AF/PRE) and the Director of Planning, Programming and Analysis (AF/RDXI), as to industrial installations, of Headquarters, USAF, are responsible for initiating all...

  8. 32 CFR 644.26 - Required clearances.

    Code of Federal Regulations, 2013 CFR

    2013-07-01

    ... Director of Engineering and Services (AF/PRE) and the Director of Planning, Programming and Analysis (AF/RDXI), as to industrial installations, of Headquarters, USAF, are responsible for initiating all...

  9. 32 CFR 644.26 - Required clearances.

    Code of Federal Regulations, 2014 CFR

    2014-07-01

    ... Director of Engineering and Services (AF/PRE) and the Director of Planning, Programming and Analysis (AF/RDXI), as to industrial installations, of Headquarters, USAF, are responsible for initiating all...

  10. 32 CFR 644.26 - Required clearances.

    Code of Federal Regulations, 2011 CFR

    2011-07-01

    ... Director of Engineering and Services (AF/PRE) and the Director of Planning, Programming and Analysis (AF/RDXI), as to industrial installations, of Headquarters, USAF, are responsible for initiating all...

  11. Intelligence Surveillance And Reconnaissance Full Motion Video Automatic Anomaly Detection Of Crowd Movements: System Requirements For Airborne Application

    DTIC Science & Technology

    The collection of Intelligence , Surveillance, and Reconnaissance (ISR) Full Motion Video (FMV) is growing at an exponential rate, and the manual... intelligence for the warfighter. This paper will address the question of how can automatic pattern extraction, based on computer vision, extract anomalies in

  12. Emerging Patterns in the Global Defense Industry

    DTIC Science & Technology

    2011-04-30

    vehicles developed for reconnaissance, or both reconnaissance and strike. We also attempt to place the rapid growth of UAVs in the U.S. inventory ...ORIGINS • Late 90s: S ecial n u p Operatio s Comm nity interested in man-portable UAV • FY 98-02 Military Operations in Urban Terrain ACTD

  13. The Information Edge: Imagery Intelligence and Geospatial Information in an Evolving National Security Environment

    DTIC Science & Technology

    2000-12-01

    8. PERFORMING ORGANIZATION REPORT NUMBER 9. SPONSORING/MONITORING AGENCY NAME(S) AND ADDRESS(ES) 10 . SPONSOR/MONITOR’S ACRONYM(S) 11. SPONSOR...Activities................................................................................ 48 10 . NIMA and Its Suppliers...Agency (DIA), the National Reconnaissance Office (NRO), the Defense Airborne Reconnaissance Office (DARO), and the Central Intelligence Agency” ibid. 10

  14. Publications - PIR 2011-1 | Alaska Division of Geological & Geophysical

    Science.gov Websites

    content DGGS PIR 2011-1 Publication Details Title: Reconnaissance evaluation of the Lake Clark fault Koehler, R.D., and Reger, R.D., 2011, Reconnaissance evaluation of the Lake Clark fault, Tyonek area M) Keywords Cook Inlet; Glacial Stratigraphy; Lake Clark Fault; Neotectonics; STATEMAP Project Top

  15. 33 CFR 240.8 - Credit criteria for projects authorized after 17 November 1986.

    Code of Federal Regulations, 2010 CFR

    2010-07-01

    ..., work eligible for credit will be explicitly addressed in recommendations to Congress. If a report has... within 5 years before the first obligation of funds for the reconnaissance study began, whichever is..., credit can be considered only for local work undertaken after the end of the reconnaissance study and for...

  16. 33 CFR 240.8 - Credit criteria for projects authorized after 17 November 1986.

    Code of Federal Regulations, 2011 CFR

    2011-07-01

    ..., work eligible for credit will be explicitly addressed in recommendations to Congress. If a report has... within 5 years before the first obligation of funds for the reconnaissance study began, whichever is..., credit can be considered only for local work undertaken after the end of the reconnaissance study and for...

  17. Publications - RI 2000-1C | Alaska Division of Geological & Geophysical

    Science.gov Websites

    Sagavanirktok B-1 Quadrangle, eastern North Slope, Alaska Authors: Pinney, D.S. Publication Date: 2000 Publisher Bibliographic Reference Pinney, D.S., 2000, Reconnaissance surficial-geologic map of the Sagavanirktok B-1 Sheets Sheet 1 Reconnaissance surficial-geologic map of the Sagavanirktok B-1 Quadrangle, eastern North

  18. A Man-in-the-Loop Support Concept for Military Ambush Threat-Assessment Based on Reconnaissance Reports

    DTIC Science & Technology

    2004-03-01

    On all levels of the military command hierarchy there is a strong demand for support through the automated processing of reconnaissance reports. This...preconditions for the improvement of computer support and then illustrates the automated processing of report information using a military ambush situation in

  19. Advanced Pattern Recognition Techniques (Techniques avancees de reconnaissance de forme)

    DTIC Science & Technology

    1998-09-01

    alarmes dans la d6tection des mines terrestres et des munitions explosives non explos6es. Les m~thodes classiques de reconnaissance de forme...the XVIII. Congress of the International Society for [19] DIN EN 60825-1(IEC 825-1) VDE 0837, Photogrammetry and Remote Sensing Sicherheit von Laser

  20. Lunar Reconnaissance Orbiter Contamination Sensitivity Training

    NASA Technical Reports Server (NTRS)

    Rivera, Rachel

    2007-01-01

    The following packet is a contamination control training intended for personnel handling or coming to contact with Lunar Reconnaissance Or biter (LRO) flight hardware. This training is being implemented to f amiliarize personnel, coming into contact with LRO hardware, what its contamination sensitivities are and what can be done by all to maint ain its cleanliness levels.

  1. Lunar Reconnaissance Orbiter Artist Concept

    NASA Image and Video Library

    2008-07-24

    Artist rendering of the Lunar Reconnaissance Orbiter LRO, above the moon. LRO carries seven instruments that make comprehensive remote sensing observations of the moon and measurements of the lunar radiation environment. The LRO mission is managed by NASA Goddard for the Science Mission Directorate at NASA Headquarters in Washington. http://photojournal.jpl.nasa.gov/catalog/PIA18163

  2. Tier-scalable reconnaissance: the challenge of sensor optimization, sensor deployment, sensor fusion, and sensor interoperability

    NASA Astrophysics Data System (ADS)

    Fink, Wolfgang; George, Thomas; Tarbell, Mark A.

    2007-04-01

    Robotic reconnaissance operations are called for in extreme environments, not only those such as space, including planetary atmospheres, surfaces, and subsurfaces, but also in potentially hazardous or inaccessible operational areas on Earth, such as mine fields, battlefield environments, enemy occupied territories, terrorist infiltrated environments, or areas that have been exposed to biochemical agents or radiation. Real time reconnaissance enables the identification and characterization of transient events. A fundamentally new mission concept for tier-scalable reconnaissance of operational areas, originated by Fink et al., is aimed at replacing the engineering and safety constrained mission designs of the past. The tier-scalable paradigm integrates multi-tier (orbit atmosphere surface/subsurface) and multi-agent (satellite UAV/blimp surface/subsurface sensing platforms) hierarchical mission architectures, introducing not only mission redundancy and safety, but also enabling and optimizing intelligent, less constrained, and distributed reconnaissance in real time. Given the mass, size, and power constraints faced by such a multi-platform approach, this is an ideal application scenario for a diverse set of MEMS sensors. To support such mission architectures, a high degree of operational autonomy is required. Essential elements of such operational autonomy are: (1) automatic mapping of an operational area from different vantage points (including vehicle health monitoring); (2) automatic feature extraction and target/region-of-interest identification within the mapped operational area; and (3) automatic target prioritization for close-up examination. These requirements imply the optimal deployment of MEMS sensors and sensor platforms, sensor fusion, and sensor interoperability.

  3. 2. Credit USAF, ca. 1945. Original housed in the Records ...

    Library of Congress Historic Buildings Survey, Historic Engineering Record, Historic Landscapes Survey

    2. Credit USAF, ca. 1945. Original housed in the Records of the Defense Intelligence Agency. Record Group 373. National Archives. Cartographic and Architectural Branch. Washington, D.C. Oblique aerial photo 16PS5M79-1-0-48-4:3:1152:12:120003500N11745W looking roughly north northeast across North Base from a position over Rogers Dry Lake. Largest structures are hangars, beginning with Building 4305 (Unicon Portable Hangar) at view center and continuing to right with Buildings 4401 and 4402 (Type HANG-N-A hangars), with Building 4505 (Type HANG-P-A hangar) in the distance. Bachelor Officers' Quarters known as the "Desert Rat Hotel" (T-l) was located adjacent to Building 4305. - Edwards Air Force Base, North Base, North Base Road, Boron, Kern County, CA

  4. Seventh Annual Workshop on Space Operations Applications and Research (SOAR 1993), volume 1

    NASA Technical Reports Server (NTRS)

    Krishen, Kumar (Editor)

    1994-01-01

    This document contains papers presented at the Space Operations, Applications and Research Symposium (SOAR) Symposium hosted by NASA/Johnson Space Center (JSC) on August 3-5, 1993, and held at JSC Gilruth Recreation Center. SOAR included NASA and USAF programmatic overview, plenary session, panel discussions, panel sessions, and exhibits. It invited technical papers in support of U.S. Army, U.S. Navy, Department of Energy, NASA, and USAF programs in the following areas: robotics and telepresence, automation and intelligent systems, human factors, life support, and space maintenance and servicing. SOAR was concerned with Government-sponsored research and development relevant to aerospace operations. More than 100 technical papers, 17 exhibits, a plenary session, several panel discussions, and several keynote speeches were included in SOAR '93.

  5. NASA Conjunction Assessment Organizational Approach and the Associated Determination of Screening Volume Sizes

    NASA Technical Reports Server (NTRS)

    Newman, Lauri K.; Hejduk, Matthew D.

    2015-01-01

    NASA is committed to safety of flight for all of its operational assets Performed by CARA at NASA GSFC for robotic satellites Focus of this briefing Performed by TOPO at NASA JSC for human spaceflight he Conjunction Assessment Risk Analysis (CARA) was stood up to offer this service to all NASA robotic satellites Currently provides service to 70 operational satellites NASA unmanned operational assets Other USG assets (USGS, USAF, NOAA) International partner assets Conjunction Assessment (CA) is the process of identifying close approaches between two orbiting objects; sometimes called conjunction screening The Joint Space Operations Center (JSpOC) a USAF unit at Vandenberg AFB, maintains the high accuracy catalog of space objects, screens CARA-supported assets against the catalog, performs OD tasking, and generates close approach data.

  6. Operation REDWING 1956

    DTIC Science & Technology

    1982-08-01

    AIRCRAFT UNIT Hq TAU 2 0 1 0 Eniwetok Is. 20 Mar Hq USAF Elm 0 4 0 0 Eniwetok Is. 30 Apr Hq USAF Elm 4 3 2 0 Parry Is. 30 Apr 4g Drop & Cann Elm 15 41 0...0 Eniwrv k Is. 1 5-36 16 Mar i 4 2 5-52 mqý Effects Elm 14 7 8 53 Eniwecck Is. 1 B-52 21 Mar 1 B-47 I B-57 1 B-66 2 F-84F 1 F-101 IBDA Elm 11 35 0 0...Eniwetok Is. 3 B-47 30 Apr Ionosphere Elm 6 12 0 0 Eniwetok Is. 1 C-97 30 Apr * "Navy Effects Elm 8 31 13 0 I A3D "I P2V Early Pe.ietr Elm 16 40 0 0

  7. Weather forecasting expert system study

    NASA Technical Reports Server (NTRS)

    1985-01-01

    Weather forecasting is critical to both the Space Transportation System (STS) ground operations and the launch/landing activities at NASA Kennedy Space Center (KSC). The current launch frequency places significant demands on the USAF weather forecasters at the Cape Canaveral Forecasting Facility (CCFF), who currently provide the weather forecasting for all STS operations. As launch frequency increases, KSC's weather forecasting problems will be great magnified. The single most important problem is the shortage of highly skilled forecasting personnel. The development of forecasting expertise is difficult and requires several years of experience. Frequent personnel changes within the forecasting staff jeopardize the accumulation and retention of experience-based weather forecasting expertise. The primary purpose of this project was to assess the feasibility of using Artificial Intelligence (AI) techniques to ameliorate this shortage of experts by capturing aria incorporating the forecasting knowledge of current expert forecasters into a Weather Forecasting Expert System (WFES) which would then be made available to less experienced duty forecasters.

  8. USAF bioenvironmental noise data handbook. Volume 163: GPC-28 compressor

    NASA Astrophysics Data System (ADS)

    Rau, T. H.

    1982-05-01

    The GPC-28 is a gasoline engine-driven compressor with a 120 volt 60 Hz generator used for general purpose maintenance. This report provides measured and extrapolated data defining the bioacoustic environments produced by this unit operating outdoors on a concrete apron at a normal rated condition. Near-field data are reported for 37 locations in a wide variety of physical and psychoacoustic measures: overall and band sound pressure levels, C-weighted and A-weighted sound levels, preferred speech interference level, perceived noise level, and limiting times for total daily exposure of personnel with and without standard Air Force ear protectors. Far-field data measured at 36 locations are normalized to standard meteorological conditions and extrapolated from 10 - 1600 meters to derive sets of equal-value contours for these same seven acoustic measures as functions of angle and distance from the source.

  9. Aircraft measurements of electrified clouds at Kennedy Space Center, part 3

    NASA Technical Reports Server (NTRS)

    Jones, J. J.; Winn, W. P.; Hunyady, S. J.; Moore, C. B.; Bullock, J. W.; Fleischhacker, P.

    1990-01-01

    Flights made by the Special Purpose Test Vehicle for Atmospheric Research (SPTVAR) airplane during a second deployment to Florida during the summer of 1989 are discussed. The findings based on the data gathered are presented. The progress made during the second year of the project is discussed. The summer 1989 study was carried out with the support and guidance of Col. John Madura, Commander of Detachment 11, 2nd Weather Squadron, USAF, at Patrick Air Force Base (PAFB) and Cape Canaveral Air Force Station. The project goals were to develop and demonstrate techniques for measuring the electric field aloft and locating regions of charge during flight within and near clouds; to characterize the electric conditions that are presently identified as a threat to space launch vehicles; and to study the correlation between the electric field aloft and that at Kennedy Space Center's ground-based electric field mill array for a variety of electrified clouds.

  10. 32 CFR 813.3 - Responsibilities.

    Code of Federal Regulations, 2010 CFR

    2010-07-01

    ... component and joint commands with deliberate and crisis action planning for USAF's COMCAM assets. (6... and 2, and AFI 31-401, Information Security Program Management. The authority in charge of the event...

  11. Satellite Vulnerabilities

    DTIC Science & Technology

    2008-02-18

    allies. 8  Satellites and Intelligence , Surveillance, and Reconnaissance We have become dependent also on our satellite surveillance assets...uninterrupted ISR”, with “space intelligence , surveillance, and reconnaissance (ISR) systems…fundamental to air power—especially to the execution...tremendous informational and intelligence advantage. But if we lose those satellites, or the links to them, we also lose the advantages of them, and

  12. Reconnaissance blind multi-chess: an experimentation platform for ISR sensor fusion and resource management

    NASA Astrophysics Data System (ADS)

    Newman, Andrew J.; Richardson, Casey L.; Kain, Sean M.; Stankiewicz, Paul G.; Guseman, Paul R.; Schreurs, Blake A.; Dunne, Jeffrey A.

    2016-05-01

    This paper introduces the game of reconnaissance blind multi-chess (RBMC) as a paradigm and test bed for understanding and experimenting with autonomous decision making under uncertainty and in particular managing a network of heterogeneous Intelligence, Surveillance and Reconnaissance (ISR) sensors to maintain situational awareness informing tactical and strategic decision making. The intent is for RBMC to serve as a common reference or challenge problem in fusion and resource management of heterogeneous sensor ensembles across diverse mission areas. We have defined a basic rule set and a framework for creating more complex versions, developed a web-based software realization to serve as an experimentation platform, and developed some initial machine intelligence approaches to playing it.

  13. Reconnaissance techniques for determining soil-gas radon concentrations: an example from Prince Georges County, Maryland

    USGS Publications Warehouse

    Reimer, G.M.

    1990-01-01

    Radon reconnaissance requires some special considerations because a large area must be covered in a short period of time and analyses must be made soon after collection because of Rn decay. A simple approach to collection and field analysis consists of a small-diameter probe pounded into the ground to a depth of at least 0.75 m. Analysis is by an alpha-scintillometer. Soil-gas samples collected along a traverse in Prince Georges County, Maryland, demonstrates the utility of the technique. The reconnaissance sampling revealed Rn soil-gas concentrations of up to 2500 pCi/L (picocuries per liter) indicating that the potential exists for indoor accumulations in excess of 4 pCi/L. -from Author

  14. The mineral resource potential of the Wadi Habawnah and Najran quadrangles, sheets 17/44A and 17/44C, Kingdom of Saudi Arabia

    USGS Publications Warehouse

    Fenton, Michael D.

    1983-01-01

    The metallic resource potential of the Wadi Habawnah and Najran quadrangles in the southern Precambrian Arabian Shield has been determined primarily by reconnaissance rock geochemistry, limited wadi-sediment and colluvium geochemistry, and gossanous and ferruginous outcrop geochemistry. These surveys were guided by geological information acquired during previous reconnaissance mapping. Locally anomalous areas in alkalic and calc-alkalic granitic terrane are possible sources of niobium-zirconiumthorium-fluorite, tin-tungsten, and copper-molybdenum, although the potential of these areas does not appear to be outstanding. The reconnaissance geochemistry of the layered volcanic terrane and the geochemistry of gossanous and ferruginous outcrops indicate that the potential for stratiform base metal sulfide deposits is low.

  15. NASA Weather Support 2017

    NASA Technical Reports Server (NTRS)

    Carroll, Matt

    2017-01-01

    In the mid to late 1980's, as NASA was studying ways to improve weather forecasting capabilities to reduce excessive weather launch delays and to reduce excessive weather Launch Commit Criteria (LCC) waivers, the Challenger Accident occurred and the AC-67 Mishap occurred.[1] NASA and USAF weather personnel had advance knowledge of extremely high levels of weather hazards that ultimately caused or contributed to both of these accidents. In both cases, key knowledge of the risks posed by violations of weather LCC was not in the possession of final decision makers on the launch teams. In addition to convening the mishap boards for these two lost missions, NASA convened expert meteorological boards focusing on weather support. These meteorological boards recommended the development of a dedicated organization with the highest levels of weather expertise and influence to support all of American spaceflight. NASA immediately established the Weather Support Office (WSO) in the Office of Space Flight (OSF), and in coordination with the United Stated Air Force (USAF), initiated an overhaul of the organization and an improvement in technology used for weather support as recommended. Soon after, the USAF established a senior civilian Launch Weather Officer (LWO) position to provide meteorological support and continuity of weather expertise and knowledge over time. The Applied Meteorology Unit (AMU) was established by NASA, USAF, and the National Weather Service to support initiatives to place new tools and methods into an operational status. At the end of the Shuttle Program, after several weather office reorganizations, the WSO function had been assigned to a weather branch at Kennedy Space Center (KSC). This branch was dismantled in steps due to further reorganization, loss of key personnel, and loss of budget line authority. NASA is facing the loss of sufficient expertise and leadership required to provide current levels of weather support. The recommendation proposed herein is to re-establish the WSO under a high level office, with funding set at about the same levels as today, with a revitalized charter and focus to allow for the WSO to operate as originally intended.

  16. 32 CFR 865.105 - Jurisdiction and authority.

    Code of Federal Regulations, 2010 CFR

    2010-07-01

    ... DRB instructs the USAF Manpower and Personnel Center (AFMPC) to change the discharge reason or to... to result in a decision favorable to the former military member, without the member's knowledge or...

  17. 32 CFR 865.105 - Jurisdiction and authority.

    Code of Federal Regulations, 2012 CFR

    2012-07-01

    ... DRB instructs the USAF Manpower and Personnel Center (AFMPC) to change the discharge reason or to... to result in a decision favorable to the former military member, without the member's knowledge or...

  18. 32 CFR 865.105 - Jurisdiction and authority.

    Code of Federal Regulations, 2014 CFR

    2014-07-01

    ... DRB instructs the USAF Manpower and Personnel Center (AFMPC) to change the discharge reason or to... to result in a decision favorable to the former military member, without the member's knowledge or...

  19. 32 CFR 865.105 - Jurisdiction and authority.

    Code of Federal Regulations, 2011 CFR

    2011-07-01

    ... DRB instructs the USAF Manpower and Personnel Center (AFMPC) to change the discharge reason or to... to result in a decision favorable to the former military member, without the member's knowledge or...

  20. 32 CFR 865.105 - Jurisdiction and authority.

    Code of Federal Regulations, 2013 CFR

    2013-07-01

    ... DRB instructs the USAF Manpower and Personnel Center (AFMPC) to change the discharge reason or to... to result in a decision favorable to the former military member, without the member's knowledge or...

  1. Evaluation of airborne thermal infrared imagery for locating mine drainage sites in the Lower Kettle Creek and Cooks Run Basins, Pennsylvania, USA

    USGS Publications Warehouse

    Sams, James I.; Veloski, Garret

    2003-01-01

    High-resolution airborne thermal infrared (TIR) imagery data were collected over 90.6 km2 (35 mi2) of remote and rugged terrain in the Kettle Creek and Cooks Run Basins, tributaries of the West Branch of the Susquehanna River in north-central Pennsylvania. The purpose of this investigation was to evaluate the effectiveness of TIR for identifying sources of acid mine drainage (AMD) associated with abandoned coal mines. Coal mining from the late 1800s resulted in many AMD sources from abandoned mines in the area. However, very little detailed mine information was available, particularly on the source locations of AMD sites. Potential AMD sources were extracted from airborne TIR data employing custom image processing algorithms and GIS data analysis. Based on field reconnaissance of 103 TIR anomalies, 53 sites (51%) were classified as AMD. The AMD sources had low pH (<4) and elevated concentrations of iron and aluminum. Of the 53 sites, approximately 26 sites could be correlated with sites previously documented as AMD. The other 27 mine discharges identified in the TIR data were previously undocumented. This paper presents a summary of the procedures used to process the TIR data and extract potential mine drainage sites, methods used for field reconnaissance and verification of TIR data, and a brief summary of water-quality data.

  2. Reconnaissance investigation of the alluvial gold deposits in the North Takhar Area of Interest, Takhar Province, Afghanistan

    USGS Publications Warehouse

    Chirico, Peter G.; Malpeli, Katherine C.; Moran, Thomas W.

    2013-01-01

    This study is a reconnaissance assessment of the alluvial gold deposits of the North Takhar Area of Interest (AOI) in Takhar Province, Afghanistan. Soviet and Afghan geologists collected data and calculated the gold deposit reserves in Takhar Province in the 1970s, prior to the development of satellite-based remote-sensing platforms and new methods of geomorphic mapping. The purpose of this study was to integrate new mapping techniques with previously collected borehole sampling and concentration sampling data and geomorphologic interpretations to reassess the alluvial gold placer deposits in the North Takhar AOI. Through a combination of historical borehole and cross-section data and digital terrain modeling, the Samti, Nooraba-Khasar-Anjir, and Kocha River placer deposits were reassessed. Resource estimates were calculated to be 20,927 kilograms (kg) for Samti, 7,626 kg for Nooraba-Khasar-Anjir, 160 kg for the mouth of the Kocha, 1,047 kg for the lower Kocha, 113 kg for the middle Kocha, and 168 kg for the upper Kocha. Previous resource estimates conducted by the Soviets for the Samti and Nooraba-Khasar-Anjir deposits estimated 30,062 kg and 802 kg of gold, respectively. This difference between the new estimates and previous estimates results from the higher resolution geomorphic model and the interpretation of areas outside of the initial work zone studied by Soviet and Afghan geologists.

  3. A water-quality reconnaissance of Big Bear Lake, San Bernardino County, California, 1972-1973

    USGS Publications Warehouse

    Irwin, George A.; Lemons, Michael

    1974-01-01

    A water-quality reconnaissance study of the Big Bear Lake area in southern California was made by the U.S. Geological Survey from April 1972 through April 1973. The primary purpose of the study was to measure the concentration and distribution of selected primary nutrients, organic carbon, dissolved oxygen, phytoplankton, and water temperature in the lake. Estimates of the nitrogen, phosphorus, and silica loading to the lake from surface-water tributaries and precipitation were also made.Results of the study indicate that Big Bear Lake is moderately eutrophic, at least in regard to nitrogen, phosphorus, and organic content. Nitrate was found in either trace concentrations or below detectable limits; however, ammonia nitrogen was usually detected in concentrations greater than 0.05 milligrams per liter. Orthophosphate phosphorus was detected in mean concentrations ranging from 0.01 to 0.05 milligrams per liter. Organic nitrogen and phosphorus were also detected in measurable concentrations.Seasonal levels of dissolved oxygen indicated that the nutrients and other controlling factors were optimum for relatively high primary productivity. However, production varied both seasonally and areally in the lake. Primary productivity seemed highest in the eastern and middle parts of the lake. The middle and western parts of the lake exhibited severe oxygen deficits in the deeper water during the warmer summer months of June and July 1972.

  4. A bacterial enrichment study and overview of the extractable lipids from paleosols in the Dry Valleys, Antarctica: implications for future Mars reconnaissance.

    PubMed

    Hart, Kris M; Szpak, Michal T; Mahaney, William C; Dohm, James M; Jordan, Sean F; Frazer, Andrew R; Allen, Christopher C R; Kelleher, Brian P

    2011-05-01

    The Dry Valleys of Antarctica are one of the coldest and driest environments on Earth with paleosols in selected areas that date to the emplacement of tills by warm-based ice during the Early Miocene. Cited as an analogue to the martian surface, the ability of the Antarctic environment to support microbial life-forms is a matter of special interest, particularly with the upcoming NASA/ESA 2018 ExoMars mission. Lipid biomarkers were extracted and analyzed by gas chromatography--mass spectrometry to assess sources of organic carbon and evaluate the contribution of microbial species to the organic matter of the paleosols. Paleosol samples from the ice-free Dry Valleys were also subsampled and cultivated in a growth medium from which DNA was extracted with the explicit purpose of the positive identification of bacteria. Several species of bacteria were grown in solution and the genus identified. A similar match of the data to sequenced DNA showed that Alphaproteobacteria, Gammaproteobacteria, Bacteriodetes, and Actinobacteridae species were cultivated. The results confirm the presence of bacteria within some paleosols, but no assumptions have been made with regard to in situ activity at present. These results underscore the need not only to further investigate Dry Valley cryosols but also to develop reconnaissance strategies to determine whether such likely Earth-like environments on the Red Planet also contain life.

  5. Reconnaissance investigation of the placer gold deposits in the Zarkashan Area of Interest, Ghazni Province, Afghanistan

    USGS Publications Warehouse

    Malpeli, Katherine C.; Chirico, Peter G.; McLoughlin, Isabel H.

    2013-01-01

    This study is a reconnaissance investigation of the placer gold deposits in the Zarkashan Area of Interest (AOI) in Ghazni Province, Afghanistan. Detailed investigations of the Zarkashan gold deposits were conducted by Soviet and Afghan geologists in the 1960s and 1970s, prior to the development of satellite-based remote-sensing platforms and new methods of geomorphic mapping. The purpose of this study was to integrate new mapping techniques with previously collected concentration and borehole sampling data and geomorphologic interpretations to reassess the placer gold deposits in the Zarkashan AOI. A methodology combining the collection and analysis of historical sampling data, digital database development, hydrologic analysis, and geomorphic modeling was used. The analysis led to the reinterpretation of four gold-bearing seams along the Zarkashan River, and the calculation of an estimated gold reserve of approximately 3,000 kilograms (kg). This estimate is approximately 1,500 kg greater than the Soviet estimate. The result differs in large part due to the reinterpretation of the seams based on a much lower cutoff grade of 100 mg/m3. Because cutoff grade is dependent in part on the price of gold, the sevenfold increase in the price of gold since the undertaking of the Soviet investigation warranted our re-evaluation of their 500 mg/m3 cutoff grade.

  6. 32 CFR 644.27 - Authority to issue Real Estate Directives.

    Code of Federal Regulations, 2011 CFR

    2011-07-01

    ... Department of the Army policies, excepting the acquisition by lease of industrial and commercial facilities..., Directorate of Engineering and Services, HQ, USAF. Major Air Commands and Air Force Regional Civil Engineers...

  7. 78 FR 34047 - Takes of Marine Mammals Incidental to Specified Activities; Navy Research, Development, Test and...

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-06-06

    ... observe the area when the system is undergoing a small track close to the support platform. (2) Operating... the An/AQS-20A Mine Reconnaissance Sonar System in the NSWC PCD Testing Range, 2012-2014,'' which is... incidental to conducting testing of the AN/AQS- 20A Mine Reconnaissance Sonar System (hereafter referred to...

  8. Magnificent Mars 10 Years of Mars Reconnaissance Orbiter

    NASA Image and Video Library

    2016-03-09

    NASA's Mars Reconnaissance Orbiter has clocked more than a decade of service at the Red Planet and has yielded scientific discoveries and magnificent views of a distant world. Video uses spacecraft animation and stills set to music. These images taken by MRO's HiRISE camera are not in true color because they include infrared information in order to be optimized for geological science.

  9. Publications - PIR 2015-5-5 | Alaska Division of Geological & Geophysical

    Science.gov Websites

    ., 2015, Stratigraphic reconnaissance of the Middle Jurassic Red Glacier Formation, Tuxedni Group, at Red Surveys Skip to content State of Alaska myAlaska My Government Resident Business in Alaska content DGGS PIR 2015-5-5 Publication Details Title: Stratigraphic reconnaissance of the Middle Jurassic

  10. Reconnaissance-Pul - Seeking the Path of Least Resistance

    DTIC Science & Technology

    1990-12-15

    Carl von Clausewitz, the great eighteenth century military theorist, also professed pitting friendly strength against enemy weakness. Addressing "the...izortance of reconnaissance, its relation to intelligence, and the advantage of pitting friendly strength against enemy weaknesses. The Soviets use a...64. Ibid. 65. Vasily Gerasimovich Reznichenko, "Taktika" (Tactics), translated by Foreign Broadcast Information Service (Moscow, 1988):p.55. 66

  11. Memorandum on ground-water conditions in parts of Tps. 10 and 11 S., Rs. 23 and 24 W., Yuma County, Arizona

    USGS Publications Warehouse

    Johnson, P.W.

    1954-01-01

    In response to a request from J.R. Burger, Acting State Land Commissioner, dated September 24, 1953, a brief reconnaissance was made of ground-water conditions in southwestern Yuma County, Ariz.  This memorandum is based on the reconnaissance and on review of data available from other agencies.

  12. Army National Guard Companies Have Not Developed Effective Training Programs to Attain or Sustain Mission Essential Task Proficiency (REDACTED)

    DTIC Science & Technology

    2016-12-05

    consist of at least five company -level units: headquarters , two rifle, and two armored units. Reconnaissance squadrons generally consist of at...least four company - level units: headquarters and three reconnaissance units...Brief (U) Army National Guard Companies Have Not Developed Effective Training Programs to Attain or Sustain Mission Essential Task Proficiency

  13. Apache Aviator Evaluation of Dual-Technology Night Vision Systems in Operation Iraqi Freedom (OIF) Urban Combat (Master’s Thesis)

    DTIC Science & Technology

    2008-01-01

    figure 7), this range allowing for both near and far IR. In essence, the system allows the pilot to see what is normally invisible to the naked eye. 8...contributed to the mid- teen percentage (15.8%) preference for its use during reconnaissance operations. To help qualify preference for reconnaissance

  14. Air Force Logistics Command (AFLC) solar thermal plant

    NASA Technical Reports Server (NTRS)

    1983-01-01

    The plant proved its capability to deliver the desired energy product in a USAF industrial environment. The collector proved capable of energy conversion at insolation levels up to 25% below design minimum. The plant and the project were negatively affected by severe winter weather, with total insolation during the test period 60 percent less than the expected value. Environmental effects reduced plant availability to 55 percent. Only five, minimally good operating days were experienced during the test period. The subsequent lack of performance data prohibits the drawing of general conclusions regarding system performance. System operability was rated generally high. The only inhibiting factor was the difficulty in procuring replacement parts for rapid repair under USAF stockage and procurement policies. No inherently serious system failures were recorded, although a thermostatic valve malfunction in the freeze protection system ultimately took 30 days to repair.

  15. The NASA/USAF arcjet research and technology program

    NASA Technical Reports Server (NTRS)

    Stone, James R.; Huston, Edward S.

    1987-01-01

    Direct current arcjets have the potential to provide specific impulses greater than 500 sec with storable propellants, and greater than 1000 sec with hydrogen. This level of performance can provide significant benefits for such applications as orbit transfer, station keeping, orbit change, and maneuvering. The simplicity of the arcjet system and its elements of commonality with state-of-the-art resistojet systems offer a relatively low risk transition to these enhanced levels of performance for low power (0.5 to 1.5 kW) station keeping applications. Arcjets at power levels of 10 to 30 kW are potentially applicable to orbit transfer missions. Furthermore, with the anticipated development of space nuclear power systems, arcjets at greater than 100 kW may become attractive. This paper describes the ongoing NASA/USAF program and describes major recent accomplishments.

  16. A Review of Hydrazine Sensors: The State of the Art

    NASA Technical Reports Server (NTRS)

    Meneghelli, B. J.

    2004-01-01

    Several types of sensors have been developed over the past few years that quantify the vapor concentrations of the hydrazines. These sensor s are able to detect concentrations as low as 10 parts per billion (ppb) up to several parts per million (ppm). The scope of this review wi ll be focused on those sensors that are most current in the marketpla ce as either leak detectors or personnel monitors. Some technical information on the theory of operations of each hydrazine detector will a lso be included. The review will highlight current operations that utilize hydrazine sensors including the Kennedy Space Center (KSC), the United States Air Force (USAF) at Cape Canaveral Air Station (CCAS), USAF F-16 facilities. The orientation of the review will be towards giving users usable practical information on hydrazine sensors.

  17. OSSE Evaluation of Aircraft Reconnaissance Observations and their Impact on Hurricane Analyses and Forecasts

    NASA Astrophysics Data System (ADS)

    Ryan, K. E.; Bucci, L. R.; Delgado, J.; Atlas, R. M.; Murillo, S.; Dodge, P.

    2016-12-01

    NOAA/AOML's Hurricane Research Division (HRD) annually conducts its Hurricane Field Program during which observations are collected via NOAA aircraft to improve the understanding and prediction of hurricanes. Mission experiments suggest a variety of flight patterns and sampling strategies aimed towards their respective goals described by the Intensity Forecasting Experiment (IFEX; Rogers et al., BAMS, 2006, 2013), a collaborative effort among HRD, NHC, and EMC. Evaluating the potential impact of various trade-offs in track design is valuable for determining the optimal air reconnaissance flight pattern for a prospective mission. AOML's HRD has developed a system for performing regional Observing System Simulation Experiments (OSSEs) to assess the potential impact of proposed observing systems on hurricane track and intensity forecasts and analyses. This study focuses on investigating the potential impact of proposed aircraft reconnaissance observing system designs. Aircraft instrument and flight level retrievals were simulated from a regional WRF ARW Nature Run (Nolan et al., 2013) spanning 13 days, covering the life cycle of a rapidly intensifying Atlantic tropical cyclone. The aircraft trajectories of NOAA aircraft are simulated in a variety of ways and are evaluated to examine the potential impact of aircraft reconnaissance observations on hurricane track and intensity forecasts.

  18. OSSE Evaluation of Prospective Aircraft Reconnaissance Flight Patterns and their Impact on Hurricane Forecasts

    NASA Astrophysics Data System (ADS)

    Ryan, K. E.; Bucci, L. R.; Christophersen, H.; Atlas, R. M.; Murillo, S.; Dodge, P.

    2015-12-01

    Each year, NOAA/AOML's Hurricane Research Division (HRD) conducts its Hurricane field Program in which observations are collected via NOAA aircraft to improve the understanding and prediction of hurricanes. Mission experiments suggest a variety of flight patterns and sampling strategies aimed towards their respective goals described by the Intensity Forecasting Experiment (IFEX; Rogers et al., BAMS, 2006, 2013), a collaborative effort among HRD, NHC, and EMC. Evaluating the potential impact of various trade-offs in design is valuable for determining the optimal air reconnaissance flight pattern for a given prospective mission. AOML's HRD has developed a system for performing regional Observing System Simulation Experiments (OSSEs) to assess the potential impact of proposed observing systems on hurricane track and intensity forecasts and analyses. This study focuses on investigating the potential impact of proposed aircraft reconnaissance observing system designs. Aircraft instrument and flight level retrievals were simulated from a regional WRF ARW Nature Run (Nolan et al., 2013) spanning 13 days, covering the life cycle of a rapidly intensifying Atlantic tropical cyclone. The aircraft trajectories are simulated in a variety of ways and are evaluated to investigate the potential impact of aircraft reconnaissance observations on hurricane track and intensity forecasts.

  19. Multi-Temporal Analysis of WWII Reconnaissance Photos

    NASA Astrophysics Data System (ADS)

    Meixner, P.; Eckstein, M.

    2016-06-01

    There are millions of aerial photographs from the period of the Second Wold War available in the Allied archives, obtained by aerial photo reconnaissance, covering most of today's European countries. They are spanning the time from 1938 until the end of the war and even beyond. Photo reconnaissance provided intelligence information for the Allied headquarters and accompanied the bombing offensive against the German homeland and the occupied territories. One of the initial principal targets in Bohemia were the synthetized fuel works STW AG (Sudetenländische Treibstoffwerke AG) in Zaluzi (formerly Maltheuren) near Most (formerly Brück), Czech Republic. The STW AG synthetized fuel plant was not only subject to bombing raids, but a subject to quite intensive photo reconnaissance, too - long before the start of the bombing campaign. With a multi-temporal analysis of the available imagery from international archives we will demonstrate the factory build-up during 1942 and 1943, the effects of the bombing raids in 1944 and the struggle to keep the plant working in the last year of the war. Furthermore we would like to show the impact the bombings have today, in form of potential unexploded ordnance in the adjacent area of the open cast mines.

  20. Reconnaissance geologic mapping of a portion of the rain‐forest‐covered Guiana Shield, Northwestern Brazil, using SIR-B and digital aeromagnetic data

    USGS Publications Warehouse

    Pellon de Miranda, Fernando; McCafferty, Anne E.; Taranik, James V.

    1994-01-01

    This paper documents the result of an integrated analysis of spaceborne radar (SIR-B) and digital aeromagnetic data carried out in the heavily forested Guiana Shield. The objective of the research is to interpret the geophysical data base to its limit to produce a reconnaissance geologic map as an aid to ground work planning in a worst‐case setting. Linear geomorphic features were identified based on the interpretation of the SIR-B image. Digital manipulation of aeromagnetic data allowed the development of a color‐shaded relief map of reduced‐to‐pole magnetic anomalies, a terrace‐magnetization map, and a map showing the location of maximum values of the horizontal component of the pseudogravity gradient (magnetization boundary lines). The resultant end product was a reconnaissance geologic map where broad terrane categories were delineated and geologic faults with both topographic and magnetic expression were defined. The availability of global spaceborne radar coverage in the 1990s and the large number of existing digital aeromagnetic surveys in northwestern Brazil indicate that this approach can be potentially useful for reconnaissance geologic mapping elsewhere in the Guiana Shield.

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