Science.gov

Sample records for aircraft carrier battle

  1. Psychiatric medevacs during a 6-month aircraft carrier battle group deployment to the Persian Gulf: a Navy Force Health Protection preliminary report.

    PubMed

    Wood, Dennis Patrick; Koffman, Robert L; Arita, Anthony A

    2003-01-01

    When a U.S. Navy Aircraft Carrier battle group deploys overseas, the aircraft carrier's medical department is responsible for the medical needs of over 12,000 personnel with their indigenous developmental, stress, family, alcohol, drug, and interpersonal and intrapersonal relationship difficulties. This article reviews the effectiveness of having a U.S. Navy clinical psychologist and a psychiatric technician onboard the USS Carl Vinson, the flag ship of Vinson's battle group, during this battle group's 1998/1999 Persian Gulf deployment (i.e., Western Pacific Deployment). Importantly, these two individuals reported to the USS Vinson as permanent members of the ship's company. The clinical psychologist logged 448 individual outpatient-care consults and 79 individual consults with sailors who had a history of overusing or abusing alcohol. Additionally, nine sailors with acute disabling psychiatric diagnoses were hospitalized on the ship's medical ward, and four sailors were medically evacuated (medevaced), by fixed wing aircraft, from USS Vinson to a Navy Hospital in the United States for definitive evaluation, treatment, and disposition. These four medevacs were less than the number of medevacs from two previous Aircraft Carrier Battle Group Persian Gulf deployments. Importantly, these two previous WESTPAC deployments were made without having a clinical psychologist as a full-time member of the respective aircraft carrier's medical department. Providing clinical psychology/mental health services at the "tip of the spear" is an effective, beneficial, and cost-saving landmark improvement in providing quality medical care to the fleet.

  2. Prepositioned Trailers for Aircraft Battle Damage Support

    DTIC Science & Technology

    2004-03-01

    skilled as the ABDR team members were, many repairs could not have been accomplished without major module replacement spares ( Feiler , 1989:17...battle damaged aircraft using techniques learned in the ABDR technician course ( Feiler , 1989:13). ABDR Assessor- aircraft maintenance technician who is...Air University Review, (March-April 1966). Feiler , Robert L. Analysis of the United States Air Force Aircraft Battle Damage Repair Engineer

  3. Implications of China’s Aircraft Carrier Development

    DTIC Science & Technology

    2012-03-16

    Chong Lot 7 stated that the ship would become a floating entertainment center and casino .16 Despite that, global security suspected the actual use of...2011, http://www.defensenews.com/article/20110730/DEFSECT03/107300302/Chinese- General-Country-Needs-3-Carriers ( assessed January 10,2012) 21 Bill...aircraft-carrier-is-for-research- 072711/ ( assessed October 10, 2011) 24 War Eye, " China will build four aircraft carrier battle groups in two stages

  4. Benefits and limitations of composites in carrier-based aircraft

    NASA Technical Reports Server (NTRS)

    Mcerlean, Donald P.

    1992-01-01

    There are many unique aspects of Navy air missions that lead to the differentiation between the design and performance of ship and shore-based aircraft. The major aspects are discussed from which essentially all Navy aircraft design requirements derive. (1) Navy aircraft operate from carriers at sea imposes a broad spectrum of physical conditions, constraints, and requirements ranging from the harsh sea environment, the space limitations of a carrier, takeoff and landing requirements as well as for endurance at long distances from the carrier. (2) Because the carrier and its airwing are intended to be capable of responding to a broad range of contingencies, mission flexibility is essential (maximum weapon carriage, rapid reconfiguration, multiple mission capability). (3) The embarked aircraft provides the long range defense of the battle group against air, surface and subsurface launched antiship missiles. (4) The carrier and its aircraft must operate independently and outside of normal supply lines. Taking into account these aspects, the use of composite materials in the design and performance of naval aircraft is outlined, also listing advantages and disadvantages.

  5. Aircraft Battle Damage Repair for the 90’s and Beyond

    DTIC Science & Technology

    1994-03-01

    Battle Danrge Repair, 2. 26. Lt Col Tony L Dedmond, ’Joining Forces to Survive Tomorrow’s Battles," Aerospaw.e Ameri’ca, August 1902, 37. 27. AYR 66...17-18. 15. Fit Lt E. Bittel , Fit Lt W. A. Brown, and P. F. Jowitt, Aircraft Battle Damage Repair Studies (Farnborough, U.K.: Royal Aircraft...Establishment, June 1981), 4. 16. 1992 US Air Force-wide Aircraft Battle Damage Repair Conference Minutes, March 1992,4. 17. Ibid. 18. Ibid. 19. Bittel , Brown

  6. Nuclear Submarines and Aircraft Carriers | Radiation ...

    EPA Pesticide Factsheets

    2016-02-23

    Nuclear submarines and aircraft carriers are powered by onboard nuclear reactors. Heat from the nuclear reaction makes the steam needed to power the submarine. When a nuclear vessel is taken out of service, its radioactive parts are disposed of and monitored.

  7. China’s Aircraft Carrier Ambitions: An Update

    DTIC Science & Technology

    2010-01-01

    Takeoff?” Xiandai junshi [Contemporary Military], no. 6 (2006); Liu Jiangping, Jiang Yongjun , and Yang Zhen, “Medium-Sized Aircraft Carrier Has...Defense University. 36. See Deng Taihong and Wang Yingchao, “Exploring the Origins of the Differences between U.S. and Russian Aircraft Carriers in...Active Service,” Shipborne Weapons, 6 June 2008; Liu, Jiang, and Yang, “Medium-Sized Aircraft Carrier.” 37. Deng and Wang , “Exploring the Origins

  8. NASA's Shuttle Carrier Aircraft 911's Final Flight

    NASA Video Gallery

    NASA 911, one of NASA's two modified Boeing 747 space shuttle carrier aircraft, flew its final flight Feb. 8, a short hop from NASA's Dryden Flight Research Center at Edwards Air Force Base to the ...

  9. Improving Student Naval Aviator Aircraft Carrier Landing Performance

    ERIC Educational Resources Information Center

    Sheppard, Thomas H.; Foster, T. Chris

    2008-01-01

    This article discusses the use of human performance technology (HPT) to improve qualification rates for learning to land onboard aircraft carriers. This project started as a request for a business case analysis and evolved into a full-fledged performance improvement project, from mission analysis through evaluation. The result was a significant…

  10. 77 FR 21834 - Airborne Radar Altimeter Equipment (For Air Carrier Aircraft)

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-04-11

    ... Federal Aviation Administration Airborne Radar Altimeter Equipment (For Air Carrier Aircraft) AGENCY..., Airborne Radar Altimeter Equipment (For Air Carrier Aircraft). SUMMARY: This is a confirmation notice of the cancellation of TSO-C67, Airborne Radar Altimeter Equipment (For Air Carrier Aircraft). The...

  11. Crewmen of the Gemini 7 spacecraft arrive aboard aircraft carrier

    NASA Technical Reports Server (NTRS)

    1965-01-01

    Astronauts James A. Lovell Jr., (left), pilot, and Frank Borman, command pilot, are shown just after they arrived aboard the aircraft carrier U.S.S. Wasp. Greeting the astronauts are Donald Stullken (at Lovell's right), Recovery Operations Branch, Landing and Recovery Division; Dr. Howard Minners (standing beside Borman), Flight Medicine Branch, Cneter Medical Office, Manned Spacecraft Center, and Bennett James (standing behind Borman), a NASA Public Affairs Officer.

  12. Navy Carrier Battle Groups: The Structure and Affordability of the Future Force

    DTIC Science & Technology

    1993-02-01

    coln(’ ntic ccii fi seci wing aircraft, (2)1 Iittti tc 014. number of aircraft thc’y van carry, ant (3G) cc caflgurt’c fo r Ilt’ acinlcifilcc mi...nuclear component business to sustain then in the near term. Many suppliers would likely search for non-nuclear commarcia markets to remain in 27 Page

  13. 14 CFR 382.71 - What other aircraft accessibility requirements apply to carriers?

    Code of Federal Regulations, 2011 CFR

    2011-01-01

    ... 14 Aeronautics and Space 4 2011-01-01 2011-01-01 false What other aircraft accessibility requirements apply to carriers? 382.71 Section 382.71 Aeronautics and Space OFFICE OF THE SECRETARY, DEPARTMENT... DISABILITY IN AIR TRAVEL Accessibility of Aircraft § 382.71 What other aircraft accessibility...

  14. 14 CFR 382.71 - What other aircraft accessibility requirements apply to carriers?

    Code of Federal Regulations, 2012 CFR

    2012-01-01

    ... 14 Aeronautics and Space 4 2012-01-01 2012-01-01 false What other aircraft accessibility requirements apply to carriers? 382.71 Section 382.71 Aeronautics and Space OFFICE OF THE SECRETARY, DEPARTMENT... DISABILITY IN AIR TRAVEL Accessibility of Aircraft § 382.71 What other aircraft accessibility...

  15. 14 CFR 382.71 - What other aircraft accessibility requirements apply to carriers?

    Code of Federal Regulations, 2013 CFR

    2013-01-01

    ... 14 Aeronautics and Space 4 2013-01-01 2013-01-01 false What other aircraft accessibility requirements apply to carriers? 382.71 Section 382.71 Aeronautics and Space OFFICE OF THE SECRETARY, DEPARTMENT... DISABILITY IN AIR TRAVEL Accessibility of Aircraft § 382.71 What other aircraft accessibility...

  16. 14 CFR 382.71 - What other aircraft accessibility requirements apply to carriers?

    Code of Federal Regulations, 2014 CFR

    2014-01-01

    ... 14 Aeronautics and Space 4 2014-01-01 2014-01-01 false What other aircraft accessibility requirements apply to carriers? 382.71 Section 382.71 Aeronautics and Space OFFICE OF THE SECRETARY, DEPARTMENT... DISABILITY IN AIR TRAVEL Accessibility of Aircraft § 382.71 What other aircraft accessibility...

  17. 14 CFR 382.71 - What other aircraft accessibility requirements apply to carriers?

    Code of Federal Regulations, 2010 CFR

    2010-01-01

    ... 14 Aeronautics and Space 4 2010-01-01 2010-01-01 false What other aircraft accessibility requirements apply to carriers? 382.71 Section 382.71 Aeronautics and Space OFFICE OF THE SECRETARY, DEPARTMENT... DISABILITY IN AIR TRAVEL Accessibility of Aircraft § 382.71 What other aircraft accessibility...

  18. Current Procedures for Assessment of Battle-Damage Repair of Fixed-Wing Aircraft

    DTIC Science & Technology

    2010-05-01

    addition of ABDR Engineering training which focuses on thin-walled structural analysis and fastened joint design. ABDR engineers are typically assigned...Sheet metal thickness gauge – necessary for accurate measurement of skin panels. • Blind rivet depth gauge – necessary to prescribe the proper...Further damage  Accomplish Designated Missions  Contribute to the Battle  Deferment of Repairs for a “One Time” Flight or Self Recovery

  19. A NASA study of the impact of technology on future carrier based tactical aircraft - Overview

    NASA Technical Reports Server (NTRS)

    Wilson, S. B., III

    1992-01-01

    This paper examines the impact of technology on future carrier based tactical aircraft. The results were used in the Center for Naval Analysis Future Carrier Study. The NASA Team designed three classes of aircraft ('Fighter', 'Attack', and 'Multimission') with two different technology levels. The Multimission aircraft were further analyzed by examining the penalty on the aircraft for both catapult launch/arrested landing recovery (Cat/trap) and short take-off/vertical landing (STOVL). The study showed the so-called STOVL penalty was reduced by engine technology and the next generation Strike Fighter will pay more penalty for Cat/trap than for STOVL capability.

  20. Aircraft Battle Damage Repair (BDR) Analysis Methodolology Development Requirements. Revision 1.

    DTIC Science & Technology

    2007-11-02

    Models 6. Test & Evaluation Guidelines for BDR 7. Aircraft BDR Database Development 8. LSA Expansion for BDR 9. Sensitivity Analyses on 1st...applicability. 12 ♦ The JTCG/ME, JTCG/AS, and the Army Research Laboratories (ARL) are initiating development of a model for evaluating lethality and...Capability) 5. BDR Integration with Higher Level Models 6. Test & Evaluation Guidelines for BDR 7. Aircraft BDR Database Development I 8. LSA Expansion

  1. Requirements for an Aircraft Carrier Flight Deck Fire Fighting Test Facility

    DTIC Science & Technology

    2007-11-02

    Naval Research Laboratory Washington, DC 20375-5320 NRL/MRI6180--03-8668 Requirements for an Aircraft Carrier Flight Deck Fire Fighting Test Facility...Requirements for an Aircraft Carrier Flight Deck Fire Fighting Test Facility 5c. PROGRAM ELEMENT NUMBER 604567N 6. AUTHOR(S) 5d. PROJECT NUMBER 61-8257-0-3...Air Warfare Center, Weapons Division, China Lake, CA 93555-6100 14. ABSTRACT This report outlines the requirements for a flight deck fire fighting

  2. A Short Take-Off/Vertical Landing (STOVL) Aircraft Carrier (S-CVX).

    DTIC Science & Technology

    1998-05-01

    and operation of the modem aircraft carrier, assuming availability of short take-off and vertical landing (STOVL) aircraft, employing gas turbine ship ... propulsion and providing significant capability to support humanitarian operations. In the design study reported here, the authors take a systems

  3. 19 CFR 122.53 - Aircraft of foreign registry chartered or leased to U.S. air carriers.

    Code of Federal Regulations, 2011 CFR

    2011-04-01

    ... 19 Customs Duties 1 2011-04-01 2011-04-01 false Aircraft of foreign registry chartered or leased... Permit § 122.53 Aircraft of foreign registry chartered or leased to U.S. air carriers. Aircraft of foreign registry leased or chartered to a U.S. air carrier, while being operated by the U.S. air...

  4. 19 CFR 122.53 - Aircraft of foreign registry chartered or leased to U.S. air carriers.

    Code of Federal Regulations, 2010 CFR

    2010-04-01

    ... 19 Customs Duties 1 2010-04-01 2010-04-01 false Aircraft of foreign registry chartered or leased... Permit § 122.53 Aircraft of foreign registry chartered or leased to U.S. air carriers. Aircraft of foreign registry leased or chartered to a U.S. air carrier, while being operated by the U.S. air...

  5. 19 CFR 122.53 - Aircraft of foreign registry chartered or leased to U.S. air carriers.

    Code of Federal Regulations, 2014 CFR

    2014-04-01

    ... 19 Customs Duties 1 2014-04-01 2014-04-01 false Aircraft of foreign registry chartered or leased... Permit § 122.53 Aircraft of foreign registry chartered or leased to U.S. air carriers. Aircraft of foreign registry leased or chartered to a U.S. air carrier, while being operated by the U.S. air...

  6. 19 CFR 122.53 - Aircraft of foreign registry chartered or leased to U.S. air carriers.

    Code of Federal Regulations, 2013 CFR

    2013-04-01

    ... 19 Customs Duties 1 2013-04-01 2013-04-01 false Aircraft of foreign registry chartered or leased... Permit § 122.53 Aircraft of foreign registry chartered or leased to U.S. air carriers. Aircraft of foreign registry leased or chartered to a U.S. air carrier, while being operated by the U.S. air...

  7. 19 CFR 122.53 - Aircraft of foreign registry chartered or leased to U.S. air carriers.

    Code of Federal Regulations, 2012 CFR

    2012-04-01

    ... 19 Customs Duties 1 2012-04-01 2012-04-01 false Aircraft of foreign registry chartered or leased... Permit § 122.53 Aircraft of foreign registry chartered or leased to U.S. air carriers. Aircraft of foreign registry leased or chartered to a U.S. air carrier, while being operated by the U.S. air...

  8. Effect of Wind Over Deck Conditions on Aircraft Approach Speeds for Carrier Landings

    DTIC Science & Technology

    1991-09-01

    the glideslope established by the carrier’s Fresnel lens , a pilot will perform a successful carrier landing. The NATOPS recommended approach speed...glideslope followed during the test, which is defined by the fresnel lens , establishes the aircraft’s sink rate. The minimum recovery head wind is...of a carrier landing, the pilot’s principle guidance shifts from the AOA indexer to the glideslope indicator i.e. the "ball" seen on the Fresnel Lens . The

  9. 14 CFR 382.119 - What information must carriers give individuals with vision or hearing impairment on aircraft?

    Code of Federal Regulations, 2013 CFR

    2013-01-01

    ... 14 Aeronautics and Space 4 2013-01-01 2013-01-01 false What information must carriers give individuals with vision or hearing impairment on aircraft? 382.119 Section 382.119 Aeronautics and Space... carriers give individuals with vision or hearing impairment on aircraft? (a) As a carrier, you must...

  10. 14 CFR 382.119 - What information must carriers give individuals with vision or hearing impairment on aircraft?

    Code of Federal Regulations, 2014 CFR

    2014-01-01

    ... 14 Aeronautics and Space 4 2014-01-01 2014-01-01 false What information must carriers give individuals with vision or hearing impairment on aircraft? 382.119 Section 382.119 Aeronautics and Space... carriers give individuals with vision or hearing impairment on aircraft? (a) As a carrier, you must...

  11. 14 CFR 382.119 - What information must carriers give individuals with vision or hearing impairment on aircraft?

    Code of Federal Regulations, 2011 CFR

    2011-01-01

    ... 14 Aeronautics and Space 4 2011-01-01 2011-01-01 false What information must carriers give individuals with vision or hearing impairment on aircraft? 382.119 Section 382.119 Aeronautics and Space... carriers give individuals with vision or hearing impairment on aircraft? (a) As a carrier, you must...

  12. 14 CFR 382.119 - What information must carriers give individuals with vision or hearing impairment on aircraft?

    Code of Federal Regulations, 2012 CFR

    2012-01-01

    ... 14 Aeronautics and Space 4 2012-01-01 2012-01-01 false What information must carriers give individuals with vision or hearing impairment on aircraft? 382.119 Section 382.119 Aeronautics and Space... carriers give individuals with vision or hearing impairment on aircraft? (a) As a carrier, you must...

  13. Considerations Relative to the Use of Canes by Blind Travelers in Air Carrier Aircraft Cabins,

    DTIC Science & Technology

    1980-07-01

    U) JUL 80 R F CHANDLER , J 0 GARNER, D L LOWREY UNCLASSIF lED FAAA-012EEEMEh EIEF’Tmom FAA-AM-80-12 CONSIDERATIONS RELATIVE TO THE USE OF CANES BY...BLIND TRAVELERS IN AIR CARRIER AIRCRAFT CABINS 0R. F. Chandler , J. D. Garner, D. L. Lowrey, qJ. G. Blethrow, and J. A. Anderson Civil Aeromedical...TRAVELERS IN AIR CARRIER AIRCRAFT CABINS 6 Perarming Organization Code .. PerformingOrgan ationReport No. 7.Au R. F. Chandler J. D./Garner D. L./Lowrey J

  14. Increasing Aircraft Carrier Forward Presence: Changing the Length of the Maintenance Cycle

    DTIC Science & Technology

    2008-01-01

    midlife refueling complex over- haul (RCOH) after approximately 23 years. Increased deploy- ments could deplete reactor fuel sooner than expected...NOTE: CVN = aircraft carrier, nuclear. a As of fall 2007, the Vinson is at Northrop Grumman Newport News for her midlife RCOH. She will be homeported...interval PIA 0 Months 18 24 42 48 66 76.5 DPIAPIA Operating interval COH-1 Past, Current, and Potential Carrier Cycles 9 and DPIA2s after the midlife

  15. Navy Ford (CVN-78) Class Aircraft Carrier Program: Background and Issues for Congress

    DTIC Science & Technology

    2016-05-27

    Names Next Aircraft Carrier USS John F. Kennedy,” Navy News Service, May 29, 2011, accessed online on June 1, 2011 at http://www.navy.mil/search...and USS John F. Kennedy (CVN 79) come online ? A: The proposed plan matches the number of complete carrier air wings to the number of operationally...efficiently be performed. The CVN 79 build sequence installs 20 percent more parts in shop , and 30 percent more parts on the final assembly platen, as

  16. Navy Ford (CVN 78) Class Aircraft Carrier Program: Background and Issues for Congress

    DTIC Science & Technology

    2016-05-27

    Names Next Aircraft Carrier USS John F. Kennedy,” Navy News Service, May 29, 2011, accessed online on June 1, 2011 at http://www.navy.mil/search...and USS John F. Kennedy (CVN 79) come online ? A: The proposed plan matches the number of complete carrier air wings to the number of operationally...efficiently be performed. The CVN 79 build sequence installs 20 percent more parts in shop , and 30 percent more parts on the final assembly platen, as

  17. 77 FR 3323 - Airborne Radar Altimeter Equipment (For Air Carrier Aircraft)

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-01-23

    ... Doc No: 2012-1243] DEPARTMENT OF TRANSPORTATION Federal Aviation Administration Airborne Radar...: Notice of intent to cancel Technical Standard Order (TSO)-C67, Airborne Radar Altimeter Equipment (For... Radar Altimeter Equipment (For Air Carrier Aircraft). The effect of the cancelled TSO will result in...

  18. 15 CFR 30.26 - Reporting of vessels, aircraft, cargo vans, and other carriers and containers.

    Code of Federal Regulations, 2013 CFR

    2013-01-01

    ... 15 Commerce and Foreign Trade 1 2013-01-01 2013-01-01 false Reporting of vessels, aircraft, cargo vans, and other carriers and containers. 30.26 Section 30.26 Commerce and Foreign Trade Regulations Relating to Commerce and Foreign Trade BUREAU OF THE CENSUS, DEPARTMENT OF COMMERCE FOREIGN...

  19. 15 CFR 30.26 - Reporting of vessels, aircraft, cargo vans, and other carriers and containers.

    Code of Federal Regulations, 2012 CFR

    2012-01-01

    ... 15 Commerce and Foreign Trade 1 2012-01-01 2012-01-01 false Reporting of vessels, aircraft, cargo vans, and other carriers and containers. 30.26 Section 30.26 Commerce and Foreign Trade Regulations Relating to Commerce and Foreign Trade BUREAU OF THE CENSUS, DEPARTMENT OF COMMERCE FOREIGN...

  20. Orbiter/shuttle carrier aircraft separation: Wind tunnel, simulation, and flight test overview and results

    NASA Technical Reports Server (NTRS)

    Homan, D. J.; Denison, D. E.; Elchert, K. C.

    1980-01-01

    A summary of the approach and landing test phase of the space shuttle program is given from the orbiter/shuttle carrier aircraft separation point of view. The data and analyses used during the wind tunnel testing, simulation, and flight test phases in preparation for the orbiter approach and landing tests are reported.

  1. On the feasibility of real-time prediction of aircraft carrier motion at sea

    NASA Technical Reports Server (NTRS)

    Sidar, M. M.; Doolin, B. F.

    1983-01-01

    Landing aircraft on board carriers is a most delicate phase of flight operations at sea. The ability to predict the aircraft carrier's motion over an interval of several seconds within reasonable error bounds may allow an improvement in touchdown dispersion and reduce the value of the ramp clearance due to a smoother aircraft trajectory. Also, improved information to the landing signal officer should decrease the number of waveoffs substantially. This paper indicates and shows quantitatively that, based upon the power density spectrum data for pitch and heave measured for various ships and sea conditions, the motion can be predicted well, for up to 15 s. Moreover, the zero crossover times for both pitch and heave motions can be predicted with impressive accuracy. The predictor was designed on the basis of Kalman's optimum filtering theory (the discrete time case), being compatible with real-time digital computer operation.

  2. Methodologies for reproducing in-flight loads of aircraft wings on the ground and predicting their response to battle-induced damage

    NASA Astrophysics Data System (ADS)

    Bou-Mosleh, Charbel Fouad

    Survivability of an aircraft in combat is achieved by not getting hit or by withstanding the effects of some suffered hits. Combat damage is described by the removal of one or more portions of the wing or any other flight control surface. To determine whether a wing will survive a specific damage, the structural and aerodynamic response of the wing should be predicted and tested. The response of wings to battle-induced damage is currently addressed through live-fire testing on the ground. The loading methodology used in these live-fire tests does not reproduce the loads encountered during flight, and does not account for the changes in structural stiffness and mass of the wing after damage infliction. In addition, current live-fire tests fail to address the changes in the aerodynamic performance of the wing caused by the battle-induced damage. To better address the structural response of aircraft wings to combat damage, this thesis investigates a concept for an alternative loading methodology that exploits recent advances in nonlinear aeroelastic simulations and smart material actuators. The main idea behind this concept is to accurately predict the stress states of the wing before, during, and after sustaining a hit, for a given flight condition, and reproduce them on the ground by loading the spars and ribs of the wings with programmable actuators and/or a few external tethers. Mathematically, this entails solving an optimization problem to determine the locations and gains of the actuators. Two different types of actuators are investigated: 1D actuators or actuators with tension/compression capability and bimorph bender actuators. The potential of the investigated loading methodology is evaluated for "slender" wings (ARW-2 wing) and for "delta" wings (HSCT and F-16 wing) at a transonic flight condition. The obtained numerical results suggest that the investigated loading methodology can reproduce a desired stress state fairly accurately using external tethers

  3. Aircraft

    DTIC Science & Technology

    2003-01-01

    national power. But with the recent events such as the war with Iraq, the Severe Acute Respiratory Syndrome (SARS) outbreak, some major carriers... TITLE AND SUBTITLE 2003 Industry Studies: Aircraft 5a. CONTRACT NUMBER 5b. GRANT NUMBER 5c. PROGRAM ELEMENT NUMBER 6. AUTHOR(S) 5d. PROJECT NUMBER

  4. CVN 78 Gerald R. Ford Class Nuclear Aircraft Carrier (CVN 78)

    DTIC Science & Technology

    2015-12-01

    Selected Acquisition Report (SAR) RCS: DD-A&T(Q&A)823-223 CVN 78 Gerald R. Ford Class Nuclear Aircraft Carrier (CVN 78) As of FY 2017 President’s...POE - Program Office Estimate RDT&E - Research, Development, Test, and Evaluation SAR - Selected Acquisition Report SCP - Service Cost Position TBD...Preparation contract was awarded the same day. This modification included the remaining component and steel fabrication and selected construction unit

  5. Automatic carrier landing system for V/STOL aircraft using L1 adaptive and optimal control

    NASA Astrophysics Data System (ADS)

    Hariharapura Ramesh, Shashank

    This thesis presents a framework for developing automatic carrier landing systems for aircraft with vertical or short take-off and landing capability using two different control strategies---gain-scheduled linear optimal control, and L1 adaptive control. The carrier landing sequence of V/STOL aircraft involves large variations in dynamic pressure and aerodynamic coefficients arising because of the transition from aerodynamic-supported to jet-borne flight, descent to the touchdown altitude, and turns performed to align with the runway. Consequently, the dynamics of the aircraft exhibit a highly non-linear dynamical behavior with variations in flight conditions prior to touchdown. Therefore, the implication is the need for non-linear control techniques to achieve automatic landing. Gain-scheduling has been one of the most widely employed techniques for control of aircraft, which involves designing linear controllers for numerous trimmed flight conditions, and interpolating them to achieve a global non-linear control. Adaptive control technique, on the other hand, eliminates the need to schedule the controller parameters as they adapt to changing flight conditions.

  6. NASA's NB-52B carrier aircraft rolls down a taxiway with the X-43A hypersonic research aircraft and

    NASA Technical Reports Server (NTRS)

    2001-01-01

    As part of a combined systems test conducted by NASA Dryden Flight Research Center, NASA's NB-52B carrier aircraft rolls down a taxiway at Edwards Air Force Base with the X-43A hypersonic research aircraft and its modified Pegasus booster rocket attached to a pylon under its right wing. The taxi test was one of the last major milestones in the Hyper-X research program before the first X-43A flight. The X-43A flights will be the first actual flight tests of an aircraft powered by a revolutionary supersonic-combustion ramjet ('scramjet') engine capable of operating at hypersonic speeds (above Mach 5, or five times the speed of sound). The 12-foot, unpiloted research vehicle was developed and built by MicroCraft Inc., Tullahoma, Tenn., under NASA contract. The booster was built by Orbital Sciences Corp., Dulles, Va. After being air-launched from NASA's venerable NB-52 mothership, the booster will accelerate the X-43A to test speed and altitude. The X-43A will then separate from the rocket and fly a pre-programmed trajectory, conducting aerodynamic and propulsion experiments until it descends into the Pacific Ocean. Three research flights are planned, two at Mach 7 and one at Mach 10.

  7. NASA's NB-52B carrier aircraft rolls down a taxiway with the X-43A hypersonic research aircraft and

    NASA Technical Reports Server (NTRS)

    2001-01-01

    NASA's NB-52B carrier aircraft rolls down a taxiway at Edwards Air Force Base with the X-43A hypersonic research aircraft and its modified Pegasus booster rocket slung from a pylon under its right wing. Part of a combined systems test conducted by NASA's Dryden Flight Research Center at Edwards, the taxi test was one of the last major milestones in the Hyper-X research program before the first X-43A flight. The X-43A flights will be the first actual flight tests of an aircraft powered by a revolutionary supersonic-combustion ramjet ('scramjet') engine capable of operating at hypersonic speeds (above Mach 5, or five times the speed of sound). The 12-foot, unpiloted research vehicle was developed and built by MicroCraft Inc., Tullahoma, Tenn., under NASA contract. The booster was built by Orbital Sciences Corp., Dulles, Va.,After being air-launched from NASA's venerable NB-52 mothership, the booster will accelerate the X-43A to test speed and altitude. The X-43A will then separate from the rocket and fly a pre-programmed trajectory, conducting aerodynamic and propulsion experiments until it descends into the Pacific Ocean. Three research flights are planned, two at Mach 7 and one at Mach 10, with the first tentatively scheduled for late spring to early summer, 2001.

  8. Unmanned Carrier-based Aircraft System: Navy Needs to Demonstrate Match between Its Requirements and Available Resources

    DTIC Science & Technology

    2015-05-01

    UNMANNED CARRIER-BASED AIRCRAFT SYSTEM Navy Needs to Demonstrate Match between Its Requirements and Available...for reviewing instructions, searching existing data sources, gathering and maintaining the data needed , and completing and reviewing the collection of...DATES COVERED 00-00-2015 to 00-00-2015 4. TITLE AND SUBTITLE Unmanned Carrier-based Aircraft System: Navy Needs to Demonstrate Match between Its

  9. Depot Maintenance: Navy Has Revised Its Estimated Workforce Cost for Basing an Aircraft Carrier at Mayport, Florida (Briefing charts)

    DTIC Science & Technology

    2011-03-03

    issues, the House report directed GAO to provide an assessment of the readiness and cost impacts of the aircraft carrier homeporting and maintenance...homeporting an aircraft carrier at Mayport warrant the production of an independent cost estimate—an industry and a government cost- estimating best...GAO-11-257R Depot Maintenance United States Government Accountability Office Washington, DC 20548 March 3, 2011

  10. 14 CFR 382.111 - What services must carriers provide to passengers with a disability on board the aircraft?

    Code of Federal Regulations, 2012 CFR

    2012-01-01

    ... 14 Aeronautics and Space 4 2012-01-01 2012-01-01 false What services must carriers provide to passengers with a disability on board the aircraft? 382.111 Section 382.111 Aeronautics and Space OFFICE OF... NONDISCRIMINATION ON THE BASIS OF DISABILITY IN AIR TRAVEL Services on Aircraft § 382.111 What services...

  11. 14 CFR 382.111 - What services must carriers provide to passengers with a disability on board the aircraft?

    Code of Federal Regulations, 2013 CFR

    2013-01-01

    ... 14 Aeronautics and Space 4 2013-01-01 2013-01-01 false What services must carriers provide to passengers with a disability on board the aircraft? 382.111 Section 382.111 Aeronautics and Space OFFICE OF... NONDISCRIMINATION ON THE BASIS OF DISABILITY IN AIR TRAVEL Services on Aircraft § 382.111 What services...

  12. 14 CFR 382.111 - What services must carriers provide to passengers with a disability on board the aircraft?

    Code of Federal Regulations, 2011 CFR

    2011-01-01

    ... 14 Aeronautics and Space 4 2011-01-01 2011-01-01 false What services must carriers provide to passengers with a disability on board the aircraft? 382.111 Section 382.111 Aeronautics and Space OFFICE OF... NONDISCRIMINATION ON THE BASIS OF DISABILITY IN AIR TRAVEL Services on Aircraft § 382.111 What services...

  13. 14 CFR 382.111 - What services must carriers provide to passengers with a disability on board the aircraft?

    Code of Federal Regulations, 2014 CFR

    2014-01-01

    ... 14 Aeronautics and Space 4 2014-01-01 2014-01-01 false What services must carriers provide to passengers with a disability on board the aircraft? 382.111 Section 382.111 Aeronautics and Space OFFICE OF... NONDISCRIMINATION ON THE BASIS OF DISABILITY IN AIR TRAVEL Services on Aircraft § 382.111 What services...

  14. 14 CFR 382.119 - What information must carriers give individuals with vision or hearing impairment on aircraft?

    Code of Federal Regulations, 2010 CFR

    2010-01-01

    ... 14 Aeronautics and Space 4 2010-01-01 2010-01-01 false What information must carriers give individuals with vision or hearing impairment on aircraft? 382.119 Section 382.119 Aeronautics and Space... NONDISCRIMINATION ON THE BASIS OF DISABILITY IN AIR TRAVEL Services on Aircraft § 382.119 What information...

  15. 14 CFR 382.111 - What services must carriers provide to passengers with a disability on board the aircraft?

    Code of Federal Regulations, 2010 CFR

    2010-01-01

    ... 14 Aeronautics and Space 4 2010-01-01 2010-01-01 false What services must carriers provide to passengers with a disability on board the aircraft? 382.111 Section 382.111 Aeronautics and Space OFFICE OF... NONDISCRIMINATION ON THE BASIS OF DISABILITY IN AIR TRAVEL Services on Aircraft § 382.111 What services...

  16. Aircraft Battle Damage Repair (ABDR) 2000: Will ABDR Become the Logistics Center of Gravity by the Year 2000

    DTIC Science & Technology

    1989-05-01

    damage repair comes from the conflict in Southeast Asia CSEA ) and data available from the Arab-Israeli 1973 Yom Kippur war. Battle damage experience data...Performance." Air Force Journal of Loglutics, Vol. VIII, No. 4. Fall 1984, p. 9. 3. Department of the A~r Forcei Headquarters U.S. Air Force. "R&M 2000...Key to Combat Strength." 1.jr Force Journal of Logistl, Winter 1988, pp. 5-6. 17. Kitfield, James. "Concern Over Composites." ° Forum, January-February

  17. 14 CFR 298.63 - Reporting of aircraft operating expenses and related statistics by small certificated air carriers.

    Code of Federal Regulations, 2010 CFR

    2010-01-01

    ... 14 Aeronautics and Space 4 2010-01-01 2010-01-01 false Reporting of aircraft operating expenses and related statistics by small certificated air carriers. 298.63 Section 298.63 Aeronautics and Space... EXEMPTIONS FOR AIR TAXI AND COMMUTER AIR CARRIER OPERATIONS Reporting Requirements § 298.63 Reporting...

  18. 14 CFR 298.63 - Reporting of aircraft operating expenses and related statistics by small certificated air carriers.

    Code of Federal Regulations, 2014 CFR

    2014-01-01

    ... and related statistics by small certificated air carriers. 298.63 Section 298.63 Aeronautics and Space... aircraft operating expenses and related statistics by small certificated air carriers. (a) Each small... Related Statistics.” This schedule shall be filed quarterly as prescribed in § 298.60. Data reported...

  19. 14 CFR 298.63 - Reporting of aircraft operating expenses and related statistics by small certificated air carriers.

    Code of Federal Regulations, 2011 CFR

    2011-01-01

    ... and related statistics by small certificated air carriers. 298.63 Section 298.63 Aeronautics and Space... aircraft operating expenses and related statistics by small certificated air carriers. (a) Each small... Related Statistics.” This schedule shall be filed quarterly as prescribed in § 298.60. Data reported...

  20. 14 CFR 298.63 - Reporting of aircraft operating expenses and related statistics by small certificated air carriers.

    Code of Federal Regulations, 2012 CFR

    2012-01-01

    ... and related statistics by small certificated air carriers. 298.63 Section 298.63 Aeronautics and Space... aircraft operating expenses and related statistics by small certificated air carriers. (a) Each small... Related Statistics.” This schedule shall be filed quarterly as prescribed in § 298.60. Data reported...

  1. 14 CFR 298.63 - Reporting of aircraft operating expenses and related statistics by small certificated air carriers.

    Code of Federal Regulations, 2013 CFR

    2013-01-01

    ... and related statistics by small certificated air carriers. 298.63 Section 298.63 Aeronautics and Space... aircraft operating expenses and related statistics by small certificated air carriers. (a) Each small... Related Statistics.” This schedule shall be filed quarterly as prescribed in § 298.60. Data reported...

  2. Application of the concept of dynamic trim control to automatic landing of carrier aircraft. [utilizing digital feedforeward control

    NASA Technical Reports Server (NTRS)

    Smith, G. A.; Meyer, G.

    1980-01-01

    The results of a simulation study of an alternative design concept for an automatic landing control system are presented. The alternative design concept for an automatic landing control system is described. The design concept is the total aircraft flight control system (TAFCOS). TAFCOS is an open loop, feed forward system that commands the proper instantaneous thrust, angle of attack, and roll angle to achieve the forces required to follow the desired trajector. These dynamic trim conditions are determined by an inversion of the aircraft nonlinear force characteristics. The concept was applied to an A-7E aircraft approaching an aircraft carrier. The implementation details with an airborne digital computer are discussed. The automatic carrier landing situation is described. The simulation results are presented for a carrier approach with atmospheric disturbances, an approach with no disturbances, and for tailwind and headwind gusts.

  3. On the feasibility of real-time prediction of aircraft carrier motion at sea

    NASA Technical Reports Server (NTRS)

    Sidar, M.; Doolin, B. F.

    1975-01-01

    The ability to predict the aircraft carrier's motion over an interval of several seconds within reasonable error bounds may allow an improvement in touchdown dispersion and a more certain value for ramp clearance due to a smoother aircraft trajectory. Also, improved information to the landing signal officer should decrease the number of waveoffs substantially. It is quantitatively shown that, based on the power density spectrum data for pitch and heave measured for various ships and sea conditions, the motion can be predicted well for up to 15 seconds. The zero crossover times for both pitch and heave motions can be predicted with impressive accuracy. The predictor was designed on the basis of Kalman's optimum filtering theory for the discrete time case, adapted for real-time digital computer operation.

  4. Large >60 gallon/day ‘pulse-tube’ oxygen liquefier for aircraft carriers

    NASA Astrophysics Data System (ADS)

    Spoor, P. S.

    2015-12-01

    An oxygen liquefier using a large ‘pulse-tube’ or acoustic-Stirling cryocooler is described, which has a liquefaction rate in excess of 60 gallons per day (227 liters per day) as measured by the increase in weight of a storage dewar, from <20 kWe input. Several of these systems will be deployed on U.S. Navy aircraft carriers to provide shipboard liquid oxygen. Paths to improvement in future systems are identified, although it is noted that since the present system exceeds the required specifications, these improvements may not be implemented in the near term.

  5. Changing Aircraft Carrier Procurement Schedules: Effects that a Five-Year Procurement Cycle would have on Cost, Availability, and Shipyard Manpower and Workload

    DTIC Science & Technology

    2011-01-01

    carri- ers might increase by 1 or 2 percent; the cost of other carriers would decrease by a like percentage. The cost of future midlife RCOHs might...80 aircraft. U.S. Navy (USN) nuclear- powered aircraft carriers currently require a major refueling and com- plex overhaul (RCOH) at midlife . When...Northrop Grumman Shipbuilding—Newport News (NGSB-NN), the sole ship- yard that builds aircraft carriers and performs their midlife RCOHs; and the

  6. The Shuttle Carrier Aircraft, with Columbia on top, gets ready for the flight to California

    NASA Technical Reports Server (NTRS)

    1999-01-01

    The Boeing 747 Shuttle Carrier Aircraft, with the orbiter Columbia strapped to its back, waits at the Shuttle Landing Facility for clear weather to take off for its final destination, Palmdale, Calif. The oldest of four orbiters in NASA's fleet, Columbia is being ferried to Palmdale to undergo extensive inspections and modifications in Boeing's Orbiter Assembly Facility. The nine-month orbiter maintenance down period (OMDP) is the second in Columbia's history. Orbiters are periodically removed from flight operations for an OMDP. Columbia's first was in 1994. Along with more than 100 modifications on the vehicle, Columbia will be the second orbiter to be outfitted with the multifunctional electronic display system, or 'glass cockpit.' Columbia is expected to return to KSC in July 2000.

  7. Aircraft

    DTIC Science & Technology

    2002-01-01

    Company, Washington, DC Boeing Commercial Aircraft Division, Seattle, WA and Long Beach, CA Boeing Military Aircraft and Missile Division, St. Louis, MO and... aircraft ; military fixed-wing aircraft ; rotorcraft (helicopters and tiltrotor aircraft ); and aircraft jet engines. Two companies dominate the commercial... aircraft business, Boeing and Airbus. Four companies dominate the military fixed-wing market, Boeing, Lockheed Martin, BAE Systems, and European

  8. Sabot high speed interceptor AE 4273 aircraft design

    NASA Technical Reports Server (NTRS)

    Dober, Dave; Al-Hashel, Waleed; Baldocchi, Bob; Berg, Tim; Lindsay, Curt; Mcatee, Aaron; Sergent, Dan; Dunbrack, Harry

    1992-01-01

    Today's carrier based deck launched intercept (DLI) mission is a vital one that is aimed at protecting the carrier battle group and detering potential adversaries. The assets deployed on our carrier decks are able to complete this mission but with very limited range. The waverider concept has great potential to increase the range of this carrier based mission. As a result, a request for proposals (RFP) was developed which contains design requirements for an aircraft that can complete this mission through the utilization of waverider technology.

  9. STS-92 - Towing of Shuttle Discovery and Boeing 747 Shuttle Carrier Aircraft (SCA)

    NASA Technical Reports Server (NTRS)

    2000-01-01

    The Space Shuttle Discovery sits atop one of NASA's modified Boeing 747 Shuttle Carrier Aircraft as the unusual piggyback duo is towed along a taxiway at NASA's Dryden Flight Research Center at Edwards, California. The Discovery was ferried from NASA Dryden to NASA's Kennedy Space Center in Florida on November 2, 2000, after extensive pre-ferry servicing and preparations. STS-92 was the 100th mission since the fleet of four Space Shuttles began flying in 1981. (Due to schedule changes, missions are not always launched in the order that was originally planned.) The almost 13-day mission, the 46th Shuttle mission to land at Edwards, was the last construction mission for the International Space Station prior to the first scientists taking up residency in the orbiting space laboratory the following month. The seven-member crew on STS-92 included mission specialists Koichi Wakata, Michael Lopez-Alegria, Jeff Wisoff, Bill McArthur and Leroy Chiao, pilot Pam Melroy and mission commander Brian Duffy.

  10. Apollo 11 Crew Boards U.S.S. Hornet Aircraft Carrier

    NASA Technical Reports Server (NTRS)

    1969-01-01

    The Apollo 11 mission, the first manned lunar mission, launched from the Kennedy Space Center, Florida via the Marshall Space Flight Center (MSFC) developed Saturn V launch vehicle on July 16, 1969 and safely returned to Earth on July 24, 1969. Aboard the space craft were astronauts Neil A. Armstrong, commander; Michael Collins, Command Module (CM) pilot; and Edwin E. Aldrin Jr., Lunar Module (LM) pilot. The CM, piloted by Michael Collins remained in a parking orbit around the Moon while the LM, named 'Eagle'', carrying astronauts Neil Armstrong and Edwin Aldrin, landed on the Moon. During 2½ hours of surface exploration, the crew collected 47 pounds of lunar surface material for analysis back on Earth. Shown here are the three astronauts (L-R) Aldrin, Armstrong, and Collins leaving the recovery helicopter aboard the U.S.S. Hornet after their splashdown in the Pacific Ocean. Wearing biological isolation garments donned before leaving the spacecraft, the three went directly into the Mobile Quarantine Facility (MQF) on the aircraft carrier. The MQF served as their home for 21 days following the mission. With the success of Apollo 11, the national objective to land men on the Moon and return them safely to Earth had been accomplished.

  11. 75 FR 12975 - Establishment of Class E Airspace; Battle Mountain, NV

    Federal Register 2010, 2011, 2012, 2013, 2014

    2010-03-18

    ... Federal Aviation Administration 14 CFR Part 71 Establishment of Class E Airspace; Battle Mountain, NV... establish Class E airspace at Battle Mountain, NV, to accommodate aircraft using the VHF Omni-Directional... Battle Mountain Airport. This will improve the safety and management of Instrument Flight Rules...

  12. One of NASA's Two Modified Boeing 747 Shuttle Carrier (SCA) Aircraft in Flight over NASA Dryden Flig

    NASA Technical Reports Server (NTRS)

    1999-01-01

    One of NASA's Boeing 747 Shuttle Carrier Aircraft flies over the Dryden Flight Research Center main building at Edwards Air Force Base, Edwards, California, in May 1999. NASA uses two modified Boeing 747 jetliners, originally manufactured for commercial use, as Space Shuttle Carrier Aircraft (SCA). One is a 747-100 model, while the other is designated a 747-100SR (short range). The two aircraft are identical in appearance and in their performance as Shuttle Carrier Aircraft. The 747 series of aircraft are four-engine intercontinental-range swept-wing 'jumbo jets' that entered commercial service in 1969. The SCAs are used to ferry space shuttle orbiters from landing sites back to the launch complex at the Kennedy Space Center, and also to and from other locations too distant for the orbiters to be delivered by ground transportation. The orbiters are placed atop the SCAs by Mate-Demate Devices, large gantry-like structures which hoist the orbiters off the ground for post-flight servicing, and then mate them with the SCAs for ferry flights. Features which distinguish the two SCAs from standard 747 jetliners are: o Three struts, with associated interior structural strengthening, protruding from the top of the fuselage (two aft, one forward) on which the orbiter is attached o Two additional vertical stabilizers, one on each end of the standard horizontal stabilizer, to enhance directional stability o Removal of all interior furnishings and equipment aft of the forward No. 1 doors o Instrumentation used by SCA flight crews and engineers to monitor orbiter electrical loads during the ferry flights and also during pre- and post-ferry flight operations. The two SCAs are under the operational control of NASA's Johnson Space Center, Houston, Tex. NASA 905 NASA 905 was the first SCA. It was obtained from American Airlines in 1974. Shortly after it was accepted by NASA it was flown in a series of wake vortex research flights at the Dryden Flight Research Center in a study to

  13. Comparing the performance of expert user heuristics and an integer linear program in aircraft carrier deck operations.

    PubMed

    Ryan, Jason C; Banerjee, Ashis Gopal; Cummings, Mary L; Roy, Nicholas

    2014-06-01

    Planning operations across a number of domains can be considered as resource allocation problems with timing constraints. An unexplored instance of such a problem domain is the aircraft carrier flight deck, where, in current operations, replanning is done without the aid of any computerized decision support. Rather, veteran operators employ a set of experience-based heuristics to quickly generate new operating schedules. These expert user heuristics are neither codified nor evaluated by the United States Navy; they have grown solely from the convergent experiences of supervisory staff. As unmanned aerial vehicles (UAVs) are introduced in the aircraft carrier domain, these heuristics may require alterations due to differing capabilities. The inclusion of UAVs also allows for new opportunities for on-line planning and control, providing an alternative to the current heuristic-based replanning methodology. To investigate these issues formally, we have developed a decision support system for flight deck operations that utilizes a conventional integer linear program-based planning algorithm. In this system, a human operator sets both the goals and constraints for the algorithm, which then returns a proposed schedule for operator approval. As a part of validating this system, the performance of this collaborative human-automation planner was compared with that of the expert user heuristics over a set of test scenarios. The resulting analysis shows that human heuristics often outperform the plans produced by an optimization algorithm, but are also often more conservative.

  14. STS-35 Leaves Dryden on 747 Shuttle Carrier Aircraft (SCA) Bound for Kennedy Space Center

    NASA Technical Reports Server (NTRS)

    1990-01-01

    The first rays of the morning sun light up the side of NASA's Boeing 747 Shuttle Carrier Aircraft (SCA) as it departs for the Kennedy Space Center, Florida, with the orbiter from STS-35 attached to its back. Space Shuttles are the main element of America's Space Transportation System and are used for space research and other space applications. The shuttles are the first vehicles capable of being launched into space and returning to Earth on a routine basis. Space Shuttles are used as orbiting laboratories in which scientists and mission specialists conduct a wide variety of scientific experiments. Crews aboard shuttles place satellites in orbit, rendezvous with satellites to carry out repair missions and return them to space, and retrieve satellites and return them to Earth for refurbishment and reuse. Space Shuttles are true aerospace vehicles. They leave Earth and its atmosphere under rocket power provided by three liquid-propellant main engines with two solid-propellant boosters attached plus an external liquid-fuel tank. After their orbital missions, they streak back through the atmosphere and land like airplanes. The returning shuttles, however, land like gliders, without power and on runways. Other rockets can place heavy payloads into orbit, but, they can only be used once. Space Shuttles are designed to be continually reused. When Space Shuttles are used to transport complete scientific laboratories into space, the laboratories remain inside the payload bay throughout the mission. They are then removed after the Space Shuttle returns to Earth and can be reused on future flights. Some of these orbital laboratories, like the Spacelab, provide facilities for several specialists to conduct experiments in such fields as medicine, astronomy, and materials manufacturing. Some types of satellites deployed by Space Shuttles include those involved in environmental and resources protection, astronomy, weather forecasting, navigation, oceanographic studies, and other

  15. Treatment of psychiatric disorders onboard an aircraft carrier assisted with psychotropic medication: a retrospective review describing one aspect of Navy Force health protection.

    PubMed

    Wood, Dennis Patrick; Walker, Errika; Moses, Kennett; Gilleran, Louis

    2006-04-01

    Navy clinical psychologists, assigned to aircraft carriers, are playing an increasing role in not only implementing Navy force health protection, but also in further specializing the delivery of mental health evaluation, treatment, and disposition services at the "tip of the spear." An aircraft carrier's medical department, augmented with a clinical psychologist, is now better able to coordinate diagnostic, psychotropic, and psychotherapeutic treatments for both shipboard and air wing personnel. This retrospective review reports the outcomes of a 6-month treatment program for personnel, assigned to the USS Constellation (CV-64), who were prescribed a psychotropic medication while receiving psychotherapy. We concluded that psychotropic medications can be safely and effectively used onboard an aircraft carrier. Furthermore, personnel prescribed psychotropic medication successfully completed their assigned duties and obtained recommendations for advancement and retention. Lastly, our medical department proactively fulfilled the Navy force health protection tenet of preserving a healthy and fit force.

  16. Navy Ford (CVN-78) Class Aircraft Carrier Program: Background and Issues for Congress

    DTIC Science & Technology

    2015-12-17

    implications on future carriers in the Ford-class and any subsequent new class of carriers. I also have concerns with manning and berthing on CVN 78. The Navy... berthing . These problems are similar to those seen on other recent ship classes such as DDG 1000 and the Littoral Combat Ship (LCS).... There are...required for delivery, such as berthing spaces for the aviation detachment, and has removed this work from the shipbuilder’s contract. This deferred

  17. 15 CFR 30.26 - Reporting of vessels, aircraft, cargo vans, and other carriers and containers.

    Code of Federal Regulations, 2011 CFR

    2011-01-01

    ... REGULATIONS Special Provisions and Specific-Type Transactions § 30.26 Reporting of vessels, aircraft, cargo... a port in such area, EEI shall be reported in accordance with the general requirements of the... car, car, vehicle, or container first leaves the United States after sale or transfer. If the...

  18. 15 CFR 30.26 - Reporting of vessels, aircraft, cargo vans, and other carriers and containers.

    Code of Federal Regulations, 2010 CFR

    2010-01-01

    ... REGULATIONS Special Provisions and Specific-Type Transactions § 30.26 Reporting of vessels, aircraft, cargo... a port in such area, EEI shall be reported in accordance with the general requirements of the... car, car, vehicle, or container first leaves the United States after sale or transfer. If the...

  19. Aircraft

    DOEpatents

    Hibbs, B.D.; Lissaman, P.B.S.; Morgan, W.R.; Radkey, R.L.

    1998-09-22

    This disclosure provides a solar rechargeable aircraft that is inexpensive to produce, is steerable, and can remain airborne almost indefinitely. The preferred aircraft is a span-loaded flying wing, having no fuselage or rudder. Travelling at relatively slow speeds, and having a two-hundred foot wingspan that mounts photovoltaic cells on most all of the wing`s top surface, the aircraft uses only differential thrust of its eight propellers to turn. Each of five sections of the wing has one or more engines and photovoltaic arrays, and produces its own lift independent of the other sections, to avoid loading them. Five two-sided photovoltaic arrays, in all, are mounted on the wing, and receive photovoltaic energy both incident on top of the wing, and which is incident also from below, through a bottom, transparent surface. The aircraft is capable of a top speed of about ninety miles per hour, which enables the aircraft to attain and can continuously maintain altitudes of up to sixty-five thousand feet. Regenerative fuel cells in the wing store excess electricity for use at night, such that the aircraft can sustain its elevation indefinitely. A main spar of the wing doubles as a pressure vessel that houses hydrogen and oxygen gases for use in the regenerative fuel cell. The aircraft has a wide variety of applications, which include weather monitoring and atmospheric testing, communications, surveillance, and other applications as well. 31 figs.

  20. Aircraft

    DOEpatents

    Hibbs, Bart D.; Lissaman, Peter B. S.; Morgan, Walter R.; Radkey, Robert L.

    1998-01-01

    This disclosure provides a solar rechargeable aircraft that is inexpensive to produce, is steerable, and can remain airborne almost indefinitely. The preferred aircraft is a span-loaded flying wing, having no fuselage or rudder. Travelling at relatively slow speeds, and having a two-hundred foot wingspan that mounts photovoltaic cells on most all of the wing's top surface, the aircraft uses only differential thrust of its eight propellers to turn. Each of five sections of the wing has one or more engines and photovoltaic arrays, and produces its own lift independent of the other sections, to avoid loading them. Five two-sided photovoltaic arrays, in all, are mounted on the wing, and receive photovoltaic energy both incident on top of the wing, and which is incident also from below, through a bottom, transparent surface. The aircraft is capable of a top speed of about ninety miles per hour, which enables the aircraft to attain and can continuously maintain altitudes of up to sixty-five thousand feet. Regenerative fuel cells in the wing store excess electricity for use at night, such that the aircraft can sustain its elevation indefinitely. A main spar of the wing doubles as a pressure vessel that houses hydrogen and oxygen gasses for use in the regenerative fuel cell. The aircraft has a wide variety of applications, which include weather monitoring and atmospheric testing, communications, surveillance, and other applications as well.

  1. 12. Interior view of battle staff compartment showing the general's ...

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

    12. Interior view of battle staff compartment showing the general's chair. View toward front of aircraft. - Offutt Air Force Base, Looking Glass Airborne Command Post, Looking Glass Aircraft, On Operational Apron covering northeast half of Project Looking Glass Historic District, Bellevue, Sarpy County, NE

  2. Optimal Scheduling and Operating Target (OPTAR) Cost Model for Aircraft Carriers in the Fleet Response Plan

    DTIC Science & Technology

    2008-09-01

    depot maintenance. An additional carrier is always conducting a 3-year midlife Refueling and Complex Overhaul (RCOH) and is not included in the FRTP...to anticipate; • The economic benefits of forward-deployed naval forces, as illustrated by the impact of naval crisis response on oil futures’ prices

  3. Annual Review of Aircraft Accident Data. US Carrier Operations Calendar Year 1997

    DTIC Science & Technology

    2002-01-24

    U.S. AIR CARRIER OPERATIONS 1987 - 1997 Number of Accidents by Segements of Aviation Involved Accidents S135 N135 N135 S121 Total and and and and Year...planning/decision 1 1 Lack of familiarity with geographic area 1 0 Proper alignment 1 1 Raising of flaps 1 0 Refueling 1 0 Self-induced pressure 1 0

  4. Battle Force Capabilities/Mission Capabilities Packages

    DTIC Science & Technology

    2007-11-02

    DDG - 51 AEGIS Cruisers CG- 47 Aircraft Carriers C V Other AAW Ships CGN -36/38, DDG - 993 Other AAW Ships FFG...31 CRC CRE Weapons F-15 F- 16 Force AOC AEGIS Destroyers DDG - 51 AEGIS Cruisers CG- 47 Aircraft Carriers C V Other AAW Ships CGN -36/38, DDG - 993 Other...CG- 47 Aircraft Carriers C V Other AAW Ships CGN -36/38, DDG - 993 Other AAW Ships FFG- 7 Other Ships Force AAMDC FPTOC Control Weapons Army USMC

  5. Visible Battle Rhythm

    DTIC Science & Technology

    2006-06-01

    2006 Oculus Info Inc. COP21 TD 1 Visible Battle Rhythm Brian Cort1, Alain Bouchard2, Denis Gouin2, Pascale Proulx1, Bill Wright1 June 21, 2006 1...Oculus Info Inc. 2 DRDC Valcartier www.oculusinfo.com www.drdc-rddc.gc.ca © 2006 Oculus Info Inc. COP21 TD 2 Battle Rhythm “Process where the...commander to make timely decisions.” −Duffy et al, 2004 © 2006 Oculus Info Inc. COP21 TD 3 Visible Battle Rhythm • Real-time coordination and synchronization

  6. 9 CFR 71.6 - Carrier responsible for cleaning and disinfecting of railroad cars, trucks, boats, aircraft or...

    Code of Federal Regulations, 2011 CFR

    2011-01-01

    ... disinfecting of railroad cars, trucks, boats, aircraft or other means of conveyance. 71.6 Section 71.6 Animals... for cleaning and disinfecting of railroad cars, trucks, boats, aircraft or other means of conveyance. (a) Railroad cars, trucks, boats, aircraft, and other means of conveyance which have been used in...

  7. 9 CFR 71.6 - Carrier responsible for cleaning and disinfecting of railroad cars, trucks, boats, aircraft or...

    Code of Federal Regulations, 2014 CFR

    2014-01-01

    ... disinfecting of railroad cars, trucks, boats, aircraft or other means of conveyance. 71.6 Section 71.6 Animals... for cleaning and disinfecting of railroad cars, trucks, boats, aircraft or other means of conveyance. (a) Railroad cars, trucks, boats, aircraft, and other means of conveyance which have been used in...

  8. Battle of France WWII

    NASA Astrophysics Data System (ADS)

    Gadhath, Arpitha Rao

    The purpose of this thesis is to build an interactive Geographical Information System (GIS) tool, relating to the series of events that occurred during the Battle of France World War II. The tool gives us an insight about the countries involved in the battle, their allies and their strategies. This tool was created to use it as a one stop source of information regarding all the important battles that took place, which lead to the fall of France. The tool brings together the maps of all the countries involved. Integrated with each map is the data relevant to that map. The data for each country includes the place of attack, the strategies used during the attack, and the kind of warfare. The tool also makes use of HTML files to give all the information, along with the images from the time of the war and a footage which explains everything about the particular battle. The tool was build using JAVA, along with the use of MOJO (Map Objects Java Objects) to develop Maps of each of the countries. MOJO is developed by ESRI (Environmental Science Research Institute) which makes it easier to add data to the maps. It also makes highlighting important information easier making use of pop-up windows, charts and infographics. HTML files were designed making use of the open-source template developed by Bootstrap. The tool is built in such a way that the interface is simple and easy for the user to use and understand.

  9. Battle Staff Integration

    DTIC Science & Technology

    1992-02-01

    This paper sets forth a research-based conceptual framework for understanding and addressing battle staff functioning and its relation to the...organizational theories and concepts is included, and the concept of team work and the characteristics of effective teams are discussed. A conceptual ... framework is presented for teamwork in problem-solving and decision-making activities within hierarchical organizations.

  10. Planning for Battle

    ERIC Educational Resources Information Center

    Plummer, David; Johnson, Wallace

    2008-01-01

    The concept of "the fog of war" brings to mind the chaos of smoke-covered battlefields, along with the randomness inherent in any rapidly developing situation. The term is used most often to illustrate the difficulty military commanders have getting accurate information while a battle is being fought. Sketchy and often inaccurate information…

  11. Battle Command Staff Training

    DTIC Science & Technology

    1992-12-01

    collective performance. There are a variety of ideas that need attention, ranging Lvm how * staffs should operate vertically , how to measure staff...4-12 Preparation for Vertical BCST .........................................lC S...1.1-1 Appendix 1.2- Vertical BCST-Fire Support ........................................ 1.2-1 Appendix 1.3- Conceptual Innovations in Battle

  12. 9 CFR 71.6 - Carrier responsible for cleaning and disinfecting of railroad cars, trucks, boats, aircraft or...

    Code of Federal Regulations, 2012 CFR

    2012-01-01

    ... 9 Animals and Animal Products 1 2012-01-01 2012-01-01 false Carrier responsible for cleaning and... and Animal Products ANIMAL AND PLANT HEALTH INSPECTION SERVICE, DEPARTMENT OF AGRICULTURE INTERSTATE TRANSPORTATION OF ANIMALS (INCLUDING POULTRY) AND ANIMAL PRODUCTS GENERAL PROVISIONS § 71.6 Carrier...

  13. 9 CFR 71.6 - Carrier responsible for cleaning and disinfecting of railroad cars, trucks, boats, aircraft or...

    Code of Federal Regulations, 2013 CFR

    2013-01-01

    ... 9 Animals and Animal Products 1 2013-01-01 2013-01-01 false Carrier responsible for cleaning and... and Animal Products ANIMAL AND PLANT HEALTH INSPECTION SERVICE, DEPARTMENT OF AGRICULTURE INTERSTATE TRANSPORTATION OF ANIMALS (INCLUDING POULTRY) AND ANIMAL PRODUCTS GENERAL PROVISIONS § 71.6 Carrier...

  14. Self-Directed Violence Aboard U.S. Navy Aircraft Carriers: An Examination of General and Shipboard-Specific Risk and Protective Factors.

    PubMed

    Saitzyk, Arlene; Vorm, Eric

    2016-04-01

    Self-directed violence (SDV), which includes suicidal ideation with and without intent, suicidal preparatory behaviors and attempts with and without harm, non-suicidal self-directed violence, and completed suicide, has been a rising concern in the military. Military shipboard personnel may represent a unique subset of this population due to the distinct nature of deployment stressors and embedded supports. As such, one might expect differences in the prevalence of SDV between this group and other active duty personnel, signifying a distinct operational impact. This study analyzed the prevalence of SDV among personnel assigned or deployed to U.S. Navy aircraft carriers, and examined whether occurrences varied by descriptors commonly identified in the literature (e.g., age, gender, marital status, pay grade/rank). This study also examined characteristics specific to life aboard a U.S. Navy aircraft carrier in order to better understand the issues particular to this population. Descriptive analyses and relative risk findings suggested similarities in demographic risk factors to the general military population, but also striking differences related to occupational specialty and assigned department. This study is the first to shed light on risk and protective factors relevant to shipboard personnel.

  15. Aircraft Survivability. Spring 2011

    DTIC Science & Technology

    2011-01-01

    advancing and applying technology to predict, evaluate , and improve combat survivability of US flight vehicles. John graduated from the University of...support for most of the aircraft and anti-aircraft programs conducted to date under LFT&E statutory requirements. A number of these test and evaluation ...initiatives to improve the state-of-the-art of LFT&E, to place greater emphasis on the evaluation of human casualties, to integrate Battle Damage

  16. [Psychophysiological aspects of naval aviation pilots of the Navy in the operation of highly carrier-based aircraft].

    PubMed

    Mel'nik, S G; Chulaevskiĭ, A O

    2011-08-01

    The authors have shown that the most difficult elements of the flight deck of the ship are springboard takeoff and aerofinishing landing. An important task is to study the aerodynamic characteristics of the behavior of the aircraft during takeoff different characteristics, forming crews ready to act in particular situations. Adverse factors are the operating conditions of habitability of aircraft (noise, vibration, fumes in the air at work, and aircraft engines, etc.) that have a significant impact on the life of air crew and engineering staff. It is concluded that the development and use of effective means of protecting the organism from the effect of these factors is a priority for specialists in aviation medicine.

  17. Airland Battle Doctrine

    DTIC Science & Technology

    1988-09-01

    follow-on forces attack ( FOFA ) doctrine. These critics believe that NATO, with the FOFA concept, already has the flexibility to carry the battle to...confusing and redundant and that it would cause the U.S. to pursue a course independent of the rest of NATO. FOFA is thought by many to address the problem of...for the processing and analysis of intelligence data, make possible "natural language" recognition, give "vision" ability to target acquisition and

  18. Battle Space Action Centers

    DTIC Science & Technology

    2011-05-14

    VREEDE, G. J. D., & KOLFSCHOTEN, G. L . (2008). Extending the contextual and organizational elements of adaptive structurization theory in GSS...Reiter-Palmon, R., & Harland, L . (2009). Computer Assisted Collaboration Engineering and Process Support Systems: The BattleSpace ActionCenters...Collaboration Science, 27 February, University of Nebraska at Omaha, Omaha, NE. 18. BRIGGS, R.O., VREEDE, G.J. DE, REITER-PALMON, R., HARLAND, L

  19. Studies in Battle Command

    DTIC Science & Technology

    1995-01-01

    Creek stronghold at Horseshoe Bend . Red Eagle and some 1,500 Creeks had fortified a peninsula there by erecting a substantial breastwork along its... Horseshoe Bend proved decisive. A proud but defeated Red Eagle surrendered himself to General Jackson in April, stating that “If I had an army, I 23...STUDIES IN BATTLE COMMAND By the Faculty Combat Studies Institute U.S. Army Command and General Staff ColIege Fort Leavenworth, Kansas IES

  20. Battle Management Language Transformations

    DTIC Science & Technology

    2006-10-01

    usability and the effectiveness of selected technologies for C2 – simulation interoperation. This demonstrator was tested operationally during a Brigade...execute in the simulation to evaluate the COA. Figure 4: Initial Conditions as displayed on APLET Battle Management Language Transformations RTO-MP...representational foundation capable of supporting cognitive and automated processes. These functions apply not only to the current C2-Simulation role, but also

  1. Aircraft Survivability: Aircraft Battle Damage and Repair, Summer 2007

    DTIC Science & Technology

    2007-01-01

    Christina P. McNemar Phone: 703/984–0733 mcnemar_christina@bah.com Creative Director K. Ahnie Jenkins Art Director Donald Rowe Technical Editor...Calendar of Events may be sent to: SURVIAC, Washington Satellite Office Attn: Christina McNemar 13200 Woodland Park Road, Suite 6047 Herndon, VA 20171 Phone

  2. Particle Image Velocimetry Measurements to Evaluate the Effectiveness of Deck-Edge Columnar Vortex Generators on Aircraft Carriers

    NASA Technical Reports Server (NTRS)

    Landman, Drew; Lamar, John E.; Swift, Russell

    2005-01-01

    Candidate passive flow control devices were chosen from a NASA flow visualization study to investigate their effectiveness at improving flow quality over a flat-top carrier model. Flow over the deck was analyzed using a particle image velocimeter and a 1/120th scaled carrier model in a low-speed wind tunnel. Baseline (no devices) flow quality was compared to flow quality from combinations of bow and deck-edge devices at both zero and 20 degrees yaw. Devices included plain flaps and spiral cross-section columnar vortex generators attached in various combinations to the front and sides of the deck. Centerline and cross plane measurements were made with velocity and average turbulence measurements reported. Results show that the bow/deck-edge flap and bow/deck-edge columnar vortex generator pairs reduce flight deck turbulence both at zero yaw and at 20 degrees yaw by a factor of approximately 20. Of the devices tested, the most effective bow-only device appears to be the plain flap.

  3. Ohio incinerator battle continues

    SciTech Connect

    Melody, M.

    1993-05-01

    Waste Technologies Industries (WTI; East Liverpool, Ohio) is trying to wing what it hopes will be its final battle in a 13-year, $160 million war with the government, and community and environmental groups. The company since 1980 has sought EPA approval to operate a hazardous waste incinerator in East Liverpool, Ohio. WTI late last year conducted a pre-test burn, or shakedown, during which the incinerator burned certain types of hazardous waste. The test demonstrates the incinerator's performance under normal operating conditions, Regulatory authorities, including EPA and the Ohio Environmental Protection Agency (OEPA), monitored activity during the shakedown, which was limited to 720 hours of operation. In accordance with RCRA requirements, the company in March conducted a trial burn to demonstrate that the incinerator meets permit standards. WTI's permit specifies three performance parameters the incinerator must meet -- particulate and hydrogen chloride emissions limits, and destruction removal efficiencies (DREs).

  4. 77 FR 33083 - Airworthiness Directives; WACO Classic Aircraft Corporation Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-06-05

    ... Aircraft Corporation Airplanes AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule... Aircraft Corporation Models 2T-1A, 2T-1A-1, and 2T-1A-2 airplanes. This AD requires inspection of the front..., contact WACO Classic Aircraft Corporation; 15955 South Airport Rd., Battle Creek, Michigan...

  5. Battling Malaria in Rural Zambia with Modern Technology: A Qualitative Study on the Value of Cell Phones, Geographical Information Systems, Asymptomatic Carriers and Rapid Diagnostic Tests to Identify, Treat and Control Malaria

    PubMed Central

    Isaksson, Arvid Lissel

    2014-01-01

    During the last decade much progress has been made in reducing malaria transmission in Macha, Southern Province, Zambia. Introduction of artemisinin combination therapies as well as mass screenings of asymptomatic carriers is believed to have contributed the most. When an endemic malaria situation is moving towards a non-endemic situation the resident population loses acquired immunity and therefore active case detection and efficient surveillance is crucial to prevent epidemic outbreaks. Our purpose was to evaluate the impact of cell phone surveillance and geographical information systems on malaria control in Macha. Furthermore, it evaluates what screening and treatment of asymptomatic carriers and implementation of rapid diagnostic tests in rural health care has led to. Ten in-depth semi-structured interviews, field observations and data collection were performed at the Macha Research Trust and at surrounding rural health centers. This qualitative method was inspired by rapid assessment procedure. The cell phone surveillance has been easily integrated in health care, and its integration with Geographical Information Systems has provided the ability to follow malaria transmission on a weekly basis. In addition, active case detection of asymptomatic carriers has been fruitful, which is reflected in it soon being applied nationwide. Furthermore, rapid diagnostic tests have provided rural health centers with reliable malaria diagnostics, thereby decreasing excessive malaria treatments and selection for drug resistance. This report reflects the importance of asymptomatic carriers in targeting malaria elimination, as well as development of effective surveillance systems when transmission decreases. Such an approach would be cost-efficient in the long run through positive effects in reduced child mortality and relief in health care. PMID:28299110

  6. Battling Malaria in Rural Zambia with Modern Technology: A Qualitative Study on the Value of Cell Phones, Geographical Information Systems, Asymptomatic Carriers and Rapid Diagnostic Tests to Identify, Treat and Control Malaria.

    PubMed

    Nygren, David; Isaksson, Arvid Lissel

    2014-02-04

    During the last decade much progress has been made in reducing malaria transmission in Macha, Southern Province, Zambia. Introduction of artemisinin combination therapies as well as mass screenings of asymptomatic carriers is believed to have contributed the most. When an endemic malaria situation is moving towards a non-endemic situation the resident population loses acquired immunity and therefore active case detection and efficient surveillance is crucial to prevent epidemic outbreaks. Our purpose was to evaluate the impact of cell phone surveillance and geographical information systems on malaria control in Macha. Furthermore, it evaluates what screening and treatment of asymptomatic carriers and implementation of rapid diagnostic tests in rural health care has led to. Ten in-depth semi-structured interviews, field observations and data collection were performed at the Macha Research Trust and at surrounding rural health centers. This qualitative method was inspired by rapid assessment procedure. The cell phone surveillance has been easily integrated in health care, and its integration with Geographical Information Systems has provided the ability to follow malaria transmission on a weekly basis. In addition, active case detection of asymptomatic carriers has been fruitful, which is reflected in it soon being applied nationwide. Furthermore, rapid diagnostic tests have provided rural health centers with reliable malaria diagnostics, thereby decreasing excessive malaria treatments and selection for drug resistance. This report reflects the importance of asymptomatic carriers in targeting malaria elimination, as well as development of effective surveillance systems when transmission decreases. Such an approach would be cost-efficient in the long run through positive effects in reduced child mortality and relief in health care.

  7. Predictive models of battle dynamics

    NASA Astrophysics Data System (ADS)

    Jelinek, Jan

    2001-09-01

    The application of control and game theories to improve battle planning and execution requires models, which allow military strategists and commanders to reliably predict the expected outcomes of various alternatives over a long horizon into the future. We have developed probabilistic battle dynamics models, whose building blocks in the form of Markov chains are derived from the first principles, and applied them successfully in the design of the Model Predictive Task Commander package. This paper introduces basic concepts of our modeling approach and explains the probability distributions needed to compute the transition probabilities of the Markov chains.

  8. Bibliography of Battle Fatigue Literature

    DTIC Science & Technology

    1986-01-16

    on the shell shock in the wake of the Yom Kippur war). Harefuah, 88(11), 519-521. " Ahrenfeld, R. H. (1958). Psychiatry in the British Army in the...29-37. Belenky, G. L., Tyner, C. F., & Sodetz, F. J. (1983, August). Israeli battle shock casualties (Report WRAIR NP-83-4). Washington, DC: Water Reed...Academic Press. Deeken, M. G. (1985, July). Battle shock during reforger: A case report. Medical Bulletin of the U.S. Army, Europe, 42(7), 14-16

  9. Sea level rise and the ongoing Battle of Tarawa

    NASA Astrophysics Data System (ADS)

    Donner, Simon

    2012-04-01

    At dawn on 20 November 1943, U.S. marines launched an assault on Tarawa, a Japanese-held atoll in the British Protectorate of the Gilbert and Ellice Islands. The water in the lagoon was only 3 feet deep that morning, less than the 4-5 feet required by a fully loaded personnel carrier to navigate the waters. As a result, marines saddled with equipment were forced to wade almost a mile across the lagoon under heavy Japanese fire. The United States won the Battle of Tarawa, but it proved to be one of the bloodiest battles of the war; almost 6000 Japanese, Americans, and Gilbertese were killed in just 3 days of fighting. Of the American fatalities, almost half occurred because U.S. military planners ignored warnings about the local tides on the morning of the assault [e.g., Wright, 2000].

  10. Otolaryngic health service support in the airland battle.

    PubMed

    Zajtchuk, J T

    1989-05-01

    The Blast Injuries of the Ear Seminar was conducted to better define the state of knowledge about the medical care and consequences of blast injuries of the ear in battle. The immediate concern of this discussion was the relative importance of the finding of widespread eardrum ruptures in penetrating attacks by shaped charge munitions against the Bradley Fighting Vehicle and the M113 Armored Personnel Carrier. In order to focus on the care of the soldier with such injuries, a brief description of the current medical care and evacuation chain of the US Army, as well as the proposed future evacuation chain in the Airland Battle scenario, will be discussed. Detailed treatment of patients will be discussed in the descriptions from the Quad Service Clinical Data Base regarding wounds of the tympanic membrane. Most blast injuries of the ear would not be considered as incapacitating casualties by the Army Medical Department, except in severe circumstances.

  11. The Civil War Battle that Helped Create a State

    ERIC Educational Resources Information Center

    Chick, Kay A.

    2009-01-01

    The Battle of Bull Run is routinely cited as the first land battle of the Civil War. This battle between Union and Confederate forces took place near Manassas, Virginia, on July 21, 1861. But was this battle really the initial skirmish between the North and the South? Historians today concede that the first land battle actually took place on June…

  12. 59. Credit FM. Flood waters on South Battle Creek next ...

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

    59. Credit FM. Flood waters on South Battle Creek next to powerhouse. Note height of water in relation to tailraces. - Battle Creek Hydroelectric System, Battle Creek & Tributaries, Red Bluff, Tehama County, CA

  13. A Combat Battle Damage Assessor Expert System,

    DTIC Science & Technology

    1984-05-01

    Next, the requirements should receive just enough repair to allow for the battle damage assessor software it to be flown to a rear area for complete are...R’ D-Ai48 898 A COMBAT BATTLE DAMAGE ASSESSOR EXPERT SYSTEM(U) AIR 1/i FORCE WRIGHT AERONAUTICAL LABS WRIGHT-PATTERSON AFB ON D E NELSON MAY 84 SBI...8217.c.sw-x -: "--..... . .. .-. :;.-...... .............. .. . .. . . .. . .. . . r74 IV A COMBAT BATTLE DAMAGE ASSESSOR EXPERT SYSTEM DAL E. NELSON

  14. A Comparative Analysis of a CV Helicopter and a JVX (Joint Services Advanced Vertical Lift) Tilt-Rotor Aircraft in an Aircraft Carrier Based ASW (anti-Submarine Warfare)

    DTIC Science & Technology

    1985-03-01

    D. SEARCH AND RESCUE -------------------------- 36 E. SUMMARY ------------------------------------ 45 III . COMPARISON OF THE AIRCRAFT IN A SIMULATED...aircraft may respond to contacts generated by remote sources either from an airborne or an on-deck five minute alert status. Once the dipping sonar...scenarios are modeled. The model and results are described in Chapter III . Conclusions and recommendations for further study are contained in Chapter

  15. Census U.S. Civil Aircraft: Calendar Year 1990

    DTIC Science & Technology

    1990-12-31

    Model Aircraft/ No. Air Carrier Aviation Aircraft Places Engine Type Engines R X6- 146 ....................................................... 1 20 0 0... model , and general aviation aircraft by state and county of the owner. 17. Key Words 18. Distribution Statement Air carrier, general aviation, Document...aircraft by make and model . Latest edition: ..................... .Calendar Year 1990 Order from: ........................ U.S. Government Printing Office

  16. The Battling 'Bots of Bloomsburg High

    ERIC Educational Resources Information Center

    Gorman, Lynn

    2007-01-01

    In this article, the author describes how students in Kirk Marshall's industrial technology class at Bloomsburg Area High School, Pennsylvania, designed and manufactured battling robots (BattleBots) and their participation in an annual national robotics competition. According to Marshall, designing and building a complex robot would be virtually…

  17. Carrier Landing Parameters from Survey 45, Fleet and Training Command Aircraft Landing Aboard USS ENTERPRISE CVN-65 (Appendices B Through R)

    DTIC Science & Technology

    1991-12-01

    nu B-3 NADC-91124-0 MODEL F-14A AIRCRAFT USS ENTERPRISE (CVN-65) DAY LANDINGS FRESNEL LENS SETTING-3.50 DEGREES (.061 RADIANS) N-158 X-27.85 KNOTS...ENTERPRISE (CVN-65) DAY LANDINGS FRESNEL LENS SETTING-3.50 DEGREES (.061 RADIANS) N-158 1-27.85 KNOTS (14.32 METRES/SEC) A3-.38 S-3.39 KNOTS (1.74 XETRES...AIRCRAFT USS ENTERPRISE (CVN-65) DAY LANDINGS FRESNEL LENS SETTING-3.50 DEGREES (.061 RADIANS) N-158 1-140.43 KNOTS (72.24 METRES/SEC) A3--.01 8-4.03 KNOTS

  18. Distributed rf sensor systems for battle group defense. Final report

    SciTech Connect

    Not Available

    1985-08-01

    As exemplified by the Falkland's war, a stationary battle group is especially vulnerable to attack by small, low-flying missiles. Shipboard sensors are unable to provide timely alerting of such an attack to the various defensive elements because the low-flying attacking missile is over the horizon and invisible to radars until it pops over the horizon near the ships. Even at the time, it is difficult to see because it is lost in background sea clutter. An early alerting technique is needed. The concept is that of a fence of radar buoys, deployed in an arc at 65 km to 130 km from the ship group in a direction identified as a potential threat axis. The buoys would be expendable, operate for 10 hours on station, by deployed by P-3 or S-2 ASW aircraft, and would communicate detection alarms to the ship group by HF radio.

  19. Loftin Collection - Boeing Aircraft

    NASA Technical Reports Server (NTRS)

    1933-01-01

    Either a F2B-1 or F3B-1, both aircraft were built by Boeing and both were powered by Pratt and Whitney Wasp engines. These fighters were intended for Navy shipboard use. Boeing F3B-1: While most Boeing F3B-1s served the U. S. Navy aircraft carriers the Lexington and the Saratoga, this example flew in NACA hands at the Langley Memorial Aeronautical Laboratory in the late 1920's. Also known as the Boeing Model 77, the aircraft was the next to last F3B-1 build in November 1928.

  20. OVRhyp, Scramjet Test Aircraft

    NASA Technical Reports Server (NTRS)

    Aslan, J.; Bisard, T.; Dallinga, S.; Draper, K.; Hufford, G.; Peters, W.; Rogers, J.

    1990-01-01

    A preliminary design for an unmanned hypersonic research vehicle to test scramjet engines is presented. The aircraft will be launched from a carrier aircraft at an altitude of 40,000 feet at Mach 0.8. The vehicle will then accelerate to Mach 6 at an altitude of 100,000 feet. At this stage the prototype scramjet will be employed to accelerate the vehicle to Mach 10 and maintain Mach 10 flight for 2 minutes. The aircraft will then decelerate and safely land.

  1. Hypersonic reconnaissance aircraft

    NASA Technical Reports Server (NTRS)

    Bulk, Tim; Chiarini, David; Hill, Kevin; Kunszt, Bob; Odgen, Chris; Truong, Bon

    1992-01-01

    A conceptual design of a hypersonic reconnaissance aircraft for the U.S. Navy is discussed. After eighteen weeks of work, a waverider design powered by two augmented turbofans was chosen. The aircraft was designed to be based on an aircraft carrier and to cruise 6,000 nautical miles at Mach 4;80,000 feet and above. As a result the size of the aircraft was only allowed to have a length of eighty feet, fifty-two feet in wingspan, and roughly 2,300 square feet in planform area. Since this is a mainly cruise aircraft, sixty percent of its 100,000 pound take-off weight is JP fuel. At cruise, the highest temperature that it will encounter is roughly 1,100 F, which can be handled through the use of a passive cooling system.

  2. Aircraft Disinsection: A Guide for Military and Civilian Air Carriers (Desinsectisation des aeronefs: Un guide a l’intention des responsables des transports aeriens civils et militaires)

    DTIC Science & Technology

    1996-04-01

    D.K. Hayes, K. Stalker, and R. Pal, 1978. A comparison of Freon- and water -based insecticidal aerosols for air- craft disinsection. Bull. WHO 56(1):129...Chemical Pest Management Decision-making 32 12.2 Scheduling Insecticide Treatments 33 vi 12.3 Insecticide Selection 34 12.4 Equipment and Materials...walk to Aircraft Connections 42 12.7 Use of Insecticidal Baits 42 12.8 Fumigation 42 12.8.1 Fumigation with Methyl Bromide 42 12.8.2 Fumigation

  3. Corps Communications for the Airland Battle

    DTIC Science & Technology

    1985-04-01

    PROUOTABLE) DAVID J. KELLEY, SC LIEUTENANT COLONEL CLINTON A. BOOTH. SC LIEUTENANT COLONEL RICHARD P. BflADDOCK. SC ^/ DTIC ELECTE JUN 5 «66...Communications for the Airland Battle 7. AUTHORf«) COL Alan B. Cupples LTC(P) David J. Kelley LTC Clinton A. Booth LTC Richard P. Braddock ». PERFORMING...FOR THE AIRLAND BATTLE A GROUP STUDY PROJECT BY Colonel Alan B. Cupples, SC Lieutenant Colonel (Promotable) David J. Kelley, SC Lieutenant

  4. 14 CFR 291.22 - Aircraft accident liability insurance requirement.

    Code of Federal Regulations, 2012 CFR

    2012-01-01

    ... 14 Aeronautics and Space 4 2012-01-01 2012-01-01 false Aircraft accident liability insurance... for All-Cargo Air Transportation § 291.22 Aircraft accident liability insurance requirement. No air carrier shall operate all-cargo aircraft or provide all-cargo air transportation unless such carrier...

  5. 14 CFR 252.13 - Small aircraft.

    Code of Federal Regulations, 2013 CFR

    2013-01-01

    ... 14 Aeronautics and Space 4 2013-01-01 2013-01-01 false Small aircraft. 252.13 Section 252.13 Aeronautics and Space OFFICE OF THE SECRETARY, DEPARTMENT OF TRANSPORTATION (AVIATION PROCEEDINGS) ECONOMIC REGULATIONS SMOKING ABOARD AIRCRAFT § 252.13 Small aircraft. Air carriers shall prohibit smoking on...

  6. 14 CFR 252.13 - Small aircraft.

    Code of Federal Regulations, 2014 CFR

    2014-01-01

    ... 14 Aeronautics and Space 4 2014-01-01 2014-01-01 false Small aircraft. 252.13 Section 252.13 Aeronautics and Space OFFICE OF THE SECRETARY, DEPARTMENT OF TRANSPORTATION (AVIATION PROCEEDINGS) ECONOMIC REGULATIONS SMOKING ABOARD AIRCRAFT § 252.13 Small aircraft. Air carriers shall prohibit smoking on...

  7. 14 CFR 252.13 - Small aircraft.

    Code of Federal Regulations, 2010 CFR

    2010-01-01

    ... 14 Aeronautics and Space 4 2010-01-01 2010-01-01 false Small aircraft. 252.13 Section 252.13 Aeronautics and Space OFFICE OF THE SECRETARY, DEPARTMENT OF TRANSPORTATION (AVIATION PROCEEDINGS) ECONOMIC REGULATIONS SMOKING ABOARD AIRCRAFT § 252.13 Small aircraft. Air carriers shall prohibit smoking on...

  8. 14 CFR 252.13 - Small aircraft.

    Code of Federal Regulations, 2012 CFR

    2012-01-01

    ... 14 Aeronautics and Space 4 2012-01-01 2012-01-01 false Small aircraft. 252.13 Section 252.13 Aeronautics and Space OFFICE OF THE SECRETARY, DEPARTMENT OF TRANSPORTATION (AVIATION PROCEEDINGS) ECONOMIC REGULATIONS SMOKING ABOARD AIRCRAFT § 252.13 Small aircraft. Air carriers shall prohibit smoking on...

  9. 14 CFR 252.13 - Small aircraft.

    Code of Federal Regulations, 2011 CFR

    2011-01-01

    ... 14 Aeronautics and Space 4 2011-01-01 2011-01-01 false Small aircraft. 252.13 Section 252.13 Aeronautics and Space OFFICE OF THE SECRETARY, DEPARTMENT OF TRANSPORTATION (AVIATION PROCEEDINGS) ECONOMIC REGULATIONS SMOKING ABOARD AIRCRAFT § 252.13 Small aircraft. Air carriers shall prohibit smoking on...

  10. The battle over workers' compensation.

    PubMed

    Ellenberger, J N

    2000-01-01

    Faced with lower profits and rapidly increasing premium costs in the 1980s, insurers and employer organizations cleverly parlayed the public perception of worker fraud and abuse in the workers' compensation system (that they helped to create) into massive legislative changes. Over the last decade, state legislators and governors, Republican and Democrat alike, have jumped on this bandwagon, one that workers and their allies have dubbed the workers' compensation "deform" movement. Alleging a "game plan" and a calculated campaign on the part of insurers and employers, the author looks at the major components of changes that were made, examines the elements of workers' compensation over which employers and insurers have gained control, and discusses Newt Gingrich's efforts to capitalize on employer and insurer fervor over the system. This campaign whistled through the country until it goaded the labor movement, injured workers, the trial bar, and others in Ohio in 1997 to organize themselves to stand up to employers by defeating the deform law through a ballot initiative. The article details that battle and suggests that similar voices can be achieved through a return to grassroots organizing and mobilization.

  11. Epidemiology of Helicopter Battle Damage

    DTIC Science & Technology

    2010-05-01

    A through Class C accident data , and consider the data to be representative of the spectrum of damage that must be dealt with by deployed...maintenance units. An analysis of the data by year dating back to 1995 was done to look at the effect of OIF and OEF on overall aircraft incident rate. This...per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and

  12. 75 FR 9327 - Aircraft Noise Certification Documents for International Operations

    Federal Register 2010, 2011, 2012, 2013, 2014

    2010-03-02

    ... the aircraft flight manual and approved as part of the aircraft's airworthiness certification, and... Airplane Flight Manual (AFM) or Rotorcraft Flight Manual (RFM) as part of an aircraft's certification... operating under part 121, a carrier is allowed to create an Aircraft Operations Manual (AOM) or a...

  13. 14 CFR 252.11 - Aircraft on the ground.

    Code of Federal Regulations, 2014 CFR

    2014-01-01

    ... 14 Aeronautics and Space 4 2014-01-01 2014-01-01 false Aircraft on the ground. 252.11 Section 252...) ECONOMIC REGULATIONS SMOKING ABOARD AIRCRAFT § 252.11 Aircraft on the ground. (a) Air carriers shall prohibit smoking whenever the aircraft is on the ground. (b) With respect to the restrictions on...

  14. 14 CFR 252.11 - Aircraft on the ground.

    Code of Federal Regulations, 2010 CFR

    2010-01-01

    ... 14 Aeronautics and Space 4 2010-01-01 2010-01-01 false Aircraft on the ground. 252.11 Section 252...) ECONOMIC REGULATIONS SMOKING ABOARD AIRCRAFT § 252.11 Aircraft on the ground. (a) Air carriers shall prohibit smoking whenever the aircraft is on the ground. (b) With respect to the restrictions on...

  15. 14 CFR 252.11 - Aircraft on the ground.

    Code of Federal Regulations, 2013 CFR

    2013-01-01

    ... 14 Aeronautics and Space 4 2013-01-01 2013-01-01 false Aircraft on the ground. 252.11 Section 252...) ECONOMIC REGULATIONS SMOKING ABOARD AIRCRAFT § 252.11 Aircraft on the ground. (a) Air carriers shall prohibit smoking whenever the aircraft is on the ground. (b) With respect to the restrictions on...

  16. 14 CFR 252.11 - Aircraft on the ground.

    Code of Federal Regulations, 2012 CFR

    2012-01-01

    ... 14 Aeronautics and Space 4 2012-01-01 2012-01-01 false Aircraft on the ground. 252.11 Section 252...) ECONOMIC REGULATIONS SMOKING ABOARD AIRCRAFT § 252.11 Aircraft on the ground. (a) Air carriers shall prohibit smoking whenever the aircraft is on the ground. (b) With respect to the restrictions on...

  17. 14 CFR 252.11 - Aircraft on the ground.

    Code of Federal Regulations, 2011 CFR

    2011-01-01

    ... 14 Aeronautics and Space 4 2011-01-01 2011-01-01 false Aircraft on the ground. 252.11 Section 252...) ECONOMIC REGULATIONS SMOKING ABOARD AIRCRAFT § 252.11 Aircraft on the ground. (a) Air carriers shall prohibit smoking whenever the aircraft is on the ground. (b) With respect to the restrictions on...

  18. Armored Battle Groups in the 21st Century

    DTIC Science & Technology

    1989-03-31

    ARMORED BATTLE GROUPS IN THE 21ST CENTURY BY LIEUTENANT COLONEL WENDELL D. KOT )STIRUMtN STATE9M A: Approved fer public releft. distribution is izulatated...RECIPIENT’S CATALOG NUMBER 4. TITLE (’ Subtitle) 5. TYPE OF REPORT & PERIOD COVERED ARMORED BATTLE GROUPS IN THE 21ST CENTURY i Individual Study Project 6...alternative to today’s heavy division force structure - Armored Battle Groups is examined. The Armored Battle Group organization devel- oped in the paper

  19. NASA's Original Shuttle Carrier Departs Dryden

    NASA Video Gallery

    NASA's Space Shuttle Carrier Aircraft (SCA) No. 905, departed NASA's Dryden Flight Research Center on Oct. 24, 2012 for the final time, ending a 38-year association with the NASA field center at Ed...

  20. Carrier Diagnosis

    MedlinePlus

    ... and Women with Hemophilia Inheritance of Hemophilia Definitions & Terminology Bleeding Symptoms Carrier Diagnosis When to Test for ... and Women with Hemophilia Inheritance of Hemophilia Definitions & Terminology Bleeding Symptoms Carrier Diagnosis When to Test for ...

  1. The Decisiveness of the Battle of Midway

    DTIC Science & Technology

    2015-06-12

    College in partial fulfillment of the requirements for the degree MASTER OF MILITARY ART AND SCIENCE Military History by ANDRES J...treatment. To challenge the basic assumptions made about the strategic effects of this battle might not only provide a more accurate view of history , but...

  2. The Battle for Open--A Perspective

    ERIC Educational Resources Information Center

    Weller, Martin

    2013-01-01

    In this article the author argues that openness in education has been successful in establishing itself as an approach. However, this initial victory should be viewed as part of a larger battle around the nature of openness. Drawing lessons from history and the green movement, a number of challenges for the open education movement are identified…

  3. Battle of Laurel Hill - May 1864.

    DTIC Science & Technology

    1986-03-31

    and burning furiously in every direction, and there was no suitable place for a rest. The road by which I was conducted was narrow and frequently... happy mistake they were fighting themselves. It seemed a heavy battle and we had nothing to do with it."(187> (See Figure 19) Federal accounts report

  4. Battle over proposed Keystone pipeline continues

    NASA Astrophysics Data System (ADS)

    Showstack, Randy

    2013-07-01

    Opposing sides in the battle over the proposed construction of the controversial Keystone XL pipeline continue to push their messages on the issue. The American Petroleum Institute (API) announced on 9 July that it has launched a new advertising campaign in support of the pipeline, which, if built, will ship oil from Canadian tar sands to refineries in the Gulf of Mexico.

  5. "Losing Battles": The Tests of Endurance.

    ERIC Educational Resources Information Center

    Rienstra, Phillis

    The works of Eudora Welty challenge the abilities of the oral reader who wishes to interpret them properly. Her novel, "Losing Battles," requires careful attention to the narrative point of view as a guide to its various dimensions of meaning. The narrative shifts through the consciousnesses of various characters of four generations in a rural…

  6. SHRUB BATTLE: Understanding the Making of Landscape

    ERIC Educational Resources Information Center

    Depigny, Sylvain; Michelin, Yves

    2007-01-01

    Landscape changes in Europe's rural areas seem to generate a more visible impact. This trend raises new questions on rural management and brings about a conflict between farmers' land-use patterns and public expectations, which are often exclusively based on esthetics. The aim of the SHRUB BATTLE board game is to help tutors make future rural…

  7. A Rhetoric of Ultimacy: Battle Orations.

    ERIC Educational Resources Information Center

    Bliese, John

    The rhetorical strategies of the speechmaker become more interesting as the involvement and risk assumed by the audience increase. Battle orations given by military leaders to their troops just before fighting the enemy provide the ultimate in audience involvement and risk. Of some 200 chronicles of northern Europe from the twelfth and thirteenth…

  8. The Gaugamela Battle Eclipse: An Archaeoastronomical Analysis

    NASA Astrophysics Data System (ADS)

    Polcaro, V. F.; Valsecchi, G. B.; Verderame, L.

    A total lunar eclipse occurred during the night preceding the decisive Battle of Gaugamela (20th September 331 BCE), when the Macedonian army, led by Alexander the Great, finally defeated the Persian king Darius and his army. This astronomical event, well known to historians, had a relevant role on the battle outcome. The eclipse was described in detail by Babylonian astronomers, though, unfortunately, the text of their report has only partially been preserved. We have reconstructed the evolution of the phenomenon as it appeared to the observer in Babylonia, by using the positional astronomy code "Planetario V2.0". On the base of this reconstruction we suggest a number of integrations to the lost part of the text, allowing a finer astrological interpretation of the eclipse and of its influence on the mood of the armies that set against each other on the following morning.

  9. Strategic Insights: The Battle of Crecy

    DTIC Science & Technology

    2011-03-20

    United States Army Dr. Richard Meinhart Project Adviser This SRP is submitted in partial fulfillment of the requirements of the...St ra te gy R es ea rc h Pr oj ec t STRATEGIC INSIGHTS: THE BATTLE OF CRECY BY LIEUTENANT COLONEL KENNETH ERNEST KOPS United States Army ...reflect the official policy or position of the Department of the Army , Department of Defense, or the U.S. Government. U.S. Army War College, Carlisle

  10. Small SDI battle stations - More is better

    SciTech Connect

    Cornet, E.

    1986-09-01

    It is presently suggested that large numbers of lower capability SDI systems, in contrast to small numbers of large battle stations, offer better overall defense performance at lower total cost, with lower technical risk, lower sensitivity to threat scenario variability, and improved survivability. This follows from such factors as the positioning of more platforms within effective range of targets during all phases of an attack, less exacting optics requirements, mass production economies-of-scale, and improved survivability.

  11. Battle Force Email (BFEM) and other HF Issues

    DTIC Science & Technology

    2007-11-02

    SMTP / POP3 E - Mail messages " Data speeds up to 9.6KBPS coded (half duplex) point-to-point ! Provides inter-ship user-to-user...of the Battle Force E - mail 66 system . 14. SUBJECT TERMS IATAC Collection, battle force, email, system , network, server, 15. NUMBER OF PAGES 14...not achieved in a programmable time period. " Packet operation insures error-free delivery. 00 11 09 N6 BFEM - 6 - Battle Force E - Mail 66 System

  12. 14 CFR 121.538 - Aircraft security.

    Code of Federal Regulations, 2011 CFR

    2011-01-01

    ... 14 Aeronautics and Space 3 2011-01-01 2011-01-01 false Aircraft security. 121.538 Section 121.538 Aeronautics and Space FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION (CONTINUED) AIR CARRIERS..., FLAG, AND SUPPLEMENTAL OPERATIONS Flight Operations § 121.538 Aircraft security. Certificate...

  13. 14 CFR 121.538 - Aircraft security.

    Code of Federal Regulations, 2013 CFR

    2013-01-01

    ... 14 Aeronautics and Space 3 2013-01-01 2013-01-01 false Aircraft security. 121.538 Section 121.538 Aeronautics and Space FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION (CONTINUED) AIR CARRIERS..., FLAG, AND SUPPLEMENTAL OPERATIONS Flight Operations § 121.538 Aircraft security. Certificate...

  14. 333 World Battles; a Bibliography of Periodical Articles (Second Series).

    DTIC Science & Technology

    1978-07-10

    Military Review, 24:28—35, Apr. 1945. AUBERS RIDGE BATTLE 1915 “The Other Side of the Hill ,” Army Quarterly, 36:242—248, Jul. 1938. 2...70, Oct. 1941v BEAUMONT—HAI4EL BATTLE 1916 “The Other Side of the Hill ,” Army Quarter ly, 28:27—36, Apr. 1934. BEIRUT LANDING 1958 “U. S...CONTAI14AISON BATTLE 1916 “The Other Side of the Hill ,” Army Quarterly, 9:245—259, Jan. 1925. CORUNNA BATTLE 1808 “The Night of Corunna , a Contemporary

  15. 14 CFR 252.3 - Smoking ban: air carriers.

    Code of Federal Regulations, 2012 CFR

    2012-01-01

    ... 14 Aeronautics and Space 4 2012-01-01 2012-01-01 false Smoking ban: air carriers. 252.3 Section... PROCEEDINGS) ECONOMIC REGULATIONS SMOKING ABOARD AIRCRAFT § 252.3 Smoking ban: air carriers. Air carriers shall prohibit smoking on all scheduled passenger flights....

  16. 14 CFR 252.3 - Smoking ban: air carriers.

    Code of Federal Regulations, 2013 CFR

    2013-01-01

    ... 14 Aeronautics and Space 4 2013-01-01 2013-01-01 false Smoking ban: air carriers. 252.3 Section... PROCEEDINGS) ECONOMIC REGULATIONS SMOKING ABOARD AIRCRAFT § 252.3 Smoking ban: air carriers. Air carriers shall prohibit smoking on all scheduled passenger flights....

  17. 14 CFR 252.5 - Smoking ban: foreign air carriers.

    Code of Federal Regulations, 2013 CFR

    2013-01-01

    ... 14 Aeronautics and Space 4 2013-01-01 2013-01-01 false Smoking ban: foreign air carriers. 252.5... PROCEEDINGS) ECONOMIC REGULATIONS SMOKING ABOARD AIRCRAFT § 252.5 Smoking ban: foreign air carriers. (a) Foreign air carriers shall prohibit smoking on all scheduled passenger flight segments: (1) Between...

  18. 14 CFR 252.5 - Smoking ban: foreign air carriers.

    Code of Federal Regulations, 2011 CFR

    2011-01-01

    ... 14 Aeronautics and Space 4 2011-01-01 2011-01-01 false Smoking ban: foreign air carriers. 252.5... PROCEEDINGS) ECONOMIC REGULATIONS SMOKING ABOARD AIRCRAFT § 252.5 Smoking ban: foreign air carriers. (a) Foreign air carriers shall prohibit smoking on all scheduled passenger flight segments: (1) Between...

  19. 14 CFR 252.5 - Smoking ban: foreign air carriers.

    Code of Federal Regulations, 2014 CFR

    2014-01-01

    ... 14 Aeronautics and Space 4 2014-01-01 2014-01-01 false Smoking ban: foreign air carriers. 252.5... PROCEEDINGS) ECONOMIC REGULATIONS SMOKING ABOARD AIRCRAFT § 252.5 Smoking ban: foreign air carriers. (a) Foreign air carriers shall prohibit smoking on all scheduled passenger flight segments: (1) Between...

  20. 14 CFR 252.5 - Smoking ban: foreign air carriers.

    Code of Federal Regulations, 2010 CFR

    2010-01-01

    ... 14 Aeronautics and Space 4 2010-01-01 2010-01-01 false Smoking ban: foreign air carriers. 252.5... PROCEEDINGS) ECONOMIC REGULATIONS SMOKING ABOARD AIRCRAFT § 252.5 Smoking ban: foreign air carriers. (a) Foreign air carriers shall prohibit smoking on all scheduled passenger flight segments: (1) Between...

  1. 14 CFR 252.5 - Smoking ban: foreign air carriers.

    Code of Federal Regulations, 2012 CFR

    2012-01-01

    ... 14 Aeronautics and Space 4 2012-01-01 2012-01-01 false Smoking ban: foreign air carriers. 252.5... PROCEEDINGS) ECONOMIC REGULATIONS SMOKING ABOARD AIRCRAFT § 252.5 Smoking ban: foreign air carriers. (a) Foreign air carriers shall prohibit smoking on all scheduled passenger flight segments: (1) Between...

  2. 14 CFR 252.3 - Smoking ban: air carriers.

    Code of Federal Regulations, 2014 CFR

    2014-01-01

    ... 14 Aeronautics and Space 4 2014-01-01 2014-01-01 false Smoking ban: air carriers. 252.3 Section... PROCEEDINGS) ECONOMIC REGULATIONS SMOKING ABOARD AIRCRAFT § 252.3 Smoking ban: air carriers. Air carriers shall prohibit smoking on all scheduled passenger flights....

  3. China’s Aircraft Carrier Dilemma

    DTIC Science & Technology

    2006-01-01

    nothing developed from them. Empresa Nacional Bazán, which merged with Astilleros Españoles S.A. (AESA) to form Navantia in 2000, reportedly attempted...acquisition and lengthy refurbishing seem to contradict the stated intention of its original buyer, Macao’s Agencia Turisticae Diversoes Chong Lot Limitada

  4. Habitability Improvements for Aircraft Carrier Messdecks

    DTIC Science & Technology

    1979-10-01

    bulkhead and overhead ship items dominate the compartment image or character of the eating areas, giving the diner the effect of eating at his...improvements in response were probably "halo" effect conditions (the men responded more positively to every- thing in general, since their total...Good Good Good Good a. Conveoieoce of locatioo] 1 2 3 4 5 6 7 i.9 b. General mena enviroment 1 2 3 4 5 6 7 3.10 c. Degree of military t.moophero

  5. 14 CFR 294.40 - Aircraft accident liability insurance requirements.

    Code of Federal Regulations, 2011 CFR

    2011-01-01

    ... 14 Aeronautics and Space 4 2011-01-01 2011-01-01 false Aircraft accident liability insurance....40 Aircraft accident liability insurance requirements. No Canadian charter air taxi operator shall engage in charter air service unless such carrier has and maintains in effect aircraft accident...

  6. 14 CFR 294.40 - Aircraft accident liability insurance requirements.

    Code of Federal Regulations, 2013 CFR

    2013-01-01

    ... 14 Aeronautics and Space 4 2013-01-01 2013-01-01 false Aircraft accident liability insurance....40 Aircraft accident liability insurance requirements. No Canadian charter air taxi operator shall engage in charter air service unless such carrier has and maintains in effect aircraft accident...

  7. 14 CFR 294.40 - Aircraft accident liability insurance requirements.

    Code of Federal Regulations, 2014 CFR

    2014-01-01

    ... 14 Aeronautics and Space 4 2014-01-01 2014-01-01 false Aircraft accident liability insurance....40 Aircraft accident liability insurance requirements. No Canadian charter air taxi operator shall engage in charter air service unless such carrier has and maintains in effect aircraft accident...

  8. 14 CFR 294.40 - Aircraft accident liability insurance requirements.

    Code of Federal Regulations, 2010 CFR

    2010-01-01

    ... 14 Aeronautics and Space 4 2010-01-01 2010-01-01 false Aircraft accident liability insurance....40 Aircraft accident liability insurance requirements. No Canadian charter air taxi operator shall engage in charter air service unless such carrier has and maintains in effect aircraft accident...

  9. 49 CFR 1544.225 - Security of aircraft and facilities.

    Code of Federal Regulations, 2010 CFR

    2010-10-01

    ...: AIR CARRIERS AND COMMERCIAL OPERATORS Operations § 1544.225 Security of aircraft and facilities. Each aircraft operator must use the procedures included, and the facilities and equipment described, in its... 49 Transportation 9 2010-10-01 2010-10-01 false Security of aircraft and facilities....

  10. 14 CFR 294.40 - Aircraft accident liability insurance requirements.

    Code of Federal Regulations, 2012 CFR

    2012-01-01

    ... 14 Aeronautics and Space 4 2012-01-01 2012-01-01 false Aircraft accident liability insurance....40 Aircraft accident liability insurance requirements. No Canadian charter air taxi operator shall engage in charter air service unless such carrier has and maintains in effect aircraft accident...

  11. 33. Site Plan: Custer Air Force Station, Battle Creek, Michigan, ...

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

    33. Site Plan: Custer Air Force Station, Battle Creek, Michigan, FD Radar Facilities-FPS-27, Electrical Plot Plan and Duet Details, USACOE, not date. - Fort Custer Military Reservation, P-67 Radar Station, .25 mile north of Dickman Road, east of Clark Road, Battle Creek, Calhoun County, MI

  12. Airland Battle Combat Airdrop Doctrine and Requirement

    DTIC Science & Technology

    1988-04-11

    experier,:_ I ,r. t cal , command and control of the force en route m. - . ,i;iintained, and Joint training is a must. (2:95) 24 Sustainment by ...The cost of using this force is best e-r’lained by tlhe fol lowino quote: "The bill for ge’ tr,_ A:) airborne diisin into battle was hair raising and ...With no other means ot resuppl>y other- than by air, the French had locked themse l ues into a prison. Poor planning and violation of all the

  13. 14 CFR 43.7 - Persons authorized to approve aircraft, airframes, aircraft engines, propellers, appliances, or...

    Code of Federal Regulations, 2010 CFR

    2010-01-01

    ... data approved by the Administrator. (e) The holder of an air carrier operating certificate or an... holder of a repairman certificate (light-sport aircraft) with a maintenance rating may approve an aircraft issued a special airworthiness certificate in light-sport category for return to service,...

  14. Fixed-wing Aircraft Combat Survivability Analysis for Operation Enduring Freedom and Operation Iraqi Freedom

    DTIC Science & Technology

    2011-03-01

    Battle Damage 9 1-6 Risk Assessment Matrix 14 2-1 Aircraft Survivability Balance 16 2-2 One vs. One Kill Chain ...Single Shot) 19 2-3 Hypothetical Kill Chain Illustrating an Insurgent vs. Aircraft 20 2-4 Keys to the AEF Vision 24 2-5...early days of the war, the Italian Army Air Corps conducted a bombing raid on a Turkish camp at Ain Zara , Libya. Figure 1-1 shows a replica of a

  15. A-2000: Close air support aircraft design team

    NASA Technical Reports Server (NTRS)

    Carrannanto, Paul; Lim, Don; Lucas, Evangeline; Risse, Alan; Weaver, Dave; Wikse, Steve

    1991-01-01

    The US Air Force is currently faced with the problem of providing adequate close air support for ground forces. Air response to troops engaged in combat must be rapid and devastating due to the highly fluid battle lines of the future. The A-2000 is the result of a study to design an aircraft to deliver massive fire power accurately. The low cost A-2000 incorporates: large weapons payload; excellent maneuverability; all weather and terrain following capacity; redundant systems; and high survivability.

  16. Aircraft Design

    NASA Technical Reports Server (NTRS)

    Bowers, Albion H. (Inventor); Uden, Edward (Inventor)

    2016-01-01

    The present invention is an aircraft wing design that creates a bell shaped span load, which results in a negative induced drag (induced thrust) on the outer portion of the wing; such a design obviates the need for rudder control of an aircraft.

  17. Comparisons of wartime and peacetime disease and non-battle injury rates aboard ships of the British Royal Navy.

    PubMed

    Blood, C G; Pugh, W M; Gauker, E D; Pearsall, D M

    1992-12-01

    Disease and non-battle injury rates were computed for ships of the British Royal Navy which were deployed during wartime and peacetime operations. The wartime sick list admission rates were lower aboard carriers, battleships, and cruisers when compared with their counterparts deployed in peacetime; rate differences for battleships and cruisers were statistically significant (p < 0.05). Several categories of disease also yielded significant differences in the wartime/peacetime contrasts. Infections and parasitic disorders aboard carriers, skin diseases aboard battleships, and skin diseases, injuries, and generative system disorders occurring on cruisers were all lower during wartime than on peacetime deployments. Illness rates also varied by ship type, with the lowest rates evidenced aboard carriers.

  18. Census U.S. Civil Aircraft Calendar Year 1993

    DTIC Science & Technology

    1993-12-31

    Turbojet 1.020 Helicopter 1,977 Total 10,692 2-3 TABLE 2.2 AIRCRAFT REPORTED IN OPERATION BY AIR CARRIERS, BY MANUFACTURER AND MODEL 1984-1993 Aircraft...2 41 1 0 146 146 A-49 U.S. REGISTERED CIVIL AIRCRAFT BY MANUFACTURER AND MODEL -NUMBER OF SEATS PISTON AS OF DECEMBER 31, 1993...AS OF DECEMBER 31, 1993 Total General TotalEngine Make Engine Model Engine Power Engines Air Carrier Aviation Aircraft ROLL-ROYCE ........... GRIFFON

  19. Battling myths in institutional energy financing

    SciTech Connect

    Hansen, S.J.

    1988-01-01

    The history of our energy situation seems to be well grounded in myths, misinformation and misunderstanding. In 1926, the Fuel Oil Conservation Board announced we had six years of oil left. In 1939, the Department of Interior declared we had thirteen years of oil left. As of August 1, 1975, the Federal Energy Administration said we had sufficient oil resources to last 3,419 days, or slightly more than nine years. Today energy is wrapped in the mantle of skepticism, cynicism or, at best, apathy. Our dependency on foreign oil is greater than in 1973. Energy analysts with considerable caution and careful deliberation are predicting $38 a barrel oil by 1992. Private sector energy financing, also called performance contracting, shared savings, etc., which in itself is a problem does provide a new arsenal to fight the quiet battle for energy efficiency.

  20. The Battle for Leyte Gulf, October 1944. Strategical and Tactical Analysis. Volume I. Preliminary Operations until 0719 October 17th, 1944 Including Battle off Formosa

    DTIC Science & Technology

    1953-01-01

    additional searohes because loss of contact* Discussion 313-31b Orders certain planes of SEVENTH Base Air Force to Ky-juhu 315 "T" Foroe departs...in serious straits. Owing to thje operations (if Allied Bubisarines and of Allied carrier and shore- based aircraft, c~hese sea lanes were becoming loss ...their destruction would not only eliminate the bases and the airormi:, looated there, but with the loss of important repair and assembly faoilities

  1. Marshal Jean Lannes in the Battles of Saalfeld, Pultusk, and Friedland, 1806 to 1807: The Application of Combined Arms in the Opening Battle

    DTIC Science & Technology

    1994-06-03

    AD-A284 591 MARSHAL JEAN LANNES IN THE BATTLES OF SAALFELD, PULTUSK, AND FRIEDLAND, 1806 TO 1807: THE APPLICATION OF COMBINED ARMS IN THE OPENING...3 Jun 94 Marshal Jean Lannes in the Battles of Saalfeld, Pultusk, and Friedland, 1806 to 1807: The Application of Combined Arms in the Opening Battle...UNCLASSIFIED UNCLASSIFIED UNCLASSIFIED * :,j * .38 8; MARSHAL JEAN LANNES IN THE BATTLES OF SAALFELD, PULTUSK, AND FRIEDLAND, 1806 TO 1807: THE APPLICATION OF

  2. Historic interior view of the entrance taken shortly after battle, ...

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

    Historic interior view of the entrance taken shortly after battle, looking toward the southwest showing damage to gorge as well as timber and earth blindage. - Fort Pulaski, Cockspur Island, Savannah, Chatham County, GA

  3. Re-seeding research will help in cheatgrass battle

    USGS Publications Warehouse

    Allen, Craig D.

    2006-01-01

    Funding from the National Interagency Fire Center’s Joint Fire Science Program is helping researchers in northwestern Arizona determine whether several native grasses can be used to battle invasive cheatgrass following fire in ponderosa pine ecosystems.

  4. Senator Arlen Specter: Backing Medical Research and Battling Lymphoma

    MedlinePlus

    ... Cover Story: Leukemia/Lymphoma Senator Arlen Specter: Backing Medical Research and Battling Lymphoma Past Issues / Summer 2008 Table ... been a long-time supporter and proponent of medical research. Recently, he underwent his second round of chemotherapy ...

  5. Aircraft Steels

    DTIC Science & Technology

    2009-02-19

    NAWCADPAX/TR-2009/ 12 AIRCRAFT STEELS by E. U. Lee R. Taylor C. Lei H. C. Sanders 19 February 2009...MARYLAND NAWCADPAX/TR-2009/ 12 19 February 2009 AIRCRAFT STEELS by E. U. Lee R. Taylor C. Lei H. C. Sanders...Prescribed by ANSI Std. Z39-18 NAWCADPAX/TR-2009/ 12 ii SUMMARY Five high strength and four stainless steels have been studied, identifying their

  6. Combat Service Support of AirLand Battle Doctrine,

    DTIC Science & Technology

    1986-05-20

    thereby causing him to lose control of the battle. In the offense, it means setting the tarfa of battle and never allowing the enemy to recover from...disorganizes his forces, causes him to lose control and ultimately brings about his defeat. To achieve these conditions on the battlefield requires a...units with a command and control system that allows the coordination and redirection of combat service support assets when and where required. Implied

  7. Embedded battle command: a vehicle systems integrator's prospective

    NASA Astrophysics Data System (ADS)

    Frey, Terry L.; Wyrembelski, Rick J.

    1999-07-01

    This paper provides an overview of a major weapon system, the Abrams Main Battle Tank, as it relates to the integration of EMbedded Battle Command and Control element is essential to the tanks future role in the Army as they focus more on increased organizational effectiveness and less on individual platforms. The Abrams is poised to field the Abrams System Enhancement Package with its 2nd generation of Command and Control.

  8. A NASA study of the impact of technology on future multimission aircraft

    NASA Technical Reports Server (NTRS)

    Samuels, Jeffrey J.

    1992-01-01

    A conceptual aircraft design study was recently completed which compared three supersonic multimission tactical aircraft. The aircraft were evaluated in two technology timeframes and were sized with consistent methods and technology assumptions so that the aircraft could be compared in operational utility or cost analysis trends. The three aircraft are a carrier-based Fighter/Attack aircraft, a land-based Multirole Fighter, and a Short Takeoff/Vertical Landing (STOVL) aircraft. This paper describes the design study ground rules used and the aircraft designed. The aircraft descriptions include weights, dimensions and layout, design mission and maneuver performance, and fallout mission performance. The effect of changing technology and mission requirements on the STOVL aircraft and the impact of aircraft navalization are discussed. Also discussed are the effects on the STOVL aircraft of both Thrust/Weight required in hover and design mission radius.

  9. Lifecycle Information of Aircraft Engine Components

    DTIC Science & Technology

    2010-04-14

    commercial aircraft, the industry generated a number of potential RFID-based applications for airlines, air- freight carriers, aircraft maintenance and...adoption of RFID technologies to track serially controlled items requires careful planning and design. Data overload and data noise also affect the...performance of RFID systems. Data overload results from continuously scanning the RFID tags within reader range and sending the repeated information

  10. 77 FR 67584 - Air Carrier Contract Maintenance Requirements

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-11-13

    ... Stations, Report No. AV-2003-047 (July 8, 2003). In 2005, the IG issued a second report on air carriers...). \\4\\ Air Carrier's Outsourcing Use of Non-Certificated Repair Facilities, Report No. AV-2006-031 (Dec... Outsourcing of Aircraft Maintenance, Report No. AV-2008-090 (Sept. 30, 2008). \\7\\ The report noted...

  11. 14 CFR 252.3 - Smoking ban: air carriers.

    Code of Federal Regulations, 2010 CFR

    2010-01-01

    ... 14 Aeronautics and Space 4 2010-01-01 2010-01-01 false Smoking ban: air carriers. 252.3 Section 252.3 Aeronautics and Space OFFICE OF THE SECRETARY, DEPARTMENT OF TRANSPORTATION (AVIATION PROCEEDINGS) ECONOMIC REGULATIONS SMOKING ABOARD AIRCRAFT § 252.3 Smoking ban: air carriers. Air...

  12. 14 CFR 252.3 - Smoking ban: air carriers.

    Code of Federal Regulations, 2011 CFR

    2011-01-01

    ... 14 Aeronautics and Space 4 2011-01-01 2011-01-01 false Smoking ban: air carriers. 252.3 Section 252.3 Aeronautics and Space OFFICE OF THE SECRETARY, DEPARTMENT OF TRANSPORTATION (AVIATION PROCEEDINGS) ECONOMIC REGULATIONS SMOKING ABOARD AIRCRAFT § 252.3 Smoking ban: air carriers. Air...

  13. 49 CFR 172.606 - Carrier information contact.

    Code of Federal Regulations, 2011 CFR

    2011-10-01

    ... 49 Transportation 2 2011-10-01 2011-10-01 false Carrier information contact. 172.606 Section 172... REQUIREMENTS, AND SECURITY PLANS Emergency Response Information § 172.606 Carrier information contact. (a) Each... required shall instruct the operator of a motor vehicle, train, aircraft, or vessel to contact the...

  14. 49 CFR 172.606 - Carrier information contact.

    Code of Federal Regulations, 2013 CFR

    2013-10-01

    ... 49 Transportation 2 2013-10-01 2013-10-01 false Carrier information contact. 172.606 Section 172... REQUIREMENTS, AND SECURITY PLANS Emergency Response Information § 172.606 Carrier information contact. (a) Each... required shall instruct the operator of a motor vehicle, train, aircraft, or vessel to contact the...

  15. 49 CFR 172.606 - Carrier information contact.

    Code of Federal Regulations, 2014 CFR

    2014-10-01

    ... 49 Transportation 2 2014-10-01 2014-10-01 false Carrier information contact. 172.606 Section 172... REQUIREMENTS, AND SECURITY PLANS Emergency Response Information § 172.606 Carrier information contact. (a) Each... required shall instruct the operator of a motor vehicle, train, aircraft, or vessel to contact the...

  16. 49 CFR 172.606 - Carrier information contact.

    Code of Federal Regulations, 2012 CFR

    2012-10-01

    ... 49 Transportation 2 2012-10-01 2012-10-01 false Carrier information contact. 172.606 Section 172... REQUIREMENTS, AND SECURITY PLANS Emergency Response Information § 172.606 Carrier information contact. (a) Each... required shall instruct the operator of a motor vehicle, train, aircraft, or vessel to contact the...

  17. 49 CFR 172.606 - Carrier information contact.

    Code of Federal Regulations, 2010 CFR

    2010-10-01

    ... 49 Transportation 2 2010-10-01 2010-10-01 false Carrier information contact. 172.606 Section 172... REQUIREMENTS, AND SECURITY PLANS Emergency Response Information § 172.606 Carrier information contact. (a) Each... required shall instruct the operator of a motor vehicle, train, aircraft, or vessel to contact the...

  18. A Review of Selected Elements of the FY73 Programs on Test and Evaluation of Aircraft Survivability (TEAS). Volume 2. Appendix A: bibliography for Vulnerability and Survivability of Military Aircraft,

    DTIC Science & Technology

    1973-07-31

    17 S 1967 NASC-CREW SYSTEMS ’IV. Battle Damage und Casualty Information for Navy Air Operations In Southeast Aula 386,374L S 196...Fxpirlmental Aircraft Passive Ot f eiise Artnur System 891957L U 1970 AFATI. IK-70-112, BOOK I, II 891958L Bui 11. tic Impact Mechanics

  19. The abortion battle: the Canadian scene.

    PubMed

    Sachdev, P

    1994-01-01

    In January 1988 the Supreme Court of Canada struck down the country's archaic abortion law on the ground that it imposed arbitrary delays and unfair disparities in access to abortion across the country. Since then, the conservative government of Canada has made a few attempts to introduce a new abortion policy, but it did not get passed in the parliament because the revised bills failed to protect women's right to 'life, liberty, and security of the person' within the meaning of the Canadian Charter. Canada has been without an abortion law for over four years and there has been a wide range of provincial policies and confusion in the country. Despite the legal vacuum, Canadian women are not frenziedly having abortions. However, the militancy of the anti-abortion groups has steadily intensified with continued assault on a woman's right to make reproductive choices. Since no law, short of banning abortions altogether, is going to satisfy abortion opponents, the abortion battle will rage on in Canada.

  20. Credibility battles in the autism litigation.

    PubMed

    Kirkland, Anna

    2012-04-01

    That vaccines do not cause autism is now a widely accepted proposition, though a few dissenters remain. An 8-year court process in the US federal vaccine injury compensation court ended in 2010 with rulings that autism was not an adverse reaction to vaccination. There were two sets of trials: one against the measles-mumps-rubella (MMR) vaccine and one against the mercury-based preservative thimerosal. The MMR story is more widely known because of publicity surrounding the main proponent of an MMR-autism link, British doctor Andrew Wakefield, but the story of thimerosal in court is largely untold. This study examines the credibility battles and boundary work in the two cases, illuminating the sustaining world of alternative science that supported the parents, lawyers, researchers, and expert witnesses against vaccines. After the loss in court, the families and their advocates transformed their scientific arguments into an indictment of procedural injustice in the vaccine court. I argue that the very efforts designed to produce legitimacy in this type of lopsided dispute will be counter-mobilized as evidence of injustice, helping us understand why settling a scientific controversy in court does not necessarily mean changing anyone's mind.

  1. Hydrogen carriers

    NASA Astrophysics Data System (ADS)

    He, Teng; Pachfule, Pradip; Wu, Hui; Xu, Qiang; Chen, Ping

    2016-12-01

    Hydrogen has the potential to be a major energy vector in a renewable and sustainable future energy mix. The efficient production, storage and delivery of hydrogen are key technical issues that require improvement before its potential can be realized. In this Review, we focus on recent advances in materials development for on-board hydrogen storage. We highlight the strategic design and optimization of hydrides of light-weight elements (for example, boron, nitrogen and carbon) and physisorbents (for example, metal-organic and covalent organic frameworks). Furthermore, hydrogen carriers (for example, NH3, CH3OH-H2O and cycloalkanes) for large-scale distribution and for on-site hydrogen generation are discussed with an emphasis on dehydrogenation catalysts.

  2. Civil Applications For New V/STOL and STOL Aircraft

    NASA Technical Reports Server (NTRS)

    Albers, James A.; Zuk, John

    1990-01-01

    New designs offer benefits in congested urban areas and remote regions. Report explores potential uses in civil aviation of advanced rotorcraft, vertical/short-takeoff-and-landing (V/STOL) aircraft, and short-takeoff-and-landing (STOL) aircraft. Future opportunities overcome formidable geographic barriers and lack of major airport facilities, bringing fast, flexible transportation to remote areas. Aircraft relieves congestion at airports in densely populated areas by utilizing pads and short runways without interfering with large-air-carrier traffic.

  3. Aircraft cybernetics

    NASA Technical Reports Server (NTRS)

    1977-01-01

    The use of computers for aircraft control, flight simulation, and inertial navigation is explored. The man-machine relation problem in aviation is addressed. Simple and self-adapting autopilots are described and the assets and liabilities of digital navigation techniques are assessed.

  4. Results of a carrier aircraft (model AX13191-4) verification test in the Boeing transonic wind tunnel using a 0.03-scale 747 CAM/orbiter model 45-0 (CA6), volume 1

    NASA Technical Reports Server (NTRS)

    1976-01-01

    Force and moment data were obtained on each vehicle both mated and separated. The investigation included the effects of orbiter incidence, orbiter tail cone, orbiter strut fairings, elevon, and body flap settings. Analysis of the data indicated the 747 is suitable as a carrier of the orbiter in both the ALT launch and ferry mode. The effect of configuration changes on drag and stability was determined.

  5. Development of Longitudinal Equivalent System Models for Selected U.S. Navy Tactical Aircraft

    DTIC Science & Technology

    1981-08-01

    revaraa side II nacaaaary and Identlly by block number) Aircraft Longitudinal Flying Qualities Equivalent Systems Frequency Response Matching...is a twin turbofan powered, land and carrier based, subsonic, anti- submarine warfare aircraft . Longitudinal control is accomplished via a...based, supersonic fighter aircraft . Longitudinal control is accomplished via an irreversible mechanical flight control system which transmits

  6. 40 CFR 141.804 - Aircraft water system operations and maintenance plan.

    Code of Federal Regulations, 2011 CFR

    2011-07-01

    ...) WATER PROGRAMS (CONTINUED) NATIONAL PRIMARY DRINKING WATER REGULATIONS Aircraft Drinking Water Rule § 141.804 Aircraft water system operations and maintenance plan. (a) Each air carrier must develop and... 40 Protection of Environment 23 2011-07-01 2011-07-01 false Aircraft water system operations...

  7. 40 CFR 141.804 - Aircraft water system operations and maintenance plan.

    Code of Federal Regulations, 2014 CFR

    2014-07-01

    ...) WATER PROGRAMS (CONTINUED) NATIONAL PRIMARY DRINKING WATER REGULATIONS Aircraft Drinking Water Rule § 141.804 Aircraft water system operations and maintenance plan. (a) Each air carrier must develop and... 40 Protection of Environment 23 2014-07-01 2014-07-01 false Aircraft water system operations...

  8. 40 CFR 141.804 - Aircraft water system operations and maintenance plan.

    Code of Federal Regulations, 2013 CFR

    2013-07-01

    ...) WATER PROGRAMS (CONTINUED) NATIONAL PRIMARY DRINKING WATER REGULATIONS Aircraft Drinking Water Rule § 141.804 Aircraft water system operations and maintenance plan. (a) Each air carrier must develop and... 40 Protection of Environment 24 2013-07-01 2013-07-01 false Aircraft water system operations...

  9. 40 CFR 141.804 - Aircraft water system operations and maintenance plan.

    Code of Federal Regulations, 2012 CFR

    2012-07-01

    ...) WATER PROGRAMS (CONTINUED) NATIONAL PRIMARY DRINKING WATER REGULATIONS Aircraft Drinking Water Rule § 141.804 Aircraft water system operations and maintenance plan. (a) Each air carrier must develop and... 40 Protection of Environment 24 2012-07-01 2012-07-01 false Aircraft water system operations...

  10. 40 CFR 141.804 - Aircraft water system operations and maintenance plan.

    Code of Federal Regulations, 2010 CFR

    2010-07-01

    ...) WATER PROGRAMS (CONTINUED) NATIONAL PRIMARY DRINKING WATER REGULATIONS Aircraft Drinking Water Rule § 141.804 Aircraft water system operations and maintenance plan. (a) Each air carrier must develop and... 40 Protection of Environment 22 2010-07-01 2010-07-01 false Aircraft water system operations...

  11. 14 CFR 218.3 - Prohibition against unauthorized operations employing aircraft leased with crew.

    Code of Federal Regulations, 2010 CFR

    2010-01-01

    ... employing aircraft leased with crew. 218.3 Section 218.3 Aeronautics and Space OFFICE OF THE SECRETARY... OTHER FOREIGN PERSON OF AIRCRAFT WITH CREW § 218.3 Prohibition against unauthorized operations employing aircraft leased with crew. (a) No foreign air carrier, or other person not a citizen of the United...

  12. 78 FR 41335 - Proposed Establishment of Class E Airspace; Battle Mountain, NV

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-07-10

    ... Federal Aviation Administration 14 CFR Part 71 Proposed Establishment of Class E Airspace; Battle Mountain...). SUMMARY: This action proposes to establish Class E airspace at the Battle Mountain VHF Omni-Directional Radio Range Tactical Air Navigational Aid (VORTAC) navigation aid, Battle Mountain, NV, to...

  13. 78 FR 58159 - Establishment of Class E Airspace; Battle Mountain, NV

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-09-23

    ... Federal Aviation Administration 14 CFR Part 71 Establishment of Class E Airspace; Battle Mountain, NV... Class E airspace at the Battle Mountain VHF Omni-Directional Radio Range Tactical Air Navigational Aid (VORTAC) navigation aid, Battle Mountain, NV, to facilitate vectoring of Instrument Flight Rules...

  14. The Battle of Stones River: The Soldiers' Story. Teaching with Historic Places.

    ERIC Educational Resources Information Center

    Weller, Tammy Calvin; Harris, Michael

    Today, as people gaze across the narrow waters of Stones River (near Murfreesboro, Tennessee), it is difficult to imagine the carnage of a U.S. Civil War battle. The battle at Stones River claimed 23,000 casualties. It was the second bloodiest battle fought west of the Appalachian Mountains during the Civil War. This lesson plan is based on the…

  15. 61. Credit PG&E. South elevation from across South Battle Creek. ...

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

    61. Credit PG&E. South elevation from across South Battle Creek. Note two exciter water discharge pipes and also the transformer cooling water discharge pipes (6). Photo taken 10 November 1927. - Battle Creek Hydroelectric System, Battle Creek & Tributaries, Red Bluff, Tehama County, CA

  16. Feasibility Study for Battle Mountain Renewable Energy Park

    SciTech Connect

    Hill, Donna

    2014-09-30

    The Feasibility Study for the Battle Mountain Renewable Energy Park project (“Feasibility Study”) will assess the feasibility, benefits and impacts of a 5 Mega Watt (MW) solar photovoltaic (PV) generating system (the “Solar Project” or “Energy Park”) on the Te-Moak Tribe of Western Shoshone Indians of Nevada Battle Mountain Colony in Battle Mountain, Nevada (NV). The Energy Park will provide power for export to utility off-takers and job training and employment for Tribal members and revenue for the Tribe. This Feasibility Study will be a collaborative effort between the Tribal government, consultants, Tribal members and stakeholders and will allow the Tribe to make informed decisions regarding the Solar Project.

  17. Modelling Combat as a Series of Mini-Battles

    DTIC Science & Technology

    1988-11-30

    I iLt1 ai AD MODELLING COMBAT AS A SERIES OF MINI-BATTLLES by MICHAEL R BATHE J GRAHAM MANWELL KENNETH R MCNAUGHT NOVEMBER 1988 United States Army...Modelling Combat as o Series of Mini-Battles 12. PERSONAL AUTHOR(S) Michael R. Bathe, J. Graham Manwell , Kenneth R. McNaught 13a. TYPE OF REPORT 13b...MODELLING COMBAT AS A SERIES OF MINT-BATTLES by MICHAEL R BATHE J GRAHAM MANWELL KENNETH R MCNAUGHT NOVEMBER 1988 United States Army EUROPEAN RESEARCH

  18. Aircraft Corrosion

    DTIC Science & Technology

    1981-08-01

    chlore mais dans une proportion semblable b cells d’une eau de vil)e ; - lea solides, d’aprbs lea analyses chimique et criatallographique, paraissaiont...IATA member airlines at $100 million based on 1976 operations. Thus the numbers are large, but detailed analyses on specific aircraft types, in known...demonstrate this in any quantitative way with accurate figures. Better information is required on the cost of corrosion, together with analyses of the

  19. Aircraft Ducting

    NASA Technical Reports Server (NTRS)

    1996-01-01

    Templeman Industries developed the Ultra-Seal Ducting System, an environmental composite air duct with a 50 percent weight savings over current metallic ducting, but could not find a commercial facility with the ability to test it. Marshall Space Flight Center conducted a structural evaluation of the duct, equivalent to 86 years of take-offs and landings in an aircraft. Boeing Commercial Airplane Group and McDonnell Douglas Corporation are currently using the ducts.

  20. Robotics and Automation for Flight Deck Aircraft Servicing

    SciTech Connect

    Chesser, J.B.; Draper, J.V.; Pin, F.G.

    1999-03-01

    One of the missions of the Future Aircraft Carriers Program is to investigate methods that would improve aircraft turnaround servicing activities on carrier decks. The major objectives and criteria for evaluating alternative aircraft servicing methods are to reduce workload requirements, turnaround times (TAT), and life-cycle costs (LCC). Technologies in the field of Robotics and Automation (R and A) have the potential to significantly contribute to these objectives. The objective of this study was to investigate aircraft servicing functions on carrier decks which would offer the potentially most significant payoff if improved by various R and A technologies. Improvement in this case means reducing workload, time and LCC. This objective was accomplished using a ''bottom-up'' formalized approach as described in the following.

  1. Seuss's Butter Battle Book: Is There Hidden Harm?

    ERIC Educational Resources Information Center

    Van Cleaf, David W.; Martin, Rita J.

    1986-01-01

    Examines whether elementary school children relate to the "harmful hidden message" about nuclear war in Dr. Seuss's THE BUTTER BATTLE BOOK. After ascertaining the children's cognitive level, they participated in activities to find hidden meanings in stories, including Seuss's book. Students failed to identify the nuclear war message in…

  2. "The Butter Battle Book": Engaging Children's Thoughts of War.

    ERIC Educational Resources Information Center

    Barone, Diane

    1993-01-01

    Discusses how "The Butter Battle Book" by Dr. Seuss can be used to introduce the moral issue of war to young children. Studies the written responses of 1,187 children in grades kindergarten to 6 to the story. Notes that only the fourth- through sixth-grade students (who felt themselves beyond Dr. Seuss) understood the allegorical nature…

  3. Enacting Informal Science Learning: Exploring the Battle for Informal Learning

    ERIC Educational Resources Information Center

    Clapham, Andrew

    2016-01-01

    Informal Science Learning (ISL) is a policy narrative of interest in the United Kingdom and abroad. This paper explores how a group of English secondary school science teachers, enacted ISL science clubs through employing the Periodic Table of Videos. It examines how these teachers "battled" to enact ISL policy in performative conditions…

  4. The Milwaukee Platoon School Battle: Lessons for Activist Teachers.

    ERIC Educational Resources Information Center

    Levine, David

    2002-01-01

    Chronicles an education reform battle of the 1920s in which teacher activists within the Milwaukee Teachers' Association emerged as champions for their students. They challenged a proposal that the school system experiment with platoon schools, which applied the efficiency of the business world to education. Their challenge offers insight into…

  5. Historic interior view of gorge wall, taken shortly after battle, ...

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

    Historic interior view of gorge wall, taken shortly after battle, looking northwest at the entrance and northwest shoeing damage to gorge wall as well as timber and earth blindage (see also HABS No. GA-2158-39). - Fort Pulaski, Cockspur Island, Savannah, Chatham County, GA

  6. Deficiencies in Current and Emerging Rear Battle Doctrine.

    DTIC Science & Technology

    2014-09-26

    CLASS. (of duoe repo"t) *Unclassified SCM EDL 1S. DISTRIBUTION STATEMENT (of this Report) Approved for public release; distribution is unlimited. 17...resouring a third command post from active components . The VII US Corps has conducted the airland battle using a three command post concept (TAC, MAIN

  7. Operationalizing Air-Sea Battle in the Pacific

    DTIC Science & Technology

    2015-02-01

    systems. 35. Chris Anderson, " Agricultural Drones ,• MIT ’Technology Review 117, no. 3 (May/June 2014): 58. 36. Van Thl et al., AirSea Battle: A Point...communications are re- established. These systems are vulnerable to antiair weapons; how- ever, 11relatively cheap drones with advanced sensors and

  8. True Stories of Censorship Battles in America's Libraries

    ERIC Educational Resources Information Center

    Nye, Valerie, Ed.; Barco, Kathy, Ed.

    2012-01-01

    Intellectual freedom is a core value of librarianship, but fighting to keep controversial materials on the shelves can sometimes feel like a lonely battle. And not all censorship controversies involve the public objecting to a book in the collection--libraries are venues for displays and meetings, and sometimes library staff themselves are tempted…

  9. School Finance 2005?06. Budget Sets Off Public Battle

    ERIC Educational Resources Information Center

    Perry, Mary

    2005-01-01

    For the past year, the issue of public education funding has been particularly contentious in California. A pitched political battle between education advocates and the administration of Gov. Arnold Schwarzenegger began with a December 2004 preview of the governor's budget proposal for 2005?06. The fight continued through a spring filled with…

  10. Dictatorship of Virtue: Multiculturalism and the Battle for America's Future.

    ERIC Educational Resources Information Center

    Bernstein, Richard

    This book addresses the issue of multicultural education and the political battles waged over it in U.S. schools. The volume examines the perspectives of both advocates and critics and applauds the true meaning of multiculturalism equality of opportunity and social justice. The fear is there is pulling away from certain cultural norms…

  11. Year 10 English: Australian Texts and the Battle for Survival

    ERIC Educational Resources Information Center

    Robertson,, Alison

    2012-01-01

    The texts and classroom activities in this paper are a sample of those used within a unit on "The Battle for Survival". The unit brings classic Australian literary texts together with reportage on contemporary news events, and demonstrates an integrated approaches to the Literacy, Language and Literature strands of the AC:E. The unit…

  12. Collaborative Awareness: Experiments with Tools for Battle Command

    DTIC Science & Technology

    2006-06-01

    differences in SAt levels predict battle outcome is quite remarkable. A lighter and more agile blue force wins to a large extent via its information...with a significant degree of accuracy, the plan that the red force is implementing. At H+38, Cheetah 6, the CAU 2 commander, states that the enemy

  13. 75 FR 15765 - Request for Comments on Carriers' Temporary Exemption Requests From DOT's Tarmac Delay Rules for...

    Federal Register 2010, 2011, 2012, 2013, 2014

    2010-03-30

    ... multiple flights because the interconnecting resources required for each flight--aircraft, flight deck crew... subsequent ripple effect on the following flights that require use of the same aircraft, cockpit crew or... plans for lengthy tarmac delays that include an assurance that a carrier will not permit an aircraft...

  14. Carrier Battle Group (CVBG) Homeporting in the Puget Sound Area, Washington State. Technical Appendices.

    DTIC Science & Technology

    1986-11-01

    Mall 603 36 1049 945 1479 6. Edmonds, Lynnwood, Mountlake Terrace 419 14 740 607 1027 7. North Creek, Maltby, 1 Cathcart , Mill Valley 365 20 637 554 923...45 -- 81 66 40 402 259 80 4 140 115 377 TOTAL 419 14 740 607 1027 North Creek, Maltby, Cathcart 389 390 251 40 10 62 54 40 391 252 50 -- 90 78 60 392...filtered (0.45 um pore size membrane filter), digested using procedures developed by Chain and DeWalle (1975) for chlorides in sanitary landfill leachate

  15. Educating with Aircraft Models

    ERIC Educational Resources Information Center

    Steele, Hobie

    1976-01-01

    Described is utilization of aircraft models, model aircraft clubs, and model aircraft magazines to promote student interest in aerospace education. The addresses for clubs and magazines are included. (SL)

  16. Aerodynamic design trends for commercial aircraft

    NASA Technical Reports Server (NTRS)

    Hilbig, R.; Koerner, H.

    1986-01-01

    Recent research on advanced-configuration commercial aircraft at DFVLR is surveyed, with a focus on aerodynamic approaches to improved performance. Topics examined include transonic wings with variable camber or shock/boundary-layer control, wings with reduced friction drag or laminarized flow, prop-fan propulsion, and unusual configurations or wing profiles. Drawings, diagrams, and graphs of predicted performance are provided, and the need for extensive development efforts using powerful computer facilities, high-speed and low-speed wind tunnels, and flight tests of models (mounted on specially designed carrier aircraft) is indicated.

  17. Aircraft Electric Secondary Power

    NASA Technical Reports Server (NTRS)

    1983-01-01

    Technologies resulted to aircraft power systems and aircraft in which all secondary power is supplied electrically are discussed. A high-voltage dc power generating system for fighter aircraft, permanent magnet motors and generators for aircraft, lightweight transformers, and the installation of electric generators on turbine engines are among the topics discussed.

  18. Design definition study of NASA/Navy lift/cruise fan V/STOL aircraft. Volume 1: Summary report of Navy multimission aircraft

    NASA Technical Reports Server (NTRS)

    Cavage, R. L.

    1975-01-01

    Results are presented of a study of lift-cruise fan V/STOL aircraft for the 1980-1985 time period. Technical and operating characteristics and technology requirements for the ultimate development of this type aircraft are identified. Aircraft individually optimized to perform the antisubmarine warfare, carrier onboard delivery, combat search and rescue, and surveillance and surface attack missions are considered along with a multi-purpose aircraft concept capable of performing all five missions at minimum total program cost. It is shown that lighter and smaller aircraft could be obtained by optimizing the design and fan selection for specific missions.

  19. Nanocontamination of the Soldiers in a Battle Space

    NASA Astrophysics Data System (ADS)

    Gatti, A. M.; Montanari, S.

    The paper deals with the unusual pathologies some soldiers contracted after exposure in battle theatres in Iraq and in the Balkans, and considers the hypotheses the Authors developed to explain the origin of those diseases, that proved to be lethal in a few cases. The scenario of particulate nanopollution generated by high-temperature combustions characteristic of some weapons is described. The electron-microscopy observations carried out in 37 soldiers' pathological tissues verified the internal dissemination of toxic metallic micro and nano-particles. The article considers the way of entrance of those nanopollutants: the lung for inhalation and the digestive system for the ingestion of polluted food. Battle theatre pollution is also discussed.

  20. Battles between an insurgent army and an advanced army - focus on strategy

    NASA Astrophysics Data System (ADS)

    Sen, Surajit; Shanahan, Linda

    2008-03-01

    Detailed and aggregate analyses of the outcome of past battles focusing on rates of troop losses or on the ratios of forces on each side is at the heart of present knowledge about battles. Here we present non-equilibrium statistical mechanics based studies of possible outcomes of well matched strategic battles by a ``blue'' army against insurgency based attacks by well matched opponents in a ``red'' army in red territory. We assume that the red army attacks with randomly varying force levels to potentially confuse and drive the blue's strategies. The temporal evolution of the model battles incorporate randomness in the deployment of the reds and hence possess attendant history dependence. Our results reveal that while unpredictable events play a major role in battles, a balance between risk of exposure in a battlefield and the use of short range intelligence is needed in determining whether one side can decimate the other, and hence force a battle to end.

  1. Economic Analysis for an F-22 Organic vs. Contractor Aircraft Battle Damage Repair Ownership Decision

    DTIC Science & Technology

    1997-09-01

    USAF Weighted Inflation Indices page instructs users to use raw indices for Pay and POL [petroleum, oils, and lubricants] inflation (’USAF Raw", 1997... author and do not reflect the official policy or position of the Department of Defense or the U.S. Government. AFIT/GLM/LAL/97S-5 ECONOMIC ANALYSIS FOR...finally, I would like to especially thank my wife for being self-confident enough to know that I really do care for her more than my research. Her

  2. Maneuver the Net: Lines of Information and Battle Command

    DTIC Science & Technology

    2007-11-02

    permeates the literature on future war and thus influences the development of future concepts. For example, the concept of Network-Centric Warfare (NCW...dimension supports the other in the friendly force component of information management and protection . Information and knowledge were examined in...relation to the concept of Network- Centric Warfare . Analysis examined whether transformation force leadership (battle command) could be expected to

  3. Design of Battle Simulations for Command and Staff Training

    DTIC Science & Technology

    1988-04-01

    COMMAND AND STAFF TRAINING SECTION 1. INTRODUCTION Simulations designed to train Army commanders and staffs in planning and conducting milit-iry... plan to automate staff training at high echelons. The Army Research Institute (ARI) Field Unit at Fort Leavenworth has been participating in battle...TRAINING~ SCNA OBJECTIVE CONTRL COMANDE PERSONEL & STAFF AI SIMUATIO TACICA MODEL DAT SYSTEM MEASUEMEN & FEDBAC Figue 1.A tpica co ma.’d saff raiing

  4. Assessing Maritime Aspects of the AirSea Battle Concept

    DTIC Science & Technology

    2012-03-23

    a protracted campaign, ramping up industrial production, conducting “distant blockade” operations, and sustaining operational logistics.31 At this...defensive munitions. They indicate that the “US defense industrial base would undertake surge operations to replace expended 10 28 Center for...Battle, 53. ordnance.”32 A prolonged campaign with an emphasis on industrial production of war materials puts the U.S. industrial base in direct

  5. An n-person battle of sexes game

    NASA Astrophysics Data System (ADS)

    Zhao, Jijun; Szilagyi, Miklos N.; Szidarovszky, Ferenc

    2008-06-01

    The n-person Battle of Sexes game is first introduced. The game’s properties are discussed and payoff functions are modeled under the main assumption that players’ payoffs are based on whether they like their choices or not and also on how many other players have the same choices. Linear payoff functions are assumed and the existence of the Nash equilibrium is examined. The dependence of the equilibrium on model parameters is also analyzed.

  6. Self-Organization in the Battle of the Sexes

    NASA Astrophysics Data System (ADS)

    Alonso-Sanz, Ramón

    This paper presents a spatial version of the iterated battle of the sexes game in which every one individual plays with his nearest partners and imitates the optimal strategy of his nearest mate neighbors. It is concluded that the spatial structure enables the emergence of clusters of coincident choices, leading to the mean payoff per encounter to values that are accessible only in the cooperative two-person game scenario, which constitutes a notable case of self-organization.

  7. Interpreting Airpower: American Observation of the Battle of Britain

    DTIC Science & Technology

    2010-06-01

    certify that this thesis meets master‟s-level standards of research, argumentation, and expression. DR. THOMAS A . HUGHES (Date) DR. RICHARD R... Richards , Battle of Britain, 46-47, 136. 18 Bungay, Most Dangerous Enemy, 147. 9 the bulk of RAF fighters were Hurricanes. Although the Spitfire was a ...leaders. 9 Thus, Gardner 5 Richard G. Davis, Carl A . Spaatz and the Air War in Europe, (Washington

  8. A quantum relativistic battle of the sexes cellular automaton

    NASA Astrophysics Data System (ADS)

    Alonso-Sanz, Ramón; Situ, Haozhen

    2017-02-01

    The effect of variable entangling on the dynamics of a spatial quantum relativistic formulation of the iterated battle of the sexes game is studied in this work. The game is played in the cellular automata manner, i.e., with local and synchronous interaction. The game is assessed in fair and unfair contests. Despite the full range of quantum parameters initially accessible, they promptly converge into fairly stable configurations, that often show rich spatial structures in simulations with no negligible entanglement.

  9. The Battle of Khafji: An Assessment of Airpower

    DTIC Science & Technology

    2007-11-02

    Battle of Khafji,” p. 15. 30 Notes 9 “ EPW interviews” AWC Khafji Study (Maxwell, AFB: Air Force Historical Research Agency) Computer File Name War_reps...contradict a large-scale offensive. Instead, it appears that the attacks were limited in scope for the purpose of capturing EPWs and gaining tactical...evidence supporting a limited attack scenario were the numerous EPW reports that stated: “The sole purpose of the raid on Al-Khafji was to capture

  10. The Italian Submarine Force in the Battle of the Atlantic: Left in the Dark

    DTIC Science & Technology

    2014-12-12

    THE ITALIAN SUBMARINE FORCE IN THE BATTLE OF THE ATLANTIC: LEFT IN THE DARK A thesis presented to the Faculty of the U.S...TITLE AND SUBTITLE The Italian Submarine Force in the Battle of the Atlantic: Left in the Dark 5a. CONTRACT NUMBER 5b. GRANT NUMBER 5c...APPROVAL PAGE Name of Candidate: LCDR Kevin M. Moeller Thesis Title: The Italian Submarine Force in the Battle of the Atlantic: Left in the Dark

  11. The Battle of Prairie Grove: Civilian Recollections of the Civil War. Teaching with Historic Places.

    ERIC Educational Resources Information Center

    Montgomery, Don; Baker, Lea Flowers

    Julia West was 14 years old when she viewed the carnage and destruction of the battle field at Prairie Grove, Arkansas. She was not the only young spectator at the battle, but she had one of the best views of the conflict. From her home on West Hill (AK), Julia beheld the horror and splendor of battle when the men of the Union Army of the Frontier…

  12. 75 FR 61485 - Regulatory Training Session With Air Carriers, EPA Regional Partners and Other Interested Parties...

    Federal Register 2010, 2011, 2012, 2013, 2014

    2010-10-05

    ... for Implementation of the Aircraft Drinking Water Rule AGENCY: Environmental Protection Agency (EPA... on the regulatory requirements of the Aircraft Drinking Water Rule (ADWR). Under the ADWR, by April 19, 2011, air carriers who meet the definition of ``public water systems'' under the Safe...

  13. 14 CFR 204.3 - Applicants for new certificate or commuter air carrier authority.

    Code of Federal Regulations, 2011 CFR

    2011-01-01

    ... applicant for a type of certificate authority it does not currently hold or for commuter air carrier... interest in the applicant are related by blood or marriage, such relationship(s) shall be included in the... description of the applicant's fleet of aircraft, including: (1) The number of each type of aircraft...

  14. 14 CFR 204.3 - Applicants for new certificate or commuter air carrier authority.

    Code of Federal Regulations, 2014 CFR

    2014-01-01

    ... applicant for a type of certificate authority it does not currently hold or for commuter air carrier... interest in the applicant are related by blood or marriage, such relationship(s) shall be included in the... description of the applicant's fleet of aircraft, including: (1) The number of each type of aircraft...

  15. 14 CFR 204.3 - Applicants for new certificate or commuter air carrier authority.

    Code of Federal Regulations, 2013 CFR

    2013-01-01

    ... applicant for a type of certificate authority it does not currently hold or for commuter air carrier... interest in the applicant are related by blood or marriage, such relationship(s) shall be included in the... description of the applicant's fleet of aircraft, including: (1) The number of each type of aircraft...

  16. 14 CFR 204.3 - Applicants for new certificate or commuter air carrier authority.

    Code of Federal Regulations, 2012 CFR

    2012-01-01

    ... applicant for a type of certificate authority it does not currently hold or for commuter air carrier... interest in the applicant are related by blood or marriage, such relationship(s) shall be included in the... description of the applicant's fleet of aircraft, including: (1) The number of each type of aircraft...

  17. Portable catapult launcher for small aircraft

    NASA Technical Reports Server (NTRS)

    Rosenbaum, Bernard J. (Inventor); Petter, George E. (Inventor); Gessler, Joseph A. (Inventor); Hughes, Michael G. (Inventor)

    2005-01-01

    An apparatus for launching an aircraft having a multiplicity of interconnected elongated tracks of rigid material forming a track system and wherein each elongated track has a predetermined elongated track cross-sectional design, a winch system connected to the track system wherein the winch system has a variable mechanical advantage, one or more elongated elastic members wherein one end of each of the one or more elongated elastic members is adjustably connected to the track system, and a carrier slidably mounted to the track system wherein the carrier is connected to the winch system and to the other end of each of the one or more elongated elastic members.

  18. 19 CFR 192.4 - Liability of carriers.

    Code of Federal Regulations, 2011 CFR

    2011-04-01

    ... 19 Customs Duties 2 2011-04-01 2011-04-01 false Liability of carriers. 192.4 Section 192.4 Customs Duties U.S. CUSTOMS AND BORDER PROTECTION, DEPARTMENT OF HOMELAND SECURITY; DEPARTMENT OF THE TREASURY (CONTINUED) EXPORT CONTROL Exportation of Used Self-Propelled Vehicles, Vessels, and Aircraft §...

  19. 19 CFR 192.4 - Liability of carriers.

    Code of Federal Regulations, 2010 CFR

    2010-04-01

    ... 19 Customs Duties 2 2010-04-01 2010-04-01 false Liability of carriers. 192.4 Section 192.4 Customs Duties U.S. CUSTOMS AND BORDER PROTECTION, DEPARTMENT OF HOMELAND SECURITY; DEPARTMENT OF THE TREASURY (CONTINUED) EXPORT CONTROL Exportation of Used Self-Propelled Vehicles, Vessels, and Aircraft §...

  20. Shipboard trials of the Quiet Short-Haul Research Aircraft /QSRA/

    NASA Technical Reports Server (NTRS)

    Martin, J. L.; Strickland, P. B.

    1980-01-01

    The feasibility of the application of advanced state-of-the-art high lift STOL aircraft in the aircraft carrier environment was evaluated using the NASA Quiet Short-Haul Research Aircraft (QSRA). The QSRA made repeated unarrested landings and free deck takeoffs from the USS Kitty Hawk while being flown by three pilots of significant different backgrounds. The exercise demonstrated that the USB propulsive lift technology presents no unusual problems in the aircraft carrier environment. Optimum parameters for landing the QSRA were determined from the shore-based program; these proved satisfactory during operations aboard ship. Correlation of shipboard experience with shore-based data indicates that both free deck takeoffs and unarrested landings could be conducted with zero to 35 knots of wind across the deck of an aircraft carrier the size of the USS Kitty Hawk.

  1. Propulsion controlled aircraft computer

    NASA Technical Reports Server (NTRS)

    Cogan, Bruce R. (Inventor)

    2010-01-01

    A low-cost, easily retrofit Propulsion Controlled Aircraft (PCA) system for use on a wide range of commercial and military aircraft consists of an propulsion controlled aircraft computer that reads in aircraft data including aircraft state, pilot commands and other related data, calculates aircraft throttle position for a given maneuver commanded by the pilot, and then displays both current and calculated throttle position on a cockpit display to show the pilot where to move throttles to achieve the commanded maneuver, or is automatically sent digitally to command the engines directly.

  2. Repair and maintenance of fiber optic data links on Navy aircraft

    NASA Astrophysics Data System (ADS)

    Fryland, Eric

    1992-02-01

    This paper will examine the problems and concerns of repairing fiber optic data links on carrier based Navy aircraft and will present the results of fiber optic splice testing that was performed aboard the USS Abraham Lincoln (CVN-72) in January 1991. Mechanical splicing of 50/125 micrometer fiber was performed at the various Navy maintenance levels in order to quantify the effects of the aircraft carrier environment on fiber optic splicing. Results, conclusions and recommendations will be given.

  3. The Battle of Honey Springs: The Civil War Comes to Indian Territory. Teaching with Historic Places.

    ERIC Educational Resources Information Center

    Adkins, Mike; Jones, Ralph

    Union Army troops marched south through Indian territory on July 17, 1863, to face the Confederate Army forces in a battle that would help determine whether the Union or the Confederacy would control the West beyond the Mississippi River. The Confederate troops that these soldiers faced in the Battle of Honey Springs concealed themselves among the…

  4. Defying the Iron Duke: Assessing the Battle of Waterloo in the Classroom

    ERIC Educational Resources Information Center

    Crumplin, Michael; Divall, Carol; Wheeley, Tom

    2014-01-01

    The approaching bicentenary of the Battle of Waterloo has stimulated debate about how it should be commemorated. This article reports a collaboration between the Waterloo200 Committee and Tom Wheeley, history teacher, to create a lesson sequence analysing the causes, consequences and significance of the battle. The article adds to a long-standing…

  5. 78 FR 68699 - Establishment of Class E Airspace; Battle Mountain, NV

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-11-15

    ... Federal Aviation Administration 14 CFR Part 71 Establishment of Class E Airspace; Battle Mountain, NV... corrects a final rule published in the Federal Register of September 23, 2013, that establishes Class E...) navigation aid, Battle Mountain, NV. A favorable comment from the National Business Aviation...

  6. "This Must Have Been a Grand Sight": George Bent and the Battle of Platte Bridge

    ERIC Educational Resources Information Center

    Haack, Steven C.

    2010-01-01

    The Battle of Platte Bridge, July 26, 1865, is a noteworthy event in the annals of the American Indian Wars. An alliance of Cheyenne, Sioux, and Arapahoe, numbering in excess of 2,000 warriors, traveled three days to a specific military objective, an undertaking unusual both in terms of its magnitude and its level of organization. The battle,…

  7. The Battle of Okinawa, 1945: Final Turning Point in the Pacific.

    ERIC Educational Resources Information Center

    Tzeng, Megan

    2000-01-01

    Reviews the last major battle of World War II that occurred at Okinawa (Japan) in 1945. Explains why the Battle of Okinawa was the turning point in World War II. Includes two maps in the appendix and an annotated bibliography. (CMK)

  8. Battling Obesity in K-12 Learners from an Exercise Physiology Perspective

    ERIC Educational Resources Information Center

    Rattigan, Peter; Biren, Greg

    2007-01-01

    Physical education practitioners and programs have the opportunity and obligation to help children become physically educated, healthy, and active adults. This article discusses the battle against obesity in K-12 learners from an exercise physiology perspective and focuses on the fact that practitioners have all the tools they need to battle this…

  9. The Battle of Bentonville: Caring for Casualties of the Civil War. Teaching with Historic Places.

    ERIC Educational Resources Information Center

    Goode, John C.; Beck, Elaine

    At the First Battle of Manassas (Virginia) in 1861 many Union doctors fled the battlefield in fear. Those who remained found themselves without adequate medical supplies or ambulances for their patients. As the U.S. Civil War progressed and casualties mounted, military surgeons became more adept at caring for the wounded. By the Battle of…

  10. Douglas Haig and the Battle of the Somme

    DTIC Science & Technology

    1984-03-01

    remarkable pictures says one of his biographies. His mother died when he was eighteen. He spent four years at Clifton College, visited America with an...for us. From all I could dis - cover even then, he seemed to be the most highly equipped thinker in the British Army. 1 2 10 At the time, this was the...that Haig’s plan was a strategic success. If we evaluate the Battle of the Sommae against the written objectives that Haig established then it should

  11. Unmanned aircraft systems

    Technology Transfer Automated Retrieval System (TEKTRAN)

    Unmanned platforms have become increasingly more common in recent years for acquiring remotely sensed data. These aircraft are referred to as Unmanned Airborne Vehicles (UAV), Remotely Piloted Aircraft (RPA), Remotely Piloted Vehicles (RPV), or Unmanned Aircraft Systems (UAS), the official term used...

  12. 14 CFR 375.36 - Lease of foreign civil aircraft without crew.

    Code of Federal Regulations, 2010 CFR

    2010-01-01

    ... crew. 375.36 Section 375.36 Aeronautics and Space OFFICE OF THE SECRETARY, DEPARTMENT OF TRANSPORTATION... Authorized Operations § 375.36 Lease of foreign civil aircraft without crew. Foreign civil aircraft that are leased without crew to an air carrier or citizen or permanent resident of the United States, and used...

  13. Aircraft landing gear systems

    NASA Technical Reports Server (NTRS)

    Tanner, John A. (Editor)

    1990-01-01

    Topics presented include the laboratory simulation of landing gear pitch-plane dynamics, a summary of recent aircraft/ground vehicle friction measurement tests, some recent aircraft tire thermal studies, and an evaluation of critical speeds in high-speed aircraft. Also presented are a review of NASA antiskid braking research, titanium matrix composite landing gear development, the current methods and perspective of aircraft flotation analysis, the flow rate and trajectory of water spray produced by an aircraft tire, and spin-up studies of the Space Shuttle Orbiter main gear tire.

  14. Reflections on the Legal Battles Over Prisoners with Gender Dysphoria.

    PubMed

    Levine, Stephen B

    2016-06-01

    Momentum has shifted in the legal battles over the provision of sex reassignment surgery (SRS) for male prisoners. In 2015, two court decisions granted the operation and were not appealed by the California Department of Corrections and Rehabilitation. The author, who has participated in some of these battles as an expert, analyzes the strengths and limitations of the medical illness, developmental, and minority rights paradigms for Gender Dysphoria that are used to reach psychiatric opinions about medical necessity. Courts are influenced by the recommendation of the World Professional Association for Transgender Health (WPATH) that inmates should be treated as are individuals in the community. This is a compassionate assertion, but one not fully informed by practical experience with SRS among prisoners. Most inmates requesting SRS through litigation are serving very long or life sentences. Their backgrounds are quite unlike most transgendered individuals encountered in the community. If long-term prisoners are provided with SRS, the study of their adaptations may enable future decisions to be based on adaptation data rather than the competing opinions of experts. Gathering such data may be challenged as an experiment, however, and viewed as unethical.

  15. Muscle Activity During Unilateral vs. Bilateral Battle Rope Exercises.

    PubMed

    Calatayud, Joaquin; Martin, Fernando; Colado, Juan C; Benítez, Josep C; Jakobsen, Markus D; Andersen, Lars L

    2015-10-01

    High training intensity is important for efficient strength gains. Although battle rope training is metabolically demanding, no studies have quantified intensity of muscle activity during this type of training. This study analyzes muscle activity during unilateral alternating waves vs. bilateral waves of battle rope training. Twenty-one volunteers participated in a repeated-measures study on 2 different occasions. Surface electromyographic signals were recorded from the anterior deltoid (AD), external oblique (OBLIQ), lumbar erector spinae (LUMB), and gluteus medius (GM) during bilateral waves and unilateral waves and were normalized to the maximum voluntary isometric contraction (MVIC). Results showed that muscle activity ranged from 51%MVIC to 73%MVIC for AD, OBLIQ, and LUMB, whereas GM muscle activity was only 14-18%MVIC. OBLIQ activation was significantly greater (20%MVIC; p = 0.02) with the unilateral waves compared with the bilateral waves, whereas LUMB signal was significantly higher (16%MVIC; p = 0.001) with the bilateral waves compared with the unilateral waves. In conclusion, both wave movements can be used to provide moderate to high levels of muscle activity in the AD, OBLIQ, and LUMB. Fitness practitioners aiming for higher OBLIQ activity should perform unilateral waves, whereas the bilateral variation of the movement can be used for higher LUMB activity.

  16. Seaweed rebellion: the battle over section 8(g) revenues

    SciTech Connect

    Fitzgerald, E.A.

    1988-01-01

    Outer continental shelf development has generated a great deal of conflict between the federal and state governments. This conflict, known as the Seaweed Rebellion, has arisen both in the courts and in Congress. One of the most controversial battles of the Seaweed Rebellion involved the disposition of $5.8 billion derived from the development of oil and gas pools common to both federal and state off-shore lands. This battle came to fruition in the case of Texas v. Secretary of Interior (Texas v. Interior). Section 1337(g) (commonly referred to as Section 8(g)) of the Outer Continental Shelf Lands Act (OCSLA) established a three-mile zone extending seaward from state coastal boundaries. Hydrocarbon bearing structures, some of which overlap federal and state lands, are present in this area. Section 8(g) provided for the fair and equitable disposition of revenues derived from the common pools in this zone. In Texas v. Interior, the Federal District Court of the Eastern District of Texas interpreted the meaning of fair and equitable in section 8(g). It provided recovery to Texas for the enhancement of federal bonus receipts resulting from state leasing and the possible sharing of federal taxes. This article provides a brief overview of the conflict, analyzes the Section 8(g) controversy, and explains why the court's decision was correct. Congress eventually amended Section 8(g), and this is also reviewed.

  17. Small transport aircraft technology

    NASA Technical Reports Server (NTRS)

    Williams, L. J.

    1983-01-01

    Information on commuter airline trends and aircraft developments is provided to upgrade the preliminary findings of a NASA-formed small transport aircraft technology (STAT) team, established to determine whether the agency's research and development programs could help commuter aircraft manufacturers solve technical problems related to passenger acceptance and use of 19- to 50-passenger aircraft. The results and conclusions of the full set of completed STAT studies are presented. These studies were performed by five airplane manufacturers, five engine manufacturers, and two propeller manufacturers. Those portions of NASA's overall aeronautics research and development programs which are applicable to commuter aircraft design are summarized. Areas of technology that might beneficially be expanded or initiated to aid the US commuter aircraft manufacturers in the evolution of improved aircraft for the market are suggested.

  18. A New Foodservice System Concept for Aircraft Carriers

    DTIC Science & Technology

    1979-12-01

    Strawberry Milk Shake Flavoring Vanilla Shake Mix Chocolate Shake Mix Precooked Roast Beef Frispo Potato Mix Meatballs #10 CN Pizza Sauce #10...unit for the flake ice water dispenser, carbonated beverage dispenser, non-carbonated beverage dis- penser, iced tea dispenser, hot chocolate ...operate on a 120-Volt, 60 Hz, 1-phase system. Its dimensions are width 9%n, depth 18Vf, and height 18". DISPENSER, HOT CHOCOLATE The hot chocolate

  19. Estimates of Potential Savings by Retiring Two Aircraft Carriers Early

    DTIC Science & Technology

    1989-01-01

    statement) that you have displayed. A wide range of estimate*: can be calculated for the early retirement proposal, as you have said, Mr. Chairman...way implies, as the DOD witnesses suggested, that they agree with the proposal for an early retirement . This case assumes that there would be no indirect cost savings, such as shore base support associated with the retirement.

  20. 76 FR 69320 - Agency Request for Reinstatement of a Previously Approved Information Collection(s): Aircraft...

    Federal Register 2010, 2011, 2012, 2013, 2014

    2011-11-08

    ... Accident Liability Insurance AGENCY: Office of the Secretary (OST), DOT. ACTION: Notice and request for... INFORMATION: OMB Control Number: 2106-0030. Title: Aircraft Accident Liability Insurance. Form Numbers: OST... carriers, and contains the minimum requirements for air carrier accident liability insurance to protect...

  1. Battle Damage Assessment Using Inverse Synthetic Aperture Radar (ISAR)

    DTIC Science & Technology

    2004-12-01

    a. Part 1 - Define the radar parameters and Target Model. % b. Part 2 - Generate the blast effect on traslational motion. % c. Part...effect on traslational motion. %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% % Aircraft Area Profile - Front and Side Areafront = 7.6416

  2. Common Carrier Services.

    ERIC Educational Resources Information Center

    Federal Communications Commission, Washington, DC.

    After outlining the Federal Communications Commission's (FCC) responsibility for regulating interstate common carrier communication (non-broadcast communication whose carriers are required by law to furnish service at reasonable charges upon request), this information bulletin reviews the history, technological development, and current…

  3. The ASAC Air Carrier Investment Model (Second Generation)

    NASA Technical Reports Server (NTRS)

    Wingrove, Earl R., III; Johnson, Jesse P.; Sickles, Robin C.; Good, David H.

    1997-01-01

    To meet its objective of assisting the U.S. aviation industry with the technological challenges of the future, NASA must identify research areas that have the greatest potential for improving the operation of the air transportation system. To accomplish this, NASA is building an Aviation System Analysis Capability (ASAC). The ASAC differs from previous NASA modeling efforts in that the economic behavior of buyers and sellers in the air transportation and aviation industries is central to its conception. To link the economics of flight with the technology of flight, ASAC requires a parametrically based mode with extensions that link airline operations and investments in aircraft with aircraft characteristics. This model also must provide a mechanism for incorporating air travel demand and profitability factors into the airlines' investment decisions. Finally, the model must be flexible and capable of being incorporated into a wide-ranging suite of economic and technical models that are envisioned for ASAC. We describe a second-generation Air Carrier Investment Model that meets these requirements. The enhanced model incorporates econometric results from the supply and demand curves faced by U.S.-scheduled passenger air carriers. It uses detailed information about their fleets in 1995 to make predictions about future aircraft purchases. It enables analysts with the ability to project revenue passenger-miles flown, airline industry employment, airline operating profit margins, numbers and types of aircraft in the fleet, and changes in aircraft manufacturing employment under various user-defined scenarios.

  4. Techniques for modifying airfoils and fairings on aircraft using foam and fiberglass

    NASA Technical Reports Server (NTRS)

    Meyer, M. B.; Jiran, F.

    1981-01-01

    The concept of using foam and fiberglass reinforced plastic to modify airfoils and fairings was applied successfully to high-speed aircraft at NASA Dryden Flight Research Center. An on-aircraft installation method was used to modify an F-15 wing glove and wing leading edge and an F-104 flap trailing edge in support of the Shuttle tile airload tests. A combination of methods, both an on-aircraft installation and an off-aircraft fabrication for installation on the aircraft, was used to modify a section of an F-111 supercritical wing with a natural laminar flow airfoil. Techniques, methods, problem areas, and recommendations are presented which indicate that using foam and fiberglass to modify airfoils and fairings on high-speed aircraft is a viable means of quickly developing airfoils and fairings with desired aerodynamic characteristics with little risk to the parent or carrier aircraft.

  5. Aircraft Loss of Control Study

    NASA Technical Reports Server (NTRS)

    Jacobson, Steven R.

    2010-01-01

    Loss of control has become the leading cause of jet fatalities worldwide. Aside from their frequency of occurrence, accidents resulting from loss of aircraft control seize the public s attention by yielding large numbers of fatalities in a single event. In response to the rising threat to aviation safety, NASA's Aviation Safety Program has conducted a study of the loss of control problem. This study gathered four types of information pertaining to loss of control accidents: (1) statistical data; (2) individual accident reports that cite loss of control as a contributing factor; (3) previous meta-analyses of loss of control accidents; and (4) inputs solicited from aircraft manufacturers, air carriers, researchers, and other industry stakeholders. Using these information resources, the study team identified causal factors that were cited in the greatest number of loss of control accidents, and which were emphasized most by industry stakeholders. For each causal factor that was linked to loss of control, the team solicited ideas about what solutions are required and future research efforts that could potentially help avoid their occurrence or mitigate their consequences when they occurred in flight.

  6. The Role of the U.S. Army in Air Sea Battle

    DTIC Science & Technology

    2013-04-01

    national power to the Asia -Pacific region. The military contribution to this new national security strategy is termed “ Air Sea Battle.” Air Sea Battle...Asian focus under our new national security strategy. The military contribution to this new national security strategy is currently termed “ Air Sea...against a foe with anti-access and area-denial capabilities. As a concept, Air Sea Battle is not new . In one form or another, it has been around as a

  7. Raptors and aircraft

    USGS Publications Warehouse

    Smith, D.G.; Ellis, D.H.; Johnson, T.H.; Glinski, Richard L.; Pendleton, Beth Giron; Moss, Mary Beth; LeFranc, Maurice N.=; Millsap, Brian A.; Hoffman, Stephen W.

    1988-01-01

    Less than 5% of all bird strikes of aircraft are by raptor species, but damage to airframe structure or jet engine dysfunction are likely consequences. Beneficial aircraft-raptor interactions include the use of raptor species to frighten unwanted birds from airport areas and the use of aircraft to census raptor species. Many interactions, however, modify the raptor?s immediate behavior and some may decrease reproduction of sensitive species. Raptors may respond to aircraft stimuli by exhibiting alarm, increased heart rate, flushing or fleeing and occasionally by directly attacking intruding aircraft. To date, most studies reveal that raptor responses to aircraft are brief and do not limit reproduction; however, additional study is needed.

  8. HIV time hierarchy: winning the war while, loosing all the battles

    NASA Astrophysics Data System (ADS)

    Hershberg, Uri; Louzoun, Yoram; Atlan, Henri; Solomon, Sorin

    2001-01-01

    AIDS is the pandemic of our era. A disease that scares us not only because it is fatal but also because its insidious time course makes us all potential carriers long before it hands us our heads in a basket. The strange three stage dynamics of aids is also one of the major puzzles while describing the disease theoretically (Pantaleo et al., N. Engl. J. Med. 328 (1993) 327). Aids starts, like most diseases, in a peak of virus expression [R.M. Zorzenon dos Santos, Immune responses: Getting close to experimental results with cellular automata models, in: D. Stauffer (Ed.), Annual Review of Computational Physics VI, 1999, pp. 159-202; R.M. Zorzenon dos Santos, S.C. Coutinho, On the dynamics of the evolution of HIV infection, cond-mat/0008081], which is practically wiped out by the immune system. However it then remains in the body at a low level of expression until later (some time years later) when there is an outbreak of the disease which terminally cripples the immune system causing death from various common pathogens. In this paper we show, using a microscopic simulation, that the time course of AIDS is determined by the interactions of the virus and the immune cells in the shape space of antigens and that it is the virus's ability to move more rapidly in this space (its high mutability) that causes the time course and eventual “victory” of the disease. These results open the way for further experimental and therapeutic conclusions in the ongoing battle with the HIV epidemic.

  9. Aircraft Survivability. Spring 2009

    DTIC Science & Technology

    2009-01-01

    Surviving an Aircraft Crash with Airbag Restraintsby Thomas Barth Inflatable restraint solutions have improved the survivability of commercial...Surviving an Aircraft Crash with Airbag Restraints by Thomas Barth Transport Aircraft Interiors The AmSafe Aviation Airbag entered service on commercial...all night.” Keithley also noted that, in his early days at BRL, Walt teamed up with a group of like-minded innovators, including Jim Foulk, Roland

  10. Lightning effects on aircraft

    NASA Technical Reports Server (NTRS)

    1977-01-01

    Direct and indirect effects of lightning on aircraft were examined in relation to aircraft design. Specific trends in design leading to more frequent lightning strikes were individually investigated. These trends included the increasing use of miniaturized, solid state components in aircraft electronics and electric power systems. A second trend studied was the increasing use of reinforced plastics and other nonconducting materials in place of aluminum skins, a practice that reduces the electromagnetic shielding furnished by a conductive skin.

  11. The "Battle" of Managing Language Barriers in Health Care.

    PubMed

    Steinberg, Emma M; Valenzuela-Araujo, Doris; Zickafoose, Joseph S; Kieffer, Edith; DeCamp, Lisa Ross

    2016-02-18

    Providing safe and high-quality health care for children whose parents have limited English proficiency (LEP) remains challenging. Reports of parent perspectives on navigating language discordance in health care are limited. We analyzed portions of 48 interviews focused on language barriers from 2 qualitative interview studies of the pediatric health care experiences of LEP Latina mothers in 2 urban US cities. We found mothers experienced frustration with health care and reported suboptimal accommodation for language barriers. Six themes emerged relevant to health care across settings: the "battle" of managing language barriers, preference for bilingual providers, negative bias toward interpreted encounters, "getting by" with limited language skills, fear of being a burden, and stigma and discrimination experienced by LEP families. Parents' insights highlight reasons why effective language accommodation in health care remains challenging. Partnering with families to address the management of language barriers is needed to improve health care quality and safety for LEP patients and families.

  12. Display implementation in the Abrams Main Battle Tank

    NASA Astrophysics Data System (ADS)

    Wyrembelski, Rick J.

    1999-08-01

    This paper provides an overview of a major weapon system, the Abrams Main Battle Tank, as it relates to Flat Panel Display (FPD) technology. The Abrams pioneered FPD implementation in military ground vehicles in response to the integration of embedded computer systems into the tank. This major weapon system is poised to field the latest upgrade, the System Enhancement Package (SEP), with 2nd generation Flat Panel Displays. This has been accomplished by managing requirements, dynamic communication with FPD research and development programs, and aggressively leveraging those programs. The tank has progressed from implementing available FPDs to influencing the enabling of FPD technology. The experience gained offers valuable insight to following ground vehicle systems and to those diligently working to fully enable this critical technology.

  13. Hypersonic aircraft design

    NASA Technical Reports Server (NTRS)

    Alkamhawi, Hani; Greiner, Tom; Fuerst, Gerry; Luich, Shawn; Stonebraker, Bob; Wray, Todd

    1990-01-01

    A hypersonic aircraft is designed which uses scramjets to accelerate from Mach 6 to Mach 10 and sustain that speed for two minutes. Different propulsion systems were considered and it was decided that the aircraft would use one full scale turbofan-ramjet. Two solid rocket boosters were added to save fuel and help the aircraft pass through the transonic region. After considering aerodynamics, aircraft design, stability and control, cooling systems, mission profile, and landing systems, a conventional aircraft configuration was chosen over that of a waverider. The conventional design was chosen due to its landing characteristics and the relative expense compared to the waverider. Fuel requirements and the integration of the engine systems and their inlets are also taken into consideration in the final design. A hypersonic aircraft was designed which uses scramjets to accelerate from Mach 6 to Mach 10 and sustain that speed for two minutes. Different propulsion systems were considered and a full scale turbofan-ramjet was chosen. Two solid rocket boosters were added to save fuel and help the aircraft pass through the transonic reqion. After the aerodynamics, aircraft design, stability and control, cooling systems, mission profile, landing systems, and their physical interactions were considered, a conventional aircraft configuration was chosen over that of a waverider. The conventional design was chosen due to its landing characteristics and the relative expense compared to the waverider. Fuel requirements and the integration of the engine systems and their inlets were also considered in the designing process.

  14. Structureborne noise in aircraft

    NASA Technical Reports Server (NTRS)

    Clevenson, S. A.; Metcalf, V. L.

    1987-01-01

    The amount of noise reaching an aircraft's interior by structureborne paths, when high levels of other noises are present, involves the measurement of transfer functions between vibrating levels on the wing and interior noise. The magnitude of the structureborne noise transfer function is established by exciting the aircraft with an electrodynamic shaker; a second transfer function is measured using the same sensor locations with the aircraft engines operating. Attention is given to the case of a twin-turboprop OV-10A aircraft; the resulting transfer function values at the discrete frequencies corresponding to the propeller blade passage frequency and its first four harmonics are tabulated and illustrated.

  15. The deployable, inflatable wing technology demonstrator experiment aircraft maintains a steady attit

    NASA Technical Reports Server (NTRS)

    2001-01-01

    The deployable, inflatable wing technology demonstrator experiment aircraft maintains a steady attitude following separation from its carrier aircraft during a flight conducted by the NASA Dryden Flight Research Center, Edwards, California. The inflatable wing project represented a basic flight research effort by Dryden personnel. Three successful flights of the I2000 inflatable wing aircraft occurred. During the flights, the team air-launched the radio-controlled (R/C) I2000 from an R/C utility airplane at an altitude of 800-1000 feet. As the I2000 separated from the carrier aircraft, its inflatable wings 'popped-out,' deploying rapidly via an on-board nitrogen bottle. The aircraft remained stable as it transitioned from wingless to winged flight. The unpowered I2000 glided down to a smooth landing under complete control.

  16. Building intelligence in third-generation training and battle simulations

    NASA Astrophysics Data System (ADS)

    Jacobi, Dennis; Anderson, Don; von Borries, Vance; Elmaghraby, Adel; Kantardzic, Mehmed; Ragade, Rammohan

    2003-09-01

    Current war games and simulations are primarily attrition based, and are centered on the concept of force on force. They constitute what can be defined as "second generation" war games. So-called "first generation" war games were focused on strategy with the primary concept of mind on mind. We envision "third generation" war games and battle simulations as concentrating on effects with the primary concept being system on system. Thus the third generation systems will incorporate each successive generation and take into account strategy, attrition and effects. This paper will describe the principal advantages and features that need to be implemented to create a true "third generation" battle simulation and the architectural issues faced when designing and building such a system. Areas of primary concern are doctrine, command and control, allied and coalition warfare, and cascading effects. Effectively addressing the interactive effects of these issues is of critical importance. In order to provide an adaptable and modular system that will accept future modifications and additions with relative ease, we are researching the use of a distributed Multi-Agent System (MAS) that incorporates various artificial intelligence methods. The agent architecture can mirror the military command structure from both vertical and horizontal perspectives while providing the ability to make modifications to doctrine, command structures, inter-command communications, as well as model the results of various effects upon one another, and upon the components of the simulation. This is commonly referred to as "cascading effects," in which A affects B, B affects C and so on. Agents can be used to simulate units or parts of units that interact to form the whole. Even individuals can eventually be simulated to take into account the affect to key individuals such as commanders, heroes, and aces. Each agent will have a learning component built in to provide "individual intelligence" based on

  17. Capital versus talent. The battle that's reshaping business.

    PubMed

    Martin, Roger L; Moldoveanu, Mihnea C

    2003-07-01

    For much of the twentieth century, labor and capital fought bitterly for control of the industrialized economy. The titans of industry ultimately won a resounding victory over the unions, but the story doesn't end there. In today's economy, value is largely the product of knowledge and information. Companies cannot generate profits without the ideas, skills, and leadership capabilities of knowledge workers. It's these factors--not technologies, not factories, and certainly not capital--that give the most successful companies their unique advantages. As knowledge workers come to realize this, and see that the demand for their talent outstrips the supply, they are steadily wresting more and more of the profits from shareholders. This time the battle is between the sources of capital and the producers of value, and how it will end is far from clear. The roots of the current conflict lie in the twentieth-century shift from industrial to managerial capitalism and the creation of a new class of professional talent, the authors explain. Since the arrival of the information-based economy in the past decade, tensions have escalated. The dramatic rise of CEO pay--and the public fire it has drawn--is a telling symptom. With this new battle, we're also witnessing a fundamental change in the political alignment of capital. The Left is now siding with "the common shareholder" against the well-compensated top tier of the labor pool. Shareholders seeing an unprecedented proportion of the return on their investments siphoned off to employees may well ask, is there no end to it? Increasingly, it's human capital that is the basis of value, and financial capital has become far more generic than shareholders would like to believe. The growing tensions between shareholders and managers cannot be ignored, and capitalism is at a crossroads--again.

  18. Type 'A' V/STOL - One aircraft for all support missions

    NASA Technical Reports Server (NTRS)

    Adelt, W. H.

    1981-01-01

    An investigation is conducted regarding the feasibility of developing a single support aircraft type for the Navy, taking into account the current naval inventory of utility aircraft types. Support mission characteristics are examined, giving attention to antisubmarine warfare, airborne early warning, marine assault, carrier on board delivery/vertical on board delivery, the aerial tanker mission, long-range rescue, surface attack, and aspects of combat, search, and rescue. With the aid of a sample design for a V/STOL aircraft with a medium disc loading lift system it is demonstrated that it is now possible to design an aircraft which, with minor modifications, can meet the wide variety of support missions.

  19. B-52 Launch Aircraft in Flight

    NASA Technical Reports Server (NTRS)

    2001-01-01

    NASA's venerable B-52 mothership is seen here photographed from a KC-135 Tanker aircraft. The X-43 adapter is visible attached to the right wing. The B-52, used for launching experimental aircraft and for other flight research projects, has been a familiar sight in the skies over Edwards for more than 40 years and is also both the oldest B-52 still flying and the aircraft with the lowest flight time of any B-52. NASA B-52, Tail Number 008, is an air launch carrier aircraft, 'mothership,' as well as a research aircraft platform that has been used on a variety of research projects. The aircraft, a 'B' model built in 1952 and first flown on June 11, 1955, is the oldest B-52 in flying status and has been used on some of the most significant research projects in aerospace history. Some of the significant projects supported by B-52 008 include the X-15, the lifting bodies, HiMAT (highly maneuverable aircraft technology), Pegasus, validation of parachute systems developed for the space shuttle program (solid-rocket-booster recovery system and the orbiter drag chute system), and the X-38. The B-52 served as the launch vehicle on 106 X-15 flights and flew a total of 159 captive-carry and launch missions in support of that program from June 1959 to October 1968. Information gained from the highly successful X-15 program contributed to the Mercury, Gemini, and Apollo human spaceflight programs as well as space shuttle development. Between 1966 and 1975, the B-52 served as the launch aircraft for 127 of the 144 wingless lifting body flights. In the 1970s and 1980s, the B-52 was the launch aircraft for several aircraft at what is now the Dryden Flight Research Center, Edwards, California, to study spin-stall, high-angle-of attack, and maneuvering characteristics. These included the 3/8-scale F-15/spin research vehicle (SRV), the HiMAT (Highly Maneuverable Aircraft Technology) research vehicle, and the DAST (drones for aerodynamic and structural testing). The aircraft supported

  20. Houston ISD Competes in EPAs Sixth Annual Energy Star Battle of the Buildings

    EPA Pesticide Factsheets

    DALLAS - (July 22, 2015) Today, the Environmental Protection Agency (EPA) launched the 2015 Energy Star Battle of the Buildings. The Houston Independent School District is among the groups fielding 6,500 buildings nationwide in head-to-head competit

  1. Dallas-area School Districts Compete in EPAs Sixth Annual Energy Star Battle of the Buildings

    EPA Pesticide Factsheets

    DALLAS - (July 22, 2015) Today, the Environmental Protection Agency (EPA) launched the 2015 Energy Star Battle of the Buildings. In North Texas, the Carrollton-Farmers Branch, Mansfield and Frisco Independent School Districts are among 125 teams and

  2. New Mexico, Arkansas Kroger Stores Compete in EPAs Sixth Annual Energy Star Battle of the Buildings

    EPA Pesticide Factsheets

    DALLAS - (July 22, 2015) Today, the Environmental Protection Agency (EPA) launched the 2015 Energy Star Battle of the Buildings. Kroger supermarkets and warehouses across New Mexico and Arkansas are among the groups fielding 6,500 buildings nationwi

  3. 124 New England Buildings Compete in EPAs Sixth Annual Energy Star Battle of the Buildings

    EPA Pesticide Factsheets

    Today, the EPA launched the 2015 ENERGY STAR Battle of the Buildings. Nationwide, more than 6,500 buildings of all types and sizes, and 125 teams nationwide are competing head to head to reduce their energy and water use.

  4. 11. PWD Drawing 11,23981 (814C2) (1944), 'Battle Damage Machinery Cleaning ...

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

    11. PWD Drawing 11,239-81 (814-C-2) (1944), 'Battle Damage Machinery Cleaning Bldg., Bldg 814, Pile Record' - Mare Island Naval Shipyard, Chemical Cleaning Facility, North of Fourteenth Street, between California & Railroad Avenue, Vallejo, Solano County, CA

  5. Remote sensing in mineral exploration from LANDSAT imagery. [Battle Mountain, Nevada

    NASA Technical Reports Server (NTRS)

    Nackowski, M. P. (Principal Investigator)

    1976-01-01

    The author has identified the following significant results. Preliminary statistical analysis of length and azimuth of linear stream segments in the Battle Mountain area suggest that segment length (discriminating criterion) can be used to distinguish mineralized from nonmineralized areas.

  6. Study of aerodynamic technology for VSTOL fighter attack aircraft

    NASA Technical Reports Server (NTRS)

    Burhans, W., Jr.; Crafta, V. J., Jr.; Dannenhoffer, N.; Dellamura, F. A.; Krepski, R. E.

    1978-01-01

    Vertical short takeoff aircraft capability, supersonic dash capability, and transonic agility were investigated for the development of Fighter/attack aircraft to be accommodated on ships smaller than present aircraft carriers. Topics covered include: (1) description of viable V/STOL fighter/attack configuration (a high wing, close-coupled canard, twin-engine, control configured aircraft) which meets or exceeds specified levels of vehicle performance; (2) estimates of vehicle aerodynamic characteristics and the methodology utilized to generate them; (3) description of propulsion system characteristics and vehicle mass properties; (4) identification of areas of aerodynamic uncertainty; and (5) a test program to investigate the areas of aerodynamic uncertainty in the conventional flight mode.

  7. Aircraft fires, smoke toxicity, and survival.

    PubMed

    Chaturvedi, A K; Sanders, D C

    1996-03-01

    In-flight fires in modern aircraft are rare, but post-crash fires do occur. Cabin occupants frequently survive initial forces of such crashes but are incapacitated from smoke inhalation. According to an international study, there were 95 fire-related civil passenger aircraft accidents worldwide over a 26-yr period, claiming approximately 2400 lives. Between 1985 and 1991, about 16% (32 accidents) of all U.S. transport aircraft accidents involved fire and 22% (140 fatalities) of the deaths in these accidents resulted from fire/smoke toxicity. Our laboratory analyses of postmortem blood samples (1967-93) indicate that 360 individuals in 134 fatal fire-related civil aircraft (air carrier and general aviation) accidents had carboxyhemoglobin saturation levels (> or = 20%), with or without blood cyanide, high enough to impair performance. Combustion toxicology is now moving from a descriptive to a mechanistic phase. Methods for gas analyses have been developed and combustion/animal-exposure assemblies have been constructed. Material/fire-retardant toxicity and interactions between smoke gases are being studied. Relationships between gas exposure concentrations, blood levels, and incapacitation onset are being established in animal models. Continuing basic research in smoke toxicity will be necessary to understand its complexities, and thus enhance aviation safety and fire survival chances.

  8. Analysis of flight equipment purchasing practices of representative air carriers

    NASA Technical Reports Server (NTRS)

    1977-01-01

    The process through which representative air carriers decide whether or not to purchase flight equipment was investigated as well as their practices and policies in retiring surplus aircraft. An analysis of the flight equipment investment decision process in ten airlines shows that for the airline industry as a whole, the flight equipment investment decision is in a state of transition from a wholly informal process in earliest years to a much more organized and structured process in the future. Individual air carriers are in different stages with respect to the formality and sophistication associated with the flight equipment investment decision.

  9. The Military Decision Making Process and the Battle of the Little Bighorn

    DTIC Science & Technology

    2001-04-25

    50 APPENDIX A, The 1868 Treaty of Laramie 51 APPENDIX B, West Point Curriculum 53 APPENDIX C, Other Campaigns and/or Battles for Custer to Study 56...the defeat of the 7th Cavalry in Montana remains vivid in America’s culture. In his exhaustive character study of the battle, Evan S. Connell writes...4Evan S. Connell , Son of the Morning Star, (San Francisco: North Point Press, 1984), 356. 5Public

  10. Tobacco wars: the bloody battle between good health and good politics

    PubMed Central

    Gray, C

    1997-01-01

    A battle to introduce new antitobacco legislation in Canada has caused political battles within the Liberal Party. While one side is worried about the need to protect people's health, another is worried about the potential loss of jobs within the tobacco industry--many of which are located in politically volatile Quebec. Charlotte Gray writes about the machinations that led to the introduction of new smoking legislation in the House of Commons in November. PMID:9012729

  11. Understanding and Modeling Information Dominance in Battle Management: Applications of Fuzzy Cognitive Maps

    DTIC Science & Technology

    1998-03-01

    The report takes a unique look at information dominance and how it relates to shared situation awareness and the decision making cycles of the OODA...loop. An explanation of information dominance is developed through a historical example of battle management (the Battle of Britain) to demonstrate the...contemporary information dominance . Fuzzy cognitive mapping, a method for eliciting and modeling human interactions in complex situations (such as information

  12. Electrospark Deposition for the Repair of Army Main Battle Tank Components

    DTIC Science & Technology

    2006-07-01

    Electrospark Deposition for the Repair of Army Main Battle Tank Components by Victor Champagne, Marc Pepi, and Brian Edwards ARL-TR...July 2006 Electrospark Deposition for the Repair of Army Main Battle Tank Components Victor Champagne, Marc Pepi, and Brian Edwards...Final 3. DATES COVERED (From - To) March 2005–March 2006 5a. CONTRACT NUMBER 5b. GRANT NUMBER 4. TITLE AND SUBTITLE Electrospark Deposition for

  13. The First Battle of Fredericksburg: Lessons of Strategic and Operational Command and Control

    DTIC Science & Technology

    2011-03-15

    28 Hebert, Walter H. Fighting Joe Hooker . (New York: The Bobbs-Merrill Company, 1944), 152. 29 Marvel, William . The Battle of Fredericksburg Civil...Walter H. Fighting Joe Hooker . (New York: The Bobbs-Merrill Company, 1944), 161. 32 Marvel, William . The Battle of Fredericksburg Civil War Series...Major General Ambrose E. Burnside, to Major Ge~eral Joseph Hooker , and finally Major General George G. Meade. Organizational change can be difficult

  14. General Aviation Aircraft Reliability Study

    NASA Technical Reports Server (NTRS)

    Pettit, Duane; Turnbull, Andrew; Roelant, Henk A. (Technical Monitor)

    2001-01-01

    This reliability study was performed in order to provide the aviation community with an estimate of Complex General Aviation (GA) Aircraft System reliability. To successfully improve the safety and reliability for the next generation of GA aircraft, a study of current GA aircraft attributes was prudent. This was accomplished by benchmarking the reliability of operational Complex GA Aircraft Systems. Specifically, Complex GA Aircraft System reliability was estimated using data obtained from the logbooks of a random sample of the Complex GA Aircraft population.

  15. Development Cycle Time Simulation for Civil Aircraft

    NASA Technical Reports Server (NTRS)

    Spitz, William; Berardino, Frank; Golaszewski, Richard; Johnson, Jesse

    2001-01-01

    Cycle Time Reduction (CTR) will be one of the major factors affecting the future of the civil aerospace industry. This focus is the end reflection of the level of competition in the commercial large carrier aircraft industry. Aircraft manufacturer must minimize costs and pass a portion of those savings onto buyers. CTR is one strategy used to move the manufacturing firm down the cost curve. The current NASA Airframe Development Cycle Time Reduction Goal is 50% by year 2022. This goal is not achievable based on the program analysis done by the LMI/GRA team. This may mean that the current roster of NASA CTR programs needs to be reexamined or that the program technology progress factors, as determined by the NASA experts, were understated. Programs that duplicate the reductions of others should be replaced with non-duplicative programs. In addition, new programs targeting a specific part of the cycle can be developed.

  16. Cable Tensiometer for Aircraft

    NASA Technical Reports Server (NTRS)

    Nunnelee, Mark (Inventor)

    2008-01-01

    The invention is a cable tensiometer that can be used on aircraft for real-time, in-flight cable tension measurements. The invention can be used on any aircraft cables with high precision. The invention is extremely light-weight, hangs on the cable being tested and uses a dual bending beam design with a high mill-volt output to determine tension.

  17. Lightning protection of aircraft

    NASA Technical Reports Server (NTRS)

    Fisher, F. A.; Plumer, J. A.

    1977-01-01

    The current knowledge concerning potential lightning effects on aircraft and the means that are available to designers and operators to protect against these effects are summarized. The increased use of nonmetallic materials in the structure of aircraft and the constant trend toward using electronic equipment to handle flight-critical control and navigation functions have served as impetus for this study.

  18. Aircraft landing control system

    NASA Technical Reports Server (NTRS)

    Lambregts, Antonius A. (Inventor); Hansen, Rolf (Inventor)

    1982-01-01

    Upon aircraft landing approach, flare path command signals of altitude, vertical velocity and vertical acceleration are generated as functions of aircraft position and velocity with respect to the ground. The command signals are compared with corresponding actual values to generate error signals which are used to control the flight path.

  19. Predicting Aircraft Availability

    DTIC Science & Technology

    2013-06-01

    ENS- GRP -13-J-2 DEPARTMENT OF THE AIR FORCE AIR UNIVERSITY AIR FORCE INSTITUTE OF TECHNOLOGY Wright-Patterson Air Force Base, Ohio...AFIT-ENS- GRP -13-J-2 PREDICTING AIRCRAFT AVAILABILITY GRADUATE RESEARCH PROJECT Presented to the Faculty Department of Operational...APPROVED FOR PUBLIC RELEASE; DISTRIBUTION UNLIMITED AFIT-ENS- GRP -13-J-2 PREDICTING AIRCRAFT AVAILABILITY Mark A. Chapa

  20. Why aircraft disinsection?

    PubMed

    Gratz, N G; Steffen, R; Cocksedge, W

    2000-01-01

    A serious problem is posed by the inadvertent transport of live mosquitoes aboard aircraft arriving from tropical countries where vector-borne diseases are endemic. Surveys at international airports have found many instances of live insects, particularly mosquitoes, aboard aircraft arriving from countries where malaria and arboviruses are endemic. In some instances mosquito species have been established in countries in which they have not previously been reported. A serious consequence of the transport of infected mosquitoes aboard aircraft has been the numerous cases of "airport malaria" reported from Europe, North America and elsewhere. There is an important on-going need for the disinsection of aircraft coming from airports in tropical disease endemic areas into nonendemic areas. The methods and materials available for use in aircraft disinsection and the WHO recommendations for their use are described.

  1. Why aircraft disinsection?

    PubMed Central

    Gratz, N. G.; Steffen, R.; Cocksedge, W.

    2000-01-01

    A serious problem is posed by the inadvertent transport of live mosquitoes aboard aircraft arriving from tropical countries where vector-borne diseases are endemic. Surveys at international airports have found many instances of live insects, particularly mosquitoes, aboard aircraft arriving from countries where malaria and arboviruses are endemic. In some instances mosquito species have been established in countries in which they have not previously been reported. A serious consequence of the transport of infected mosquitoes aboard aircraft has been the numerous cases of "airport malaria" reported from Europe, North America and elsewhere. There is an important on-going need for the disinsection of aircraft coming from airports in tropical disease endemic areas into nonendemic areas. The methods and materials available for use in aircraft disinsection and the WHO recommendations for their use are described. PMID:10994283

  2. Aircraft operations management manual

    NASA Technical Reports Server (NTRS)

    1992-01-01

    The NASA aircraft operations program is a multifaceted, highly diverse entity that directly supports the agency mission in aeronautical research and development, space science and applications, space flight, astronaut readiness training, and related activities through research and development, program support, and mission management aircraft operations flights. Users of the program are interagency, inter-government, international, and the business community. This manual provides guidelines to establish policy for the management of NASA aircraft resources, aircraft operations, and related matters. This policy is an integral part of and must be followed when establishing field installation policy and procedures covering the management of NASA aircraft operations. Each operating location will develop appropriate local procedures that conform with the requirements of this handbook. This manual should be used in conjunction with other governing instructions, handbooks, and manuals.

  3. Millimeter-Wave Localizers for Aircraft-to-Aircraft Approach Navigation

    NASA Technical Reports Server (NTRS)

    Tang, Adrian J.

    2013-01-01

    Aerial refueling technology for both manned and unmanned aircraft is critical for operations where extended aircraft flight time is required. Existing refueling assets are typically manned aircraft, which couple to a second aircraft through the use of a refueling boom. Alignment and mating of the two aircraft continues to rely on human control with use of high-resolution cameras. With the recent advances in unmanned aircraft, it would be highly advantageous to remove/reduce human control from the refueling process, simplifying the amount of remote mission management and enabling new operational scenarios. Existing aerial refueling uses a camera, making it non-autonomous and prone to human error. Existing commercial localizer technology has proven robust and reliable, but not suited for aircraft-to-aircraft approaches like in aerial refueling scenarios since the resolution is too coarse (approximately one meter). A localizer approach system for aircraft-to-aircraft docking can be constructed using the same modulation with a millimeterwave carrier to provide high resolution. One technology used to remotely align commercial aircraft on approach to a runway are ILS (instrument landing systems). ILS have been in service within the U.S. for almost 50 years. In a commercial ILS, two partially overlapping beams of UHF (109 to 126 MHz) are broadcast from an antenna array so that their overlapping region defines the centerline of the runway. This is called a localizer system and is responsible for horizontal alignment of the approach. One beam is modulated with a 150-Hz tone, while the other with a 90-Hz tone. Through comparison of the modulation depths of both tones, an autopilot system aligns the approaching aircraft with the runway centerline. A similar system called a glide-slope (GS) exists in the 320-to-330MHz band for vertical alignment of the approach. While this technology has been proven reliable for millions of commercial flights annually, its UHF nature limits

  4. Field of View Requirements for Carrier Landing Training

    DTIC Science & Technology

    1980-06-01

    Pilot Training ( ASPT ) at Williams Air Force Base. The visual image for the simulation was provided by a data base which crea&.ed the aircraft carrier...USS Forrestal (CVA-59) in the ASPT computer-image-generation systor.m. The pilots in these three groups’ were trained under different conditions. Two...Advanced Simalator for Pilot Training ( ASPT ) would be ideal for this effort, and later, Lt Col Samuel T. Hannan and Capt Ricky A. Perry were assigned

  5. Portable Catapult Launcher For Small Aircraft

    NASA Technical Reports Server (NTRS)

    Rosenbaum, Bernard J. (Inventor); Petter, George E. (Inventor); Gessler, Joseph A. (Inventor); Hughes, Michael G. (Inventor)

    2005-01-01

    An apparatus for launching an aircraft having a multiplicity of interconnected elongated tracks of rigid material forming a track system and wherein each elongated track has a predetermined elongated track cross-sectional design, a winch system connected to the track system wherein the winch system has a variable mechanical advantage, one or more elongated elastic members wherein one end of each of the one or more elongated elastic members is adjustably connected to the track system, and a carrier slidably mounted to the track system wherein the canier is connected to the winch system and to the other end of each of the one or more elongated elastic members.

  6. Small transport aircraft technology. A report for the committee on commerce, science, and transportation, United States Senate

    NASA Technical Reports Server (NTRS)

    1979-01-01

    A preliminary assessment of the research and technology that NASA could undertake to improve small transport aircraft is presented. The advanced technologies currently under study for potential application to the small transport aircraft of the future are outlined. Background information on the commuter and shorthaul local service air carriers, the regulations pertaining to their aircraft and operations, and the overall airline system interface is included.

  7. SDI (Strategic Defense Initiative) Battle Management/C3 (Command, Control, and Communications) Networking Technology Program Plan

    DTIC Science & Technology

    1988-12-01

    Copy 20 o5o 00 IDA MEMORANDUM REPORT M-305 CDNN N 3 SDI BATTLE MANAGEMENT/C NETWORKING ! TECHNOLOGY PROGRAM PLAN Robert Botta Sharon Noll December...Battle Management/C3 Networking Technology Program Plan 12. PERSONAL AUTHOR(S). Robert Botta, Sharon Noll 12. TYPE OF REPORT 3b. TIME COVERED 14. DATE OF...The Institute for Defense Analyses (IDA) has collected and analyzed information on network technology that is relevant to Battle Management Command

  8. A NASA study of the impact of technology on future sea based attack aircraft

    NASA Technical Reports Server (NTRS)

    Hahn, Andrew S.

    1992-01-01

    A conceptual aircraft design study was recently completed evaluating carrier-based, subsonic attack aircraft using contemporary and future technology assumptions. The study examined a configuration matrix that was made up of light and medium bomb loads, one and two man crews, internal and external weapons carriage, as well as conventional and flying wing planforms. Use of common technology assumptions, engine cycle simulation code, design mission, and consistent application of methods allow for direct comparison of the aircraft. This paper describes the design study ground rules and the aircraft designed. The aircraft descriptions include weights, dimensions, layout, design mission, design constraints, maneuver performance, and fallout mission performance. The strengths, and weaknesses of each aircraft are highlighted.

  9. Predicting Visibility of Aircraft

    PubMed Central

    Watson, Andrew; Ramirez, Cesar V.; Salud, Ellen

    2009-01-01

    Visual detection of aircraft by human observers is an important element of aviation safety. To assess and ensure safety, it would be useful to be able to be able to predict the visibility, to a human observer, of an aircraft of specified size, shape, distance, and coloration. Examples include assuring safe separation among aircraft and between aircraft and unmanned vehicles, design of airport control towers, and efforts to enhance or suppress the visibility of military and rescue vehicles. We have recently developed a simple metric of pattern visibility, the Spatial Standard Observer (SSO). In this report we examine whether the SSO can predict visibility of simulated aircraft images. We constructed a set of aircraft images from three-dimensional computer graphic models, and measured the luminance contrast threshold for each image from three human observers. The data were well predicted by the SSO. Finally, we show how to use the SSO to predict visibility range for aircraft of arbitrary size, shape, distance, and coloration. PMID:19462007

  10. Predicting visibility of aircraft.

    PubMed

    Watson, Andrew; Ramirez, Cesar V; Salud, Ellen

    2009-05-20

    Visual detection of aircraft by human observers is an important element of aviation safety. To assess and ensure safety, it would be useful to be able to be able to predict the visibility, to a human observer, of an aircraft of specified size, shape, distance, and coloration. Examples include assuring safe separation among aircraft and between aircraft and unmanned vehicles, design of airport control towers, and efforts to enhance or suppress the visibility of military and rescue vehicles. We have recently developed a simple metric of pattern visibility, the Spatial Standard Observer (SSO). In this report we examine whether the SSO can predict visibility of simulated aircraft images. We constructed a set of aircraft images from three-dimensional computer graphic models, and measured the luminance contrast threshold for each image from three human observers. The data were well predicted by the SSO. Finally, we show how to use the SSO to predict visibility range for aircraft of arbitrary size, shape, distance, and coloration.

  11. Estimate of air carrier and air taxi crash frequencies from high altitude en route flight operations

    SciTech Connect

    Sanzo, D.; Kimura, C.Y.; Prassinos, P.G.

    1996-06-03

    In estimating the frequency of an aircraft crashing into a facility, it has been found convenient to break the problem down into two broad categories. One category estimates the aircraft crash frequency due to air traffic from nearby airports, the so-called near-airport environment. The other category estimates the aircraft crash frequency onto facilities due to air traffic from airways, jet routes, and other traffic flying outside the near-airport environment The total aircraft crash frequency is the summation of the crash frequencies from each airport near the facility under evaluation and from all airways, jet routes, and other traffic near the facility of interest. This paper will examine the problems associated with the determining the aircraft crash frequencies onto facilities outside the near-airport environment. This paper will further concentrate on the estimating the risk of aircraft crashes to ground facilities due to high altitude air carrier and air taxi traffic. High altitude air carrier and air taxi traffic will be defined as all air carrier and air taxi flights above 18,000 feet Mean Sea Level (MSL).

  12. Automatic carrier acquisition system

    NASA Technical Reports Server (NTRS)

    Bunce, R. C. (Inventor)

    1973-01-01

    An automatic carrier acquisition system for a phase locked loop (PLL) receiver is disclosed. It includes a local oscillator, which sweeps the receiver to tune across the carrier frequency uncertainty range until the carrier crosses the receiver IF reference. Such crossing is detected by an automatic acquisition detector. It receives the IF signal from the receiver as well as the IF reference. It includes a pair of multipliers which multiply the IF signal with the IF reference in phase and in quadrature. The outputs of the multipliers are filtered through bandpass filters and power detected. The output of the power detector has a signal dc component which is optimized with respect to the noise dc level by the selection of the time constants of the filters as a function of the sweep rate of the local oscillator.

  13. Some fighter aircraft trends

    NASA Technical Reports Server (NTRS)

    Spearman, L.

    1985-01-01

    Some basic trends in fighters are traced from the post World II era. Beginning with the first operational jet fighter, the P-80, the characteristics of subsequent fighter aircraft are examined for performance, mission capability, effectiveness, and cost. Characteristics presented include: power loading, wing loading, maximum speed, rate of climb, turn rate, weight and weight distribution, cost and cost distribution. The characteristics of some USSR aircraft are included for comparison. The trends indicate some of the rationale for certain fighter designs and some likely characteristics to be sought in future fighter aircraft designs.

  14. Tropospheric sampling with aircraft

    SciTech Connect

    Daum, P.H.; Springston, S.R.

    1991-03-01

    Aircraft constitute a unique environment which places stringent requirements on the instruments used to measure the concentrations of atmospheric trace gases and aerosols. Some of these requirements such as minimization of size, weight, and power consumption are general; others are specific to individual techniques. This review presents the basic principles and considerations governing the deployment of trace gas and aerosol instrumentation on an aircraft. An overview of common instruments illustrates these points and provides guidelines for designing and using instruments on aircraft-based measurement programs.

  15. Microwave imaging of aircraft

    NASA Astrophysics Data System (ADS)

    Steinberg, Bernard D.

    1988-12-01

    Three methods of imaging aircraft from the ground with microwave radar with quality suitable for aircraft target recognition are described. The imaging methods are based on a self-calibration procedure called adaptive beamforming that compensates for the severe geometric distortion inherent in any imaging system that is large enough to achieve the high angular resolution necessary for two-dimensional target imaging. The signal processing algorithm is described and X-band (3-cm)-wavelength experiments demonstrate its success on commercial aircraft flying into Philadelphia International Airport.

  16. Aircraft compass characteristics

    NASA Technical Reports Server (NTRS)

    Peterson, John B; Smith, Clyde W

    1937-01-01

    A description of the test methods used at the National Bureau of Standards for determining the characteristics of aircraft compasses is given. The methods described are particularly applicable to compasses in which mineral oil is used as the damping liquid. Data on the viscosity and density of certain mineral oils used in United States Navy aircraft compasses are presented. Characteristics of Navy aircraft compasses IV to IX and some other compasses are shown for the range of temperatures experienced in flight. Results of flight tests are presented. These results indicate that the characteristic most desired in a steering compass is a short period and, in a check compass, a low overswing.

  17. Testing Aircraft Instruments.

    DTIC Science & Technology

    1981-02-11

    AD-A095 680 ARMY TEST AND EVALUATION COMMAND ABERDEEN PROVING GRO--ETC F/S 1/4 TESTING AIRCRAFT INSTRUMENTS .(U) FEB 81 CLASSIFIED TOP-6-3-013 ML I...Test and Evaluation Command -?Final 7, Ts .to .. eg----- ( -4_ Fia - / + I ORG REPORT STesting Aircraft Instruments , j P I- I. AUTHOR(es) S. CONTRACT...Identify by block number) This document presents information and procedures for testing aircraft flight and systems performance instruments in the functional

  18. HIV-positive father wins visitation battle in Maryland.

    PubMed

    1995-03-24

    [Name removed], after a four-year court battle, has been awarded visitation rights with his three daughters. [Name removed] separated from his wife [name removed] in [name removed] 1991 after telling her he was diagnosed with HIV. The custody dispute originally centered around not only [name removed]'s HIV status, but also his homosexuality (he had left his wife for the family friend and godfather to one of the couple's daughter's). Custody judge Audrey E. Melbourne allowed [name removed] to see his daughters at his home, excluding overnight, weekday or holiday visits. [Name removed]'s appeal focused on the medical aspects of HIV transmission in the household. Since Mrs. [Name removed]' expert witness conceded that he knew of no recorded instances of a person transmitting HIV to another person through bathing, cooking or breathing, the judge agreed the risk of transmission was so small as to pose no threat to the children's safety. [Name removed] was awarded visitation on alternating weekends, plus alternating Federal holidays.

  19. Preliminary analysis of long-range aircraft designs for future heavy airlift missions

    NASA Technical Reports Server (NTRS)

    Nelms, W. P., Jr.; Murphy, R.; Barlow, A.

    1976-01-01

    A computerized design study of very large cargo aircraft for the future heavy airlift mission was conducted using the Aircraft Synthesis program (ACSYNT). The study was requested by the Air Force under an agreement whereby Ames provides computerized design support to the Air Force Flight Dynamics Laboratory. This effort is part of an overall Air Force program to study advanced technology large aircraft systems. Included in the Air Force large aircraft program are investigations of missions such as heavy airlift, airborne missile launch, battle platform, command and control, and aerial tanker. The Ames studies concentrated on large cargo aircraft of conventional design with payloads from 250,000 to 350,000 lb. Range missions up to 6500 n.mi. and radius missions up to 3600 n.mi. have been considered. Takeoff and landing distances between 7,000 and 10,000 ft are important constraints on the configuration concepts. The results indicate that a configuration employing conventional technology in all disciplinary areas weighs approximately 2 million pounds to accomplish either a 6500-n.mi. range mission or a 3600-n.mi. radius mission with a 350,000-lb payload.

  20. Solar thermal aircraft

    DOEpatents

    Bennett, Charles L.

    2007-09-18

    A solar thermal powered aircraft powered by heat energy from the sun. A heat engine, such as a Stirling engine, is carried by the aircraft body for producing power for a propulsion mechanism, such as a propeller. The heat engine has a thermal battery in thermal contact with it so that heat is supplied from the thermal battery. A solar concentrator, such as reflective parabolic trough, is movably connected to an optically transparent section of the aircraft body for receiving and concentrating solar energy from within the aircraft. Concentrated solar energy is collected by a heat collection and transport conduit, and heat transported to the thermal battery. A solar tracker includes a heliostat for determining optimal alignment with the sun, and a drive motor actuating the solar concentrator into optimal alignment with the sun based on a determination by the heliostat.

  1. Aircraft parameter estimation

    NASA Technical Reports Server (NTRS)

    Iliff, Kenneth W.

    1987-01-01

    The aircraft parameter estimation problem is used to illustrate the utility of parameter estimation, which applies to many engineering and scientific fields. Maximum likelihood estimation has been used to extract stability and control derivatives from flight data for many years. This paper presents some of the basic concepts of aircraft parameter estimation and briefly surveys the literature in the field. The maximum likelihood estimator is discussed, and the basic concepts of minimization and estimation are examined for a simple simulated aircraft example. The cost functions that are to be minimized during estimation are defined and discussed. Graphic representations of the cost functions are given to illustrate the minimization process. Finally, the basic concepts are generalized, and estimation from flight data is discussed. Some of the major conclusions for the simulated example are also developed for the analysis of flight data from the F-14, highly maneuverable aircraft technology (HiMAT), and space shuttle vehicles.

  2. Laminar Flow Aircraft Certification

    NASA Technical Reports Server (NTRS)

    Williams, Louis J. (Compiler)

    1986-01-01

    Various topics telative to laminar flow aircraft certification are discussed. Boundary layer stability, flaps for laminar flow airfoils, computational wing design studies, manufacturing requirements, windtunnel tests, and flow visualization are among the topics covered.

  3. Pollution reducing aircraft propulsion

    SciTech Connect

    Tamura, R. M.

    1985-05-28

    Aircraft engine exhaust is mixed with air and fuel and recombusted. Air is drawn into the secondary combustion chamber from suction surfaces on wings. Exhaust of the secondary combustion chamber is blown over wing and fuselage surfaces.

  4. The Aircraft Morphing Program

    NASA Technical Reports Server (NTRS)

    Wlezien, R. W.; Horner, G. C.; McGowan, A. R.; Padula, S. L.; Scott, M. A.; Silcox, R. J.; Simpson, J. O.

    1998-01-01

    In the last decade smart technologies have become enablers that cut across traditional boundaries in materials science and engineering. Here we define smart to mean embedded actuation, sensing, and control logic in a tightly coupled feedback loop. While multiple successes have been achieved in the laboratory, we have yet to see the general applicability of smart devices to real aircraft systems. The NASA Aircraft Morphing program is an attempt to couple research across a wide range of disciplines to integrate smart technologies into high payoff aircraft applications. The program bridges research in seven individual disciplines and combines the effort into activities in three primary program thrusts. System studies are used to assess the highest- payoff program objectives, and specific research activities are defined to address the technologies required for development of smart aircraft systems. In this paper we address the overall program goals and programmatic structure, and discuss the challenges associated with bringing the technologies to fruition.

  5. Aircraft electromagnetic compatibility

    NASA Technical Reports Server (NTRS)

    Clarke, Clifton A.; Larsen, William E.

    1987-01-01

    Illustrated are aircraft architecture, electromagnetic interference environments, electromagnetic compatibility protection techniques, program specifications, tasks, and verification and validation procedures. The environment of 400 Hz power, electrical transients, and radio frequency fields are portrayed and related to thresholds of avionics electronics. Five layers of protection for avionics are defined. Recognition is given to some present day electromagnetic compatibility weaknesses and issues which serve to reemphasize the importance of EMC verification of equipment and parts, and their ultimate EMC validation on the aircraft. Proven standards of grounding, bonding, shielding, wiring, and packaging are laid out to help provide a foundation for a comprehensive approach to successful future aircraft design and an understanding of cost effective EMC in an aircraft setting.

  6. Aircraft Engine Emissions. [conference

    NASA Technical Reports Server (NTRS)

    1977-01-01

    A conference on a aircraft engine emissions was held to present the results of recent and current work. Such diverse areas as components, controls, energy efficient engine designs, and noise and pollution reduction are discussed.

  7. Depreciation of aircraft

    NASA Technical Reports Server (NTRS)

    Warner, Edward P

    1922-01-01

    There is a widespread, and quite erroneous, impression to the effect that aircraft are essentially fragile and deteriorate with great rapidity when in service, so that the depreciation charges to be allowed on commercial or private operation are necessarily high.

  8. Aircraft Morphing program

    NASA Astrophysics Data System (ADS)

    Wlezien, Richard W.; Horner, Garnett C.; McGowan, Anna-Maria R.; Padula, Sharon L.; Scott, Michael A.; Silcox, Richard J.; Harrison, Joycelyn S.

    1998-06-01

    In the last decade smart technologies have become enablers that cut across traditional boundaries in materials science and engineering. Here we define smart to mean embedded actuation, sensing, and control logic in a tightly coupled feedback loop. While multiple successes have been achieved in the laboratory, we have yet to see the general applicability of smart devices to real aircraft systems. The NASA Aircraft Morphing program is an attempt to couple research across a wide range of disciplines to integrate smart technologies into high payoff aircraft applications. The program bridges research in seven individual disciplines and combines the effort into activities in three primary program thrusts. System studies are used to assess the highest-payoff program objectives, and specific research activities are defined to address the technologies required for development of smart aircraft systems. In this paper we address the overall program goals and programmatic structure, and discuss the challenges associated with bringing the technologies to fruition.

  9. Advanced hypersonic aircraft design

    NASA Technical Reports Server (NTRS)

    Utzinger, Rob; Blank, Hans-Joachim; Cox, Craig; Harvey, Greg; Mckee, Mike; Molnar, Dave; Nagy, Greg; Petersen, Steve

    1992-01-01

    The objective of this design project is to develop the hypersonic reconnaissance aircraft to replace the SR-71 and to complement existing intelligence gathering devices. The initial design considerations were to create a manned vehicle which could complete its mission with at least two airborne refuelings. The aircraft must travel between Mach 4 and Mach 7 at an altitude of 80,000 feet for a maximum range of 12,000 nautical miles. The vehicle should have an air breathing propulsion system at cruise. With a crew of two, the aircraft should be able to take off and land on a 10,000 foot runway, and the yearly operational costs were not to exceed $300 million. Finally, the aircraft should exhibit stealth characteristics, including a minimized radar cross-section (RCS) and a reduced sonic boom. The technology used in this vehicle should allow for production between the years 1993 and 1995.

  10. Preconception Carrier Screening

    MedlinePlus

    ... What can the results of a carrier screening test tell me? A genetic counselor or your health care provider will use the results to calculate the ... the publisher. Related FAQs Genetic Disorders (FAQ094) Screening Tests for Birth Defects ... Education & Events Annual Meeting CME Overview CREOG ...

  11. Common Carrier Services.

    ERIC Educational Resources Information Center

    Federal Communications Commission, Washington, DC.

    This bulletin outlines the Federal Communications Commission's (FCC) responsibilities in regulating the interstate and foreign common carrier communication via electrical means. Also summarized are the history, technological development, and current capabilities and prospects of telegraph, wire telephone, radiotelephone, satellite communications,…

  12. Synthetic carriers of oxygen.

    PubMed

    Dellacherie, E; Labrude, P; Vigneron, C; Riess, J G

    1987-01-01

    During the last decade, construction of artificial carriers of oxygen for transfusion purposes has evolved in three main directions, which can be reviewed as follows. The first approach consists of modifying hemoglobin (Hb), the natural oxygen carrier, in order to lower its oxygen affinity and increase its intravascular persistence. To achieve this aim, two basic procedures have been used: molecular and environmental modification. In the first case, Hb is modified with chemical reagents; the second requires encapsulation of Hb to obtain artificial erythrocytes. The second approach is based on the use of synthetic oxygen-carrying chelates that mimic the oxygenation function of Hb. The main products in this class are metalloporphyrins, whose chemical environment is designed to render them efficient as reversible carriers of oxygen in vivo. Finally, the third approach deals with the perfluorochemicals used in emulsified form. Perfluorochemical liquids are excellent gas solvents, but some problems remain unsolved with regard to their development as oxygen carriers in vivo: low O2 dissolving capacity, toxicity, and excretion.

  13. ANALYSIS OF AIRCRAFT MOTIONS

    NASA Technical Reports Server (NTRS)

    Wingrove, R. C.

    1994-01-01

    This program was developed by Ames Research Center, in cooperation with the National Transportation Safety Board, as a technique for deriving time histories of an aircraft's motion from Air Traffic Control (ATC) radar records. This technique uses the radar range and azimuth data, along with the downlinked altitude data, to derive an expanded set of data which includes airspeed, lift, attitude angles (pitch, roll, and heading), etc. This technique should prove useful as a source of data in the investigation of commercial airline accidents and in the analysis of accidents involving aircraft which do not have onboard data recorders (e.g., military, short-haul, and general aviation). The technique used to determine the aircraft motions involves smoothing of raw radar data. These smoothed results, in combination with other available information (wind profiles and aircraft performance data), are used to derive the expanded set of data. This program uses a cubic least-square fit to smooth the raw data. This moving-arc procedure provides a smoothed time history of the aircraft position, the inertial velocities, and accelerations. Using known winds, these inertial data are transformed to aircraft stability axes to provide true airspeed, thrust-drag, lift, and roll angle. Further derivation, based on aircraft dependent performance data, can determine the aircraft angle of attack, pitch, and heading angle. Results of experimental tests indicate that values derived from ATC radar records using this technique agree favorably with airborne measurements. This program is written in FORTRAN IV to be executed in the batch mode, and has been implemented on a CDC 6000 series computer with a central memory requirement of 64k (octal) of 60 bit words.

  14. Alternative jet aircraft fuels

    NASA Technical Reports Server (NTRS)

    Grobman, J.

    1979-01-01

    Potential changes in jet aircraft fuel specifications due to shifts in supply and quality of refinery feedstocks are discussed with emphasis on the effects these changes would have on the performance and durability of aircraft engines and fuel systems. Combustion characteristics, fuel thermal stability, and fuel pumpability at low temperature are among the factors considered. Combustor and fuel system technology needs for broad specification fuels are reviewed including prevention of fuel system fouling and fuel system technology for fuels with higher freezing points.

  15. The Battle of the Malvinas: The Argentinian Version,

    DTIC Science & Technology

    1983-05-16

    waters, where the shallow water depth prevent submarine attack. The Argentine submarine SAN LUIS (Class 209) fired one or more torpedoes at a range of...Coast Guard personnel and 13 civilian seamen were killed. On the same day, the Argentine submarine SAN LUIS fired 4 14 torpedoes at two targets at a...aircraft missile launchers of the British The reports of one or more attacks of the Argentine SEA CAT type. It is unclear submarine SAN LUIS (Class

  16. Aircraft as Research Tools

    NASA Technical Reports Server (NTRS)

    1999-01-01

    Aeronautical research usually begins with computers, wind tunnels, and flight simulators, but eventually the theories must fly. This is when flight research begins, and aircraft are the primary tools of the trade. Flight research involves doing precision maneuvers in either a specially built experimental aircraft or an existing production airplane that has been modified. For example, the AD-1 was a unique airplane made only for flight research, while the NASA F-18 High Alpha Research Vehicle (HARV) was a standard fighter aircraft that was transformed into a one-of-a-kind aircraft as it was fitted with new propulsion systems, flight controls, and scientific equipment. All research aircraft are able to perform scientific experiments because of the onboard instruments that record data about its systems, aerodynamics, and the outside environment. Since the 1970's, NASA flight research has become more comprehensive, with flights involving everything form Space Shuttles to ultralights. NASA now flies not only the fastest airplanes, but some of the slowest. Flying machines continue to evolve with new wing designs, propulsion systems, and flight controls. As always, a look at today's experimental research aircraft is a preview of the future.

  17. Automatic aircraft recognition

    NASA Astrophysics Data System (ADS)

    Hmam, Hatem; Kim, Jijoong

    2002-08-01

    Automatic aircraft recognition is very complex because of clutter, shadows, clouds, self-occlusion and degraded imaging conditions. This paper presents an aircraft recognition system, which assumes from the start that the image is possibly degraded, and implements a number of strategies to overcome edge fragmentation and distortion. The current vision system employs a bottom up approach, where recognition begins by locating image primitives (e.g., lines and corners), which are then combined in an incremental fashion into larger sets of line groupings using knowledge about aircraft, as viewed from a generic viewpoint. Knowledge about aircraft is represented in the form of whole/part shape description and the connectedness property, and is embedded in production rules, which primarily aim at finding instances of the aircraft parts in the image and checking the connectedness property between the parts. Once a match is found, a confidence score is assigned and as evidence in support of an aircraft interpretation is accumulated, the score is increased proportionally. Finally a selection of the resulting image interpretations with the highest scores, is subjected to competition tests, and only non-ambiguous interpretations are allowed to survive. Experimental results demonstrating the effectiveness of the current recognition system are given.

  18. Sealed substrate carrier for electroplating

    DOEpatents

    Ganti, Kalyana Bhargava [Fremont, CA

    2012-07-17

    One embodiment relates to a substrate carrier for use in electroplating a plurality of substrates. The substrate carrier includes a non-conductive carrier body on which the substrates are held, and conductive lines are embedded within the carrier body. A conductive bus bar is embedded into a top side of the carrier body and is conductively coupled to the conductive lines. A thermoplastic overmold covers a portion of the bus bar, and there is a plastic-to-plastic bond between the thermoplastic overmold and the non-conductive carrier body. Other embodiments, aspects and features are also disclosed.

  19. Multiple-Purpose Subsonic Naval Aircraft (MPSNA): Multiple Application Propfan Study (MAPS)

    NASA Technical Reports Server (NTRS)

    Engelbeck, R. M.; Havey, C. T.; Klamka, A.; Mcneil, C. L.; Paige, M. A.

    1986-01-01

    Study requirements, assumptions and guidelines were identified regarding carrier suitability, aircraft missions, technology availability, and propulsion considerations. Conceptual designs were executed for two missions, a full multimission aircraft and a minimum mission aircraft using three different propulsion systems, the UnDucted Fan (UDF), the Propfan and an advanced Turbofan. Detailed aircraft optimization was completed on those configurations yielding gross weight performance and carrier spot factors. Propfan STOVL conceptual designs were exercised also to show the effects of STOVL on gross weight, spot factor and cost. An advanced technology research plan was generated to identify additional investigation opportunities from an airframe contractors standpoint. Life cycle cost analysis was accomplished yielding a comparison of the UDF and propfan configurations against each other as well as against a turbofan with equivalent state of the art turbo-machinery.

  20. Carrier Battle Group (CVBG) Homeporting in the Puget Sound Area, Washington State. Volume 1. Chapters 1-12.

    DTIC Science & Technology

    1986-11-01

    0.005 Naphthalene ɘ.005 Acenaphthene ɘ.005 Fluorene ɘ.005 V Fluoranthene ɘ.005 Phenanthrene ɘ.005 - Pyrene ɘ.005 Benzo (B) Fluoranthene ɘ.005...sediment erosion concerns and limit vegetation root contact with the contaminated sediment layer. A low dike structure must be constructed to contain...that are comprised principally of bacteria, diatoms, algae, and their exudates , develop on ship hulls coated with OT paint and could affect the nature

  1. 150 Passenger Commercial Aircraft

    NASA Technical Reports Server (NTRS)

    Bucovsky, Adrian; Romli, Fairuz I.; Rupp, Jessica

    2002-01-01

    It has been projected that the need for a short-range mid-sized, aircraft is increasing. The future strategy to decrease long-haul flights will increase the demand for short-haul flights. Since passengers prefer to meet their destinations quickly, airlines will increase the frequency of flights, which will reduce the passenger load on the aircraft. If a point-to-point flight is not possible, passengers will prefer only a one-stop short connecting flight to their final destination. A 150-passenger aircraft is an ideal vehicle for these situations. It is mid-sized aircraft and has a range of 3000 nautical miles. This type of aircraft would market U.S. domestic flights or inter-European flight routes. The objective of the design of the 150-passenger aircraft is to minimize fuel consumption. The configuration of the aircraft must be optimized. This aircraft must meet CO2 and NOx emissions standards with minimal acquisition price and operating costs. This report contains all the work that has been performed for the completion of the design of a 150 passenger commercial aircraft. The methodology used is the Technology Identification, Evaluation, and Selection (TIES) developed at Georgia Tech Aerospace Systems Design laboratory (ASDL). This is an eight-step conceptual design process to evaluate the probability of meeting the design constraints. This methodology also allows for the evaluation of new technologies to be implemented into the design. The TIES process begins with defining the problem with a need established and a market targeted. With the customer requirements set and the target values established, a baseline concept is created. Next, the design space is explored to determine the feasibility and viability of the baseline aircraft configuration. If the design is neither feasible nor viable, new technologies can be implemented to open up the feasible design space and allow for a plausible solution. After the new technologies are identified, they must be evaluated

  2. A Micro-Machined Gyroscope for Rotating Aircraft

    PubMed Central

    Yan, Qingwen; Zhang, Fuxue; Zhang, Wei

    2012-01-01

    In this paper we present recent work on the design, fabrication by silicon micromachining, and packaging of a new gyroscope for stabilizing the autopilot of rotating aircraft. It operates based on oscillation of the silicon pendulum between two torsion girders for detecting the Coriolis force. The oscillation of the pendulum is initiated by the rolling and deflecting motion of the rotating carrier. Therefore, the frequency and amplitude of the oscillation are proportional to the rolling frequency and deflecting angular rate of the rotating carrier, and are measured by the sensing electrodes. A modulated pulse with constant amplitude and unequal width is obtained by a linearizing process of the gyroscope output signal and used to control the deflection of the rotating aircraft. Experimental results show that the gyroscope has a resolution of 0.008 °/s and a bias of 56.18 °/h. PMID:23012572

  3. A micro-machined gyroscope for rotating aircraft.

    PubMed

    Yan, Qingwen; Zhang, Fuxue; Zhang, Wei

    2012-01-01

    In this paper we present recent work on the design, fabrication by silicon micromachining, and packaging of a new gyroscope for stabilizing the autopilot of rotating aircraft. It operates based on oscillation of the silicon pendulum between two torsion girders for detecting the Coriolis force. The oscillation of the pendulum is initiated by the rolling and deflecting motion of the rotating carrier. Therefore, the frequency and amplitude of the oscillation are proportional to the rolling frequency and deflecting angular rate of the rotating carrier, and are measured by the sensing electrodes. A modulated pulse with constant amplitude and unequal width is obtained by a linearizing process of the gyroscope output signal and used to control the deflection of the rotating aircraft. Experimental results show that the gyroscope has a resolution of 0.008 °/s and a bias of 56.18 °/h.

  4. Census of U.S. Civil Aircraft. Calendar Year 1981.

    DTIC Science & Technology

    1981-12-31

    61 1 0 1 1 8-8MG 1 61 1 0 1 1 ROTOR REC ENGINE 61 0 4 4 TOTAL 0 4 4 BOEING V.-COLUMBIA HELICOPTERS 107-11 20 63 2 0 2 2 CH -21C 21 61 1 0 1 1 107-11 20...11NFACTURER AIR GENERAL TOTAL MODEL PL A/E N/E CARRIER AVIATION AIRCRAFT PITCAIRN ROTOR REC ENGINE 61 0 2 2 TOTAL 0 2 2 ROSINSON HELICOPTER COMPANY R22 2 61...MANUFACTURER AIR GENERAL TOTAL MODEL PL A/E N/E CARRIER AVIATION AIRCRAFT CH 2 41 1 0 1 1 CH -I 2 41 1 0 1 1 CHALLENGE 2 41 1 0 1 1 CHALLIS CHAFFINCH 1

  5. 78 FR 50050 - Record of Decision for the Construction and Operation of an Infantry Platoon Battle Course at...

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-08-16

    ... Department of the Army Record of Decision for the Construction and Operation of an Infantry Platoon Battle... decision to construct and operate a new Infantry Platoon Battle Course (IPBC) and associated infrastructure...). ] SUPPLEMENTARY INFORMATION: The IPBC will be used to train and test infantry platoons and other units on...

  6. Institute on Outdoor Education for the Handicapped. (Battle Creek Outdoor Education Center, Clear Lake, Dowling, Michigan, June 1969).

    ERIC Educational Resources Information Center

    Battle Creek Public Schools, MI.

    In early June 1969, 55 special education and physical education teachers and experts in outdoor education met for a week at the Battle Creek Public Schools' outdoor education center, Clear Lake Camp (Michigan). The participants shared in the camping activities of children from Battle Creek classes for the physically and mentally handicapped, deaf,…

  7. Agile battle management efficiency for command, control, communications, computers and intelligence (C4I)

    NASA Astrophysics Data System (ADS)

    Blasch, Erik; Bélanger, Micheline

    2016-05-01

    Various operations such as civil-military co-operation (CIMIC) affairs require orchestration of communications, assets, and actors. A key component includes technology advancements to enable coordination among people and machines the ability to know where things are, who to coordinate with, and open and consistent lines of communication. In this paper, we explore concepts of battle management (BM) to support high-tempo emergency response scenarios such as a disaster action response team (DART). Three concepts highlighted of agile battle management (ABM) include source orchestration (e.g., sensors and domains), battle management language (BML) development (e.g., software and ontologies), and command and control (C2) coordination (e.g., people and visualization); which require correlation and de-confliction. These concepts of ABM support the physical, information, and cognitive domains for efficient command, control, communications, and information (C3I) to synchronize data and people for efficient and effective operations.

  8. Yarn carrier with clutch

    NASA Technical Reports Server (NTRS)

    Doyne, Richard A. (Inventor); Benson, Rio H. (Inventor); El-Shiekh, Aly (Inventor)

    1994-01-01

    A yarn carrier apparatus particularly suited for use in braiding machinery or the like due to its capability of continuous yarn feeding and retraction of long lengths of yarn. The yarn carrier apparatus comprises a yarn supply spool which is rotatably mounted within the housing, a spring motor also mounted within the housing and operatively connected to the yarn supply spool through a mechanical transmission assembly which is adapted to multiply rotational movement between the first element of the gear assembly operatively connected to the spring motor and the final element of the gear assembly operatively connected to the yarn supply spool. The spring motor is adapted to tension the yarn during both feeding and retraction thereof, and it is further adapted to periodically rotatably slip within the housing and partially unwind so as to allow for continuous withdrawal of a long length of yarn without the spring motor becoming fully wound and preventing further yarn retraction.

  9. Hydrogen powered aircraft : The future of air transport

    NASA Astrophysics Data System (ADS)

    Khandelwal, Bhupendra; Karakurt, Adam; Sekaran, Paulas R.; Sethi, Vishal; Singh, Riti

    2013-07-01

    This paper investigates properties and traits of hydrogen with regard to environmental concerns and viability in near future applications. Hydrogen is the most likely energy carrier for the future of aviation, a fuel that has the potential of zero emissions. With investigation into the history of hydrogen, this study establishes issues and concerns made apparent when regarding the fuel in aero applications. Various strategies are analyzed in order to evaluate hydrogen's feasibility which includes production, storage, engine configurations and aircraft configurations.

  10. Current and future developments in civil aircraft non-destructive evaluation from an operator's point of view

    NASA Technical Reports Server (NTRS)

    Register, Jeff

    1992-01-01

    In June, 1988, the first International Conference on aging aircraft was held to address nondestructive tests (NDT) of aging aircraft and other issues. From this meeting, a research program was initiated and funded by the FAA. As a result of this program, a lot of work has been done to study current NDT practices in the aviation industry and secondly, to research and develop new NDT methods to improve the reliability and efficiency of in-service inspection of aircraft structures and powerplants. The following is an overview of the current and future developments in civil aircraft NDT, as viewed by an air carrier and the concerns for NDT in the future.

  11. High altitude reconnaissance aircraft

    NASA Technical Reports Server (NTRS)

    Yazdo, Renee Anna; Moller, David

    1990-01-01

    At the equator the ozone layer ranges from 65,000 to 130,000 plus feet, which is beyond the capabilities of the ER-2, NASA's current high altitude reconnaissance aircraft. The Universities Space Research Association, in cooperation with NASA, is sponsoring an undergraduate program which is geared to designing an aircraft that can study the ozone layer at the equator. This aircraft must be able to cruise at 130,000 feet for six hours at Mach 0.7, while carrying 3,000 lbs. of payload. In addition, the aircraft must have a minimum range of 6,000 miles. In consideration of the novel nature of this project, the pilot must be able to take control in the event of unforeseen difficulties. Three aircraft configurations were determined to be the most suitable - a joined-wing, a biplane, and a twin-boom conventional airplane. The performance of each configuration was analyzed to investigate the feasibility of the project.

  12. Identification of Aircraft Hazards

    SciTech Connect

    K. Ashley

    2006-12-08

    Aircraft hazards were determined to be potentially applicable to a repository at Yucca Mountain in ''Monitored Geological Repository External Events Hazards Screening Analysis'' (BSC 2005 [DIRS 174235], Section 6.4.1). That determination was conservatively based upon limited knowledge of flight data in the area of concern and upon crash data for aircraft of the type flying near Yucca Mountain. The purpose of this report is to identify specific aircraft hazards that may be applicable to a monitored geologic repository (MGR) at Yucca Mountain, using NUREG-0800, ''Standard Review Plan for the Review of Safety Analysis Reports for Nuclear Power Plants'' (NRC 1987 [DIRS 103124], Section 3.5.1.6), as guidance for the inclusion or exclusion of identified aircraft hazards. The intended use of this report is to provide inputs for further screening and analysis of identified aircraft hazards based upon the criteria that apply to Category 1 and Category 2 event sequence analyses as defined in 10 CFR 63.2 [DIRS 176544] (Section 4). The scope of this report includes the evaluation of military, private, and commercial use of airspace in the 100-mile regional setting of the repository at Yucca Mountain with the potential for reducing the regional setting to a more manageable size after consideration of applicable screening criteria (Section 7).

  13. IDENTIFICATION OF AIRCRAFT HAZARDS

    SciTech Connect

    K.L. Ashley

    2005-03-23

    Aircraft hazards were determined to be potentially applicable to a repository at Yucca Mountain in the ''Monitored Geological Repository External Events Hazards Screening Analysis'' (BSC 2004, Section 6.4.1). That determination was conservatively based on limited knowledge of flight data in the area of concern and on crash data for aircraft of the type flying near Yucca Mountain. The purpose of this report is to identify specific aircraft hazards that may be applicable to a Monitored Geologic Repository (MGR) at Yucca Mountain using NUREG-0800, ''Standard Review Plan for the Review of Safety Analysis Reports for Nuclear Power Plants'' (NRC 1987, Section 3.5.1.6), as guidance for the inclusion or exclusion of identified aircraft hazards. NUREG-0800 is being used here as a reference because some of the same considerations apply. The intended use of this report is to provide inputs for further screening and analysis of the identified aircraft hazards based on the criteria that apply to Category 1 and 2 event sequence analyses as defined in 10 CFR 63.2 (see Section 4). The scope of this technical report includes the evaluation of military, private, and commercial use of airspace in the 100-mile regional setting of the MGR at Yucca Mountain with the potential for reducing the regional setting to a more manageable size after consideration of applicable screening criteria (see Section 7).

  14. Aircraft noise synthesis system

    NASA Astrophysics Data System (ADS)

    McCurdy, David A.; Grandle, Robert E.

    1987-02-01

    A second-generation Aircraft Noise Synthesis System has been developed to provide test stimuli for studies of community annoyance to aircraft flyover noise. The computer-based system generates realistic, time-varying, audio simulations of aircraft flyover noise at a specified observer location on the ground. The synthesis takes into account the time-varying aircraft position relative to the observer; specified reference spectra consisting of broadband, narrowband, and pure-tone components; directivity patterns; Doppler shift; atmospheric effects; and ground effects. These parameters can be specified and controlled in such a way as to generate stimuli in which certain noise characteristics, such as duration or tonal content, are independently varied, while the remaining characteristics, such as broadband content, are held constant. The system can also generate simulations of the predicted noise characteristics of future aircraft. A description of the synthesis system and a discussion of the algorithms and methods used to generate the simulations are provided. An appendix describing the input data and providing user instructions is also included.

  15. Aircraft noise synthesis system

    NASA Technical Reports Server (NTRS)

    Mccurdy, David A.; Grandle, Robert E.

    1987-01-01

    A second-generation Aircraft Noise Synthesis System has been developed to provide test stimuli for studies of community annoyance to aircraft flyover noise. The computer-based system generates realistic, time-varying, audio simulations of aircraft flyover noise at a specified observer location on the ground. The synthesis takes into account the time-varying aircraft position relative to the observer; specified reference spectra consisting of broadband, narrowband, and pure-tone components; directivity patterns; Doppler shift; atmospheric effects; and ground effects. These parameters can be specified and controlled in such a way as to generate stimuli in which certain noise characteristics, such as duration or tonal content, are independently varied, while the remaining characteristics, such as broadband content, are held constant. The system can also generate simulations of the predicted noise characteristics of future aircraft. A description of the synthesis system and a discussion of the algorithms and methods used to generate the simulations are provided. An appendix describing the input data and providing user instructions is also included.

  16. Aircraft Operations Classification System

    NASA Technical Reports Server (NTRS)

    Harlow, Charles; Zhu, Weihong

    2001-01-01

    Accurate data is important in the aviation planning process. In this project we consider systems for measuring aircraft activity at airports. This would include determining the type of aircraft such as jet, helicopter, single engine, and multiengine propeller. Some of the issues involved in deploying technologies for monitoring aircraft operations are cost, reliability, and accuracy. In addition, the system must be field portable and acceptable at airports. A comparison of technologies was conducted and it was decided that an aircraft monitoring system should be based upon acoustic technology. A multimedia relational database was established for the study. The information contained in the database consists of airport information, runway information, acoustic records, photographic records, a description of the event (takeoff, landing), aircraft type, and environmental information. We extracted features from the time signal and the frequency content of the signal. A multi-layer feed-forward neural network was chosen as the classifier. Training and testing results were obtained. We were able to obtain classification results of over 90 percent for training and testing for takeoff events.

  17. Aircraft Icing Weather Data Reporting and Dissemination System

    NASA Technical Reports Server (NTRS)

    Bass, Ellen J.; Minsk, Brian; Lindholm, Tenny; Politovich, Marcia; Reehorst, Andrew (Technical Monitor)

    2002-01-01

    The long-term operational concept of this research is to develop an onboard aircraft system that assesses and reports atmospheric icing conditions automatically and in a timely manner in order to improve aviation safety and the efficiency of aircraft operations via improved real-time and forecast weather products. The idea is to use current measurement capabilities on aircraft equipped with icing sensors and in-flight data communication technologies as a reporting source. Without requiring expensive avionics upgrades, aircraft data must be processed and available for downlink. Ideally, the data from multiple aircraft can then be integrated (along with other real-time and modeled data) on the ground such that aviation-centered icing hazard metrics for volumes of airspace can be assessed. As the effect of icing on different aircraft types can vary, the information should be displayed in meaningful ways such that multiple types of users can understand the information. That is, information must be presented in a manner to allow users to understand the icing conditions with respect to individual concerns and aircraft capabilities. This research provides progress toward this operational concept by: identifying an aircraft platform capable of digitally capturing, processing, and downlinking icing data; identifying the required in situ icing data processing; investigating the requirements for routing the icing data for use by weather products; developing an icing case study in order to gain insight into major air carrier needs; developing and prototyping icing display concepts based on the National Center for Atmospheric Research's existing diagnostic and forecast experimental icing products; and conducting a usability study for the prototyped icing display concepts.

  18. BATTLE (Biomarker-based Approach of Targeted Therapy for Lung Cancer Elimination)

    DTIC Science & Technology

    2010-04-01

    asma concentration (pg/mL) and the ex pression levels of bas ic FGF (bFGF). We found a 1.5 fol d increase in the levels of the circulating cytokine...outcome measures such as progression-free survival (PFS). The final step will be to v alidate the pl asma predictive signature derived from BATTLE...PFS). The final step will be to v alidate the pl asma predictive signature derived from BATTLE with other randomized clinical studies. These

  19. Ground Forces Battle Casualty Rate Patterns: Uses in Casualty Estimation and Simulation Evaluation.

    DTIC Science & Technology

    2007-11-02

    disintegrated front is marked by both the collapse of the defender force with a heavy-to-near-total force battle casualty rate and a low-to- negligible battle...totality of collapsing Defender cohesion — which long term air-inflicted attrition may certainly help prepare, but which is neither necessarily (much less...H ■ H u. O IU > tt 3 <J Of O > 5 tt 3 vt CD 6 u«mJ^«*JOVJ^i«d Warn MS 󈧧 •23 2« ^ Median WTC (Unrfscottnted) 687 -L

  20. Aircraft icing instrumentation: Unfilled needs. [rotary wing aircraft

    NASA Technical Reports Server (NTRS)

    Kitchens, P. F.

    1980-01-01

    A list of icing instrumentation requirements are presented. Because of the Army's helicopter orientation, many of the suggestions are specific to rotary wing aircraft; however, some of the instrumentation are also suitable for general aviation aircraft.

  1. Commercial aircraft noise

    NASA Astrophysics Data System (ADS)

    Smith, M. J.

    The history of aircraft noise control development is traced with an eye to forecasting the future. Noise control became imperative with the advent of the first generation of commercial jet aircraft, which were extremely loud. The steady increases in the size of turbofans have nearly matched the progress in noise reduction capabilities in recent years. Only 5 dB of reduction in fleet noise has been achieved since early standards were met. Current engine design is concentrated on increasing fuel efficiency rather than lowering noise emissions. Further difficulties exist because of continued flights with older aircraft. Gains in noise reduction have been made mainly by decreasing exhaust velocities from 600-700 m/sec to 300-400 m/sec. New techniques being explored comprise mixing the core and bypass flows, interaction tone control, reduction of broadband sources, development of acoustic liner technology and alterations in the number of fan blades and stage spacing.

  2. Transport aircraft accident dynamics

    NASA Technical Reports Server (NTRS)

    Cominsky, A.

    1982-01-01

    A study was carried out of 112 impact survivable jet transport aircraft accidents (world wide) of 27,700 kg (60,000 lb.) aircraft and up extending over the last 20 years. This study centered on the effect of impact and the follow-on events on aircraft structures and was confined to the approach, landing and takeoff segments of the flight. The significant characteristics, frequency of occurrence and the effect on the occupants of the above data base were studied and categorized with a view to establishing typical impact scenarios for use as a basis of verifying the effectiveness of potential safety concepts. Studies were also carried out of related subjects such as: (1) assessment of advanced materials; (2) human tolerance to impact; (3) merit functions for safety concepts; and (4) impact analysis and test methods.

  3. Alternative aircraft fuels technology

    NASA Technical Reports Server (NTRS)

    Grobman, J.

    1976-01-01

    NASA is studying the characteristics of future aircraft fuels produced from either petroleum or nonpetroleum sources such as oil shale or coal. These future hydrocarbon based fuels may have chemical and physical properties that are different from present aviation turbine fuels. This research is aimed at determining what those characteristics may be, how present aircraft and engine components and materials would be affected by fuel specification changes, and what changes in both aircraft and engine design would be required to utilize these future fuels without sacrificing performance, reliability, or safety. This fuels technology program was organized to include both in-house and contract research on the synthesis and characterization of fuels, component evaluations of combustors, turbines, and fuel systems, and, eventually, full-scale engine demonstrations. A review of the various elements of the program and significant results obtained so far are presented.

  4. Aircraft Design Analysis

    NASA Technical Reports Server (NTRS)

    1979-01-01

    The helicopter pictured is the twin-turbine S-76, produced by Sikorsky Aircraft division of United Technologies, Stratford, Connecticut. It is the first transport helicopter ever dey n e d purely as a commercial vehicle rather than an adaptation of a military design. Being built in large numbers for customers in 16 countries, the S-76 is intended for offshore oil rig support, executive transportation and general utility service. The craft carries 12 passengers plus a crew of two and has a range of more than 450 miles-yet it weighs less than 10,000 pounds. Significant weight reduction was achieved by use of composite materials, which are generally lighter but stronger than conventional aircraft materials. NASA composite technology played a part in development of the S-76. Under contract with NASA's Langley Research Center, Sikorsky Aircraft designed and flight-tested a helicopter airframe of advanced composite materials.

  5. Air pollution from aircraft operations at San Jose Municipal Airport, California

    NASA Technical Reports Server (NTRS)

    Schairer, E. T.

    1978-01-01

    The amount of air pollution discharged by arriving and departing aircraft at the San Jose Municipal Airport was estimated. These estimates were made for each one hour interval of a summer weekday in 1977. The contributions of both general aviation (personal and business aircraft) and certified air carriers (scheduled airliners) were considered. The locations at which the pollutants were discharged were estimated by approximating the flight paths of arriving and departing aircraft. Three types of pollutants were considered: carbon monoxide, hydrocarbons, and oxides of nitrogen.

  6. Maintainable substrate carrier for electroplating

    DOEpatents

    Chen, Chen-An; Abas, Emmanuel Chua; Divino, Edmundo Anida; Ermita, Jake Randal G.; Capulong, Jose Francisco S.; Castillo, Arnold Villamor; Ma, Diana Xiaobing

    2016-08-02

    One embodiment relates to a substrate carrier for use in electroplating a plurality of substrates. The carrier includes a non-conductive carrier body on which the substrates are placed and conductive lines embedded within the carrier body. A plurality of conductive clip attachment parts are attached in a permanent manner to the conductive lines embedded within the carrier body. A plurality of contact clips are attached in a removable manner to the clip attachment parts. The contact clips hold the substrates in place and conductively connecting the substrates with the conductive lines. Other embodiments, aspects and features are also disclosed.

  7. Maintainable substrate carrier for electroplating

    DOEpatents

    Chen, Chen-An [Milpitas, CA; Abas, Emmanuel Chua [Laguna, PH; Divino, Edmundo Anida [Cavite, PH; Ermita, Jake Randal G [Laguna, PH; Capulong, Jose Francisco S [Laguna, PH; Castillo, Arnold Villamor [Batangas, PH; Ma,; Xiaobing, Diana [Saratoga, CA

    2012-07-17

    One embodiment relates to a substrate carrier for use in electroplating a plurality of substrates. The carrier includes a non-conductive carrier body on which the substrates are placed and conductive lines embedded within the carrier body. A plurality of conductive clip attachment parts are attached in a permanent manner to the conductive lines embedded within the carrier body. A plurality of contact clips are attached in a removable manner to the clip attachment parts. The contact clips hold the substrates in place and conductively connecting the substrates with the conductive lines. Other embodiments, aspects and features are also disclosed.

  8. Pathfinder aircraft flight

    NASA Technical Reports Server (NTRS)

    1996-01-01

    The Pathfinder research aircraft's wing structure is clearly defined as it soars under a clear blue sky during a test flight from Dryden Flight Research Center, Edwards, California, in November of 1996. Pathfinder was a lightweight, solar-powered, remotely piloted flying wing aircraft used to demonstrate the use of solar power for long-duration, high-altitude flight. Its name denotes its mission as the 'Pathfinder' or first in a series of solar-powered aircraft that will be able to remain airborne for weeks or months on scientific sampling and imaging missions. Solar arrays covered most of the upper wing surface of the Pathfinder aircraft. These arrays provided up to 8,000 watts of power at high noon on a clear summer day. That power fed the aircraft's six electric motors as well as its avionics, communications, and other electrical systems. Pathfinder also had a backup battery system that could provide power for two to five hours, allowing for limited-duration flight after dark. Pathfinder flew at airspeeds of only 15 to 20 mph. Pitch control was maintained by using tiny elevators on the trailing edge of the wing while turns and yaw control were accomplished by slowing down or speeding up the motors on the outboard sections of the wing. On September 11, 1995, Pathfinder set a new altitude record for solar-powered aircraft of 50,567 feet above Edwards Air Force Base, California, on a 12-hour flight. On July 7, 1997, it set another, unofficial record of 71,500 feet at the Pacific Missile Range Facility, Kauai, Hawaii. In 1998, Pathfinder was modified into the longer-winged Pathfinder Plus configuration. (See the Pathfinder Plus photos and project description.)

  9. Optical communications for transport aircraft

    NASA Technical Reports Server (NTRS)

    Stengel, Robert

    1994-01-01

    Optical communications for transport aircraft are discussed. The problem involves: increasing demand for radio-frequency bands from an enlarging pool of users (aircraft, ground and sea vehicles, fleet operators, traffic control centers, and commercial radio and television); desirability of providing high-bandwidth dedicated communications to and from every aircraft in the National Airspace System; need to support communications, navigation, and surveillance for a growing number of aircraft; and improved meteorological observations by use of probe aircraft. The solution involves: optical signal transmission support very high data rates; optical transmission of signals between aircraft, orbiting satellites, and ground stations, where unobstructed line-of-sight is available; conventional radio transmissions of signals between aircraft and ground stations, where optical line-of-sight is unavailable; and radio priority given to aircraft in weather.

  10. Atmospheric Electricity - Aircraft Interaction

    DTIC Science & Technology

    1980-05-01

    flux may leak inside the aircraft through apertures such as windows , radomes. canopies, seams, and joints. Other fields may arise inside the aircraft...fields of other origins are considered. The third type of c-"pling involves electric fields passing directly through aper- tures, such as windows or...Transistors Microwave Diodes Low Power Transistors 0.001 0.01 0.1 1 10 100 0.01 0.1 1 10 100 Damage Constant. K Damage Constant. K Figure 29 - Ranges

  11. Aircraft Laminar Flow Control

    NASA Technical Reports Server (NTRS)

    Joslin, Ronald D.

    1998-01-01

    Aircraft laminar flow control (LFC) from the 1930's through the 1990's is reviewed and the current status of the technology is assessed. Examples are provided to demonstrate the benefits of LFC for subsonic and supersonic aircraft. Early studies related to the laminar boundary-layer flow physics, manufacturing tolerances for laminar flow, and insect-contamination avoidance are discussed. LFC concept studies in wind-tunnel and flight experiments are the major focus of the paper. LFC design tools are briefly outlined for completeness.

  12. Combat aircraft noise

    NASA Astrophysics Data System (ADS)

    Sgarbozza, M.; Depitre, A.

    1992-04-01

    A discussion of the characteristics and the noise levels of combat aircraft and of a transport aircraft in taking off and landing are presented. Some methods of noise reduction are discussed, including the following: operational anti-noise procedures; and concepts of future engines (silent post-combustion and variable cycle). Some measurement results concerning the noise generated in flight at great speeds and low altitude will also be examined. Finally, the protection of the environment of French air bases against noise will be described and the possibilities of regulation examined.

  13. Aircraft surface coatings

    NASA Technical Reports Server (NTRS)

    1982-01-01

    Liquid, spray on elastomeric polyurethanes are selected and investigated as best candidates for aircraft external protective coatings. Flight tests are conducted to measure drag effects of these coatings compared to paints and a bare metal surface. The durability of two elastometric polyurethanes are assessed in airline flight service evaluations. Laboratory tests are performed to determine corrosion protection properties, compatibility with aircraft thermal anti-icing systems, the effect of coating thickness on erosion durability, and the erosion characteristics of composite leading edges-bare and coated. A cost and benefits assessment is made to determine the economic value of various coating configurations to the airlines.

  14. Alternative aircraft fuels

    NASA Technical Reports Server (NTRS)

    Longwell, J. P.; Grobman, J. S.

    1977-01-01

    The efficient utilization of fossil fuels by future jet aircraft may necessitate the broadening of current aviation turbine fuel specifications. The most significant changes in specifications would be an increased aromatics content and a higher final boiling point in order to minimize refinery energy consumption and costs. These changes would increase the freezing point and might lower the thermal stability of the fuel, and could cause increased pollutant emissions, increased combustor liner temperatures, and poorer ignition characteristics. The effects that broadened specification fuels may have on present-day jet aircraft and engine components and the technology required to use fuels with broadened specifications are discussed.

  15. Aircraft Flutter Testing

    NASA Technical Reports Server (NTRS)

    1997-01-01

    Wilmer Reed gained international recognition for his innovative research, contributions and patented ideas relating to flutter and aeroelasticity of aerospace vehicles at Langley Research Center. In the early 1980's, Reed retired from Langley and joined the engineering staff of Dynamic Engineering Inc. While at DEI, Reed conceived and patented the DEI Flutter Exciter, now used world-wide in flight flutter testing of new or modified aircraft designs. When activated, the DEI Flutter Exciter alternately deflects the airstream upward and downward in a rapid manner, creating a force similar to that produced by an oscillating trailing edge flap. The DEI Flutter Exciter is readily adaptable to a variety of aircraft.

  16. Aircraft engines. II

    SciTech Connect

    Smith, M.G. Jr.

    1988-01-01

    An account is given of the design features and prospective performance gains of ultrahigh bypass subsonic propulsion configurations and various candidate supersonic commercial aircraft powerplants. The supersonic types, whose enhanced thermodynamic cycle efficiency is considered critical to the economic viability of a second-generation SST, are the variable-cycle engine, the variable stream control engine, the turbine-bypass engine, and the supersonic-throughflow fan. Also noted is the turboramjet concept, which will be applicable to hypersonic aircraft whose airframe structure materials can withstand the severe aerothermodynamic conditions of this flight regime.

  17. Aircraft engine pollution reduction

    NASA Technical Reports Server (NTRS)

    Rudey, R. A.

    1972-01-01

    The effect of engine operation on the types and levels of the major aircraft engine pollutants is described and the major factors governing the formation of these pollutants during the burning of hydrocarbon fuel are discussed. Methods which are being explored to reduce these pollutants are discussed and their application to several experimental research programs are pointed out. Results showing significant reductions in the levels of carbon monoxide, unburned hydrocarbons, and oxides of nitrogen obtained from experimental combustion research programs are presented and discussed to point out potential application to aircraft engines.

  18. Solar powered aircraft

    SciTech Connect

    Phillips, W.H.

    1983-11-15

    A cruciform wing structure for a solar powered aircraft is disclosed. Solar cells are mounted on horizontal wing surfaces. Wing surfaces with spanwise axis perpendicular to surfaces maintain these surfaces normal to the sun's rays by allowing aircraft to be flown in a controlled pattern at a large bank angle. The solar airplane may be of conventional design with respect to fuselage, propeller and tail, or may be constructed around a core and driven by propeller mechanisms attached near the tips of the airfoils.

  19. Economics of technological change - A joint model for the aircraft and airline industries

    NASA Technical Reports Server (NTRS)

    Kneafsey, J. T.; Taneja, N. K.

    1981-01-01

    The principal focus of this econometric model is on the process of technological change in the U.S. aircraft manufacturing and airline industries. The problem of predicting the rate of introduction of current technology aircraft into an airline's fleet during the period of research, development, and construction for new technology aircraft arises in planning aeronautical research investments. The approach in this model is a statistical one. It attempts to identify major factors that influence transport aircraft manufacturers and airlines, and to correlate them with the patterns of delivery of new aircraft to the domestic trunk carriers. The functional form of the model has been derived from several earlier econometric models on the economics of innovation, acquisition, and technological change.

  20. Rainfall extremes: Toward reconciliation after the battle of distributions

    PubMed Central

    Serinaldi, Francesco; Kilsby, Chris G

    2014-01-01

    results from the analysis of short time series. Citation: Serinaldi, F., and C. G. Kilsby (2014), Rainfall extremes: Toward reconciliation after the battle of distributions, Water Resour. Res., 50, 336–352, doi:10.1002/2013WR014211. PMID:24829512

  1. Aircraft Fuel Systems Career Ladder.

    DTIC Science & Technology

    1985-09-01

    type fittings remove and install fuel cells clean work areas inspect aircraft for safety pin installation purge tanks or cells using blow purge method...INSPECT AIRCRAFT FOR SAFETY PIN INSTALLATION 84 H254 PURGE TANKS OR CELLS USING BLOW PURGE METHOD 83 H227 CHECK AIRCRAFT FOR LIQUID OXYGEN (LOX...H243 INSPECT AIRCRAFT FOR SAFETY PIN INSTALLATION 52 M483 MIX SEALANTS BY HAND 48 K372 CONNECT OR DISCONNECT WIGGINS TYPE FITTINGS 48 H236 DISCONNECT

  2. Aircraft community noise impact studies

    NASA Technical Reports Server (NTRS)

    1977-01-01

    The objectives of the study are to: (1) conduct a program to determine the community noise impact of advanced technology engines when installed in a supersonic aircraft, (2) determine the potential reduction of community noise by flight operational techniques for the study aircraft, (3) estimate the community noise impact of the study aircraft powered by suppressed turbojet engines and by advanced duct heating turbofan engines, and (4) compare the impact of the two supersonic designs with that of conventional commercial DC-8 aircraft.

  3. An Evaluation of Aircraft Emissions Inventory Methodology by Comparisons with Reported Airline Data

    NASA Technical Reports Server (NTRS)

    Daggett, D. L.; Sutkus, D. J.; DuBois, D. P.; Baughcum, S. L.

    1999-01-01

    This report provides results of work done to evaluate the calculation methodology used in generating aircraft emissions inventories. Results from the inventory calculation methodology are compared to actual fuel consumption data. Results are also presented that show the sensitivity of calculated emissions to aircraft payload factors. Comparisons of departures made, ground track miles flown and total fuel consumed by selected air carriers were made between U.S. Dept. of Transportation (DOT) Form 41 data reported for 1992 and results of simplified aircraft emissions inventory calculations. These comparisons provide an indication of the magnitude of error that may be present in aircraft emissions inventories. To determine some of the factors responsible for the errors quantified in the DOT Form 41 analysis, a comparative study of in-flight fuel flow data for a specific operator's 747-400 fleet was conducted. Fuel consumption differences between the studied aircraft and the inventory calculation results may be attributable to several factors. Among these are longer flight times, greater actual aircraft weight and performance deterioration effects for the in-service aircraft. Results of a parametric study on the variation in fuel use and NOx emissions as a function of aircraft payload for different aircraft types are also presented.

  4. Multimission Aircraft Design Study, Payload

    DTIC Science & Technology

    2003-03-01

    number MC2A Multisensor Command and Control Aircraft MC2A-X Multisensor Command and Control Aircraft Experiment MIDS Multifunctional Information and...reconnaissance (ISR) fleet. The MMA is alternately designated as the Multisensor Command and Control Aircraft (MC2A) as indicated in this text. Figure

  5. Bibliography for aircraft parameter estimation

    NASA Technical Reports Server (NTRS)

    Iliff, Kenneth W.; Maine, Richard E.

    1986-01-01

    An extensive bibliography in the field of aircraft parameter estimation has been compiled. This list contains definitive works related to most aircraft parameter estimation approaches. Theoretical studies as well as practical applications are included. Many of these publications are pertinent to subjects peripherally related to parameter estimation, such as aircraft maneuver design or instrumentation considerations.

  6. 77 FR 14461 - Approval of Noise Compatibility Program for W.K. Airport, Battle Creek, MI

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-03-09

    ... Federal Aviation Administration Approval of Noise Compatibility Program for W.K. Airport, Battle Creek, MI... requirements. On February 16, 2012, the FAA approved the W.K. Kellogg Airport noise compatibility program. All... effective date of the FAA's approval of the Noise Compatibility Program for W.K. Kellogg Airport is...

  7. Is There a requirement for Heavy Mortars in Airland Battle Future (ALB- F)

    DTIC Science & Technology

    1990-03-09

    ineffective the heavy mortars are in a fast -moving battle fought at the NTC, if they managed to get into the fight at all. Reports indicate that the heavy...Army Operational Concept," Final Draft, U.S. Army Combined Arms Center, Fort Leavenworth, KS. 10 January 1989. Forword . 2. Ibid. pp. D1-D3. 3. Ibid

  8. NOVA: Spring 2003 Teacher's Guide. Battle of the X-Planes.

    ERIC Educational Resources Information Center

    WGBH Educational Foundation, Boston, MA.

    This teacher's guide contains supplemental activities to go along with the NOVA television program on PBS. Activities include: (1) "Last Flight of Bomber 31"; (2) "Ancient Creature of the Deep"; (3) "Battle of the X-Planes"; (4) "Mountain of Ice"; (5) "Lost Treasures of Tibet"; and (6)…

  9. The Battle of Shiloh: A Study in Leadership and a Terrain Walk

    ERIC Educational Resources Information Center

    Day, James S.; Truss, Ruth S.

    2007-01-01

    Students from the University of Montevallo, Alabama's public liberal arts university, re-created the Battle of Shiloh (April 6-7, 1862) approximately twenty miles north of Corinth, Mississippi. For ten weeks in a classroom environment, nineteen students studied strategy, operations, and tactics that affected events nearly 143 years prior. Then,…

  10. 12. PWD Drawing 814S2 (1944), 'Facilities For Cleaning of Battle ...

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

    12. PWD Drawing 814-S-2 (1944), 'Facilities For Cleaning of Battle Damaged Machinery, Foundation Plan and Details' (note: original drawing of poor quality) - Mare Island Naval Shipyard, Chemical Cleaning Facility, North of Fourteenth Street, between California & Railroad Avenue, Vallejo, Solano County, CA

  11. 13. PWD Drawing 814S4 (1944), 'Facilities For Cleaning of Battle ...

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

    13. PWD Drawing 814-S-4 (1944), 'Facilities For Cleaning of Battle Damaged Machinery, Structural Framing' (note: original drawing of poor quality) - Mare Island Naval Shipyard, Chemical Cleaning Facility, North of Fourteenth Street, between California & Railroad Avenue, Vallejo, Solano County, CA

  12. Texas AandM Competes in EPAs Sixth Annual Energy Star Battle of the Buildings

    EPA Pesticide Factsheets

    DALLAS - (July 22, 2015) Today, the Environmental Protection Agency (EPA) launched the 2015 Energy Star Battle of the Buildings. Texas A&M University is among 125 teams and 6,500 buildings nationwide competing head-to-head to reduce their energy

  13. Nearly 400 Northwest Buildings Compete in EPAs Battle of the Buildings

    EPA Pesticide Factsheets

    (Seattle - July 28, 2015) Last week the U.S. Environmental Protection Agency launched the 2015 Energy Star Battle of the Buildings and nearly 400 competitors in the Pacific Northwest and Alaska have joined in to reduce their energy and water use. In suppor

  14. On a three-parameter quantum battle of the sexes cellular automaton

    NASA Astrophysics Data System (ADS)

    Alonso-Sanz, Ramón

    2013-05-01

    The dynamics of a spatial quantum formulation of the iterated battle of the sexes game is studied in this work. The game is played in the cellular automata manner, i.e., with local and synchronous interaction. The effect of spatial structure is assessed when allowing the players to adopt quantum strategies that are no restricted to any particular subset of the possible strategies.

  15. Woodville, AL Team Recognized as EPA's 2015 Energy Star Battle of the Buildings Competition Top Awardee

    EPA Pesticide Factsheets

    Release Date: May 5, 2015 ATLANTA - Today, the U.S. Environmental Protection Agency (EPA) announced a Woodville, Ala. building team, Going Blue for Woodville, as the top award winner in the Agency's fifth-annual Energy Star Battle of the Bui

  16. Career Education Survey K-12. Battle Creek Public Schools, 1980-81.

    ERIC Educational Resources Information Center

    Battle Creek Public Schools, MI.

    This survey describes career education activities for grades K-12 and for reading and special education classes in the Battle Creek, Michigan Public Schools. Activities, purposes and resources of career education are given individually for kindergarten through grade six; junior and senior high school activities are listed in two other sections.…

  17. Getting There is Only Half the Battle: Improving Forcible Entry Capability for Joint Force 2020

    DTIC Science & Technology

    2013-04-01

    3 . DATES COVERED 23 July 2012 thru 14 June 2013 4. TITLE AND SUBTITLE Getting There Is Only Half The Battle: Improving Forcible Entry Capability...16  CHAPTER 3 : STRATEGIC REQUIREMENTS FOR FORCIBLE ENTRY ..................24...33  Vignette 3 : Deter and Defeat Aggression .............................................................. 37  Vignette

  18. Japan’s Battle of Okinawa, April-June 1945 (Leavenworth Papers, Number 18)

    DTIC Science & Technology

    1990-05-01

    English, the Battle of Okinawa is analyzed from the vantage point of the Japanese defenders. Basing his work on extensive research in Japanese ...Landings ....................................... Planning the Japanese 12 April Offensive ..................... The American Advance...The Japanese 12 April Offensive ............................... N ight Problem s ................................................ M

  19. Our Public Intellectual: Matthew Battles--Houghton Library, Harvard University, Cambridge, MA

    ERIC Educational Resources Information Center

    Library Journal, 2004

    2004-01-01

    Many people take for granted the tools of the librarian's trade: typography, books, even the idea of a library. But when Matthew Battles looks at these things, he sees responses that evolved to meet human needs and wants to know more. What purposes were these tools put to and what do they tell people about the culture that produced them? What does…

  20. Isostatic Gravity Map of the Battle Mountain 30 x 60 Minute Quadrangle, North Central Nevada

    USGS Publications Warehouse

    Ponce, D.A.; Morin, R.L.

    2000-01-01

    Introduction Gravity investigations of the Battle Mountain 30 x 60 minute quadrangle were begun as part of an interagency effort by the U.S. Geological Survey (USGS) and the Bureau of Land Management to help characterize the geology, mineral resources, hydrology, and ecology of the Humboldt River Basin in north-central Nevada. The Battle Mountain quadrangle is located between 40?30' and 41?N. lat. and 116? and 117?W. long. This isostatic gravity map of the Battle Mountain quadrangle was prepared from data from about 1,180 gravity stations. Most of these data are publicly available on a CD-ROM of gravity data of Nevada (Ponce, 1997) and in a published report (Jewel and others, 1997). Data from about 780 gravity stations were collected by the U.S. Geological Survey since 1996; data from about 245 of these are unpublished (USGS, unpub. data, 1998). Data collected from the 400 gravity stations prior to 1996 are a subset of a gravity data compilation of the Winnemucca 1:250,000-scale quadrangle described in great detail by Wagini (1985) and Sikora (1991). This detailed information includes gravity meters used, dates of collection, sources, descriptions of base stations, plots of data, and a list of principal facts. A digital version of the entire data set for the Battle Mountain quadrangle is available on the World Wide Web at: http://wrgis.wr.usgs.gov/docs/gump/gump.html

  1. n-person Battle of sexes games—a simulation study

    NASA Astrophysics Data System (ADS)

    Zhao, Jijun; Szilagyi, Miklos N.; Szidarovszky, Ferenc

    2008-06-01

    n-person Battle of Sexes (BOS) games are examined by a special simulation study. Two types of agents are considered and there are three possible ways of making the agents’ initial decisions. The simulation study confirms the theoretical results on the existence and number of equilibria. We also investigate the effect of the model parameters on the limiting states of the system.

  2. Guerrilla War at UCLA: Political and Legal Dimensions of the Tenure Battle.

    ERIC Educational Resources Information Center

    Minami, Dale

    1990-01-01

    Shows how political campaigning and legal action won a three-year battle (beginning in 1986) for tenure by an Asian Pacific American professor, D. Nakanishi, at the University of California Los Angeles (UCLA). Describes the case's academic context, explains the legal alternatives, and analyzes the legal/political strategy adopted. (JB)

  3. Battling Obesity with Quality Elementary Physical Education: From Exposure to Competence

    ERIC Educational Resources Information Center

    Bott, Timothy S.; Mitchell, Murray

    2015-01-01

    Sedentary behaviors contribute to the obesity epidemic in this country and physical educators can play an important role in the battle to improve the quality of life of our citizens. Motor skill competency is a substantive factor in a person's decision to be active or not, and a quality physical education program can tip the balance in favor of…

  4. BATTLE: Biomarker-Based Approaches of Targeted Therapy for Lung Cancer Elimination

    DTIC Science & Technology

    2008-04-01

    of Targeted Therapy for Lung Cancer Elimination PRINCIPAL INVESTIGATOR: Waun Ki Hong, M.D...M.D. Anderson Cancer Center Houston, TX 77030 REPORT DATE: April...2008 4. TITLE AND SUBTITLE BATTLE: Biomarker-Based Approaches of Targeted Therapy for Lung Cancer 5a. CONTRACT NUMBER Elimination 5b. GRANT NUMBER

  5. A cellular automaton implementation of a quantum battle of the sexes game with imperfect information

    NASA Astrophysics Data System (ADS)

    Alonso-Sanz, Ramón

    2015-10-01

    The dynamics of a spatial quantum formulation of the iterated battle of the sexes game with imperfect information is studied in this work. The game is played with variable entangling in a cellular automata manner, i.e. with local and synchronous interaction. The effect of spatial structure is assessed in fair and unfair scenarios.

  6. Synthesis of Distributed Command and Control for the Outer Air Battle

    DTIC Science & Technology

    1988-07-01

    corresponding loci . 1984). This cost is computed for each input iask, x, and each decision strategy. The accuracy measure J is the expected value 3.3...Symposium on Large Scale Systems.: Theory and for the outer air battle, using a structured synthesis methodo - Application, Zurich, Switzerland

  7. Balancing Communities, Cultures, and Conflict: Lessons Learned From the East Ramapo School District Legal Battle

    ERIC Educational Resources Information Center

    Ober, Patrick; Decker, Janet R.

    2016-01-01

    This case illustrates why future school leaders must be prepared to handle complex legal and political issues that commonly arise in school districts today. We discuss a long-standing and unresolved legal battle between a Hasidic Jewish community and the public school district in East Ramapo, New York. In particular, we examine the difficulties…

  8. Racial Battle Fatigue for Latina/o Students: A Quantitative Perspective

    ERIC Educational Resources Information Center

    Franklin, Jeremy D.; Smith, William A.; Hung, Man

    2014-01-01

    Previous literature demonstrates that as a result of racial microaggressions and hostile campus racial climates, Latina/o students often state they experience psychological, physiological, and behavioral stress responses during and after racialized incidents on campuses. The purpose of this study is to quantitatively test the racial battle fatigue…

  9. Angels of Armageddon: The Royal Air Force in the Battle of Megiddo

    DTIC Science & Technology

    2007-06-15

    114  Pharaoh Necho II .........................................................................................................114  Saladin ... Saladin , and the Mamluke Sultan Qutuz (see appendix A). Yet of the many battles that were recorded to have been fought in the vicinity of Megiddo, there...and laid waste to the Temple.4 Israel and Judah never recovered from that fateful day on the plains of Megiddo. Saladin The twelfth century

  10. Aircraft to Medicine

    NASA Technical Reports Server (NTRS)

    1991-01-01

    This video discusses how the technology of computer modeling can improve the design and durability of artificial joints for human joint replacement surgery. Also, ultrasound, originally used to detect structural flaws in aircraft, can also be used to quickly assess the severity of a burn patient's injuries, thus aiding the healing process.

  11. Counterrotating aircraft propulsor blades

    NASA Technical Reports Server (NTRS)

    Nelson, Joey L. (Inventor); Elston, III, Sidney B. (Inventor); Tseng, Wu-Yang (Inventor); Hemsworth, Martin C. (Inventor)

    1993-01-01

    A propulsor blade for an aircraft engine includes an airfoil section formed in the shape of a scimitar. A metallic blade spar is interposed between opposed surfaces of the blade and is bonded to the surfaces to establish structural integrity of the blade. The metallic blade spar includes a root end allowing attachment of the blade to the engine.

  12. Counterrotating aircraft propulsor blades

    NASA Technical Reports Server (NTRS)

    Nelson, Joey L. (Inventor); Elston, III, Sidney B. (Inventor); Tseng, Wu-Yang (Inventor); Hemsworth, Martin C. (Inventor)

    1988-01-01

    A propulsor blade for an aircraft engine includes an airfoil section formed in the shape of a scimitar. A metallic blade spar is interposed between opposed surfaces of the blade and is bonded to the surfaces to establish structural integrity of the blade. The metallic blade spar includes a root end allowing attachment of the blade to the engine.

  13. Robots for Aircraft Maintenance

    NASA Technical Reports Server (NTRS)

    1993-01-01

    Marshall Space Flight Center charged USBI (now Pratt & Whitney) with the task of developing an advanced stripping system based on hydroblasting to strip paint and thermal protection material from Space Shuttle solid rocket boosters. A robot, mounted on a transportable platform, controls the waterjet angle, water pressure and flow rate. This technology, now known as ARMS, has found commercial applications in the removal of coatings from jet engine components. The system is significantly faster than manual procedures and uses only minimal labor. Because the amount of "substrate" lost is minimal, the life of the component is extended. The need for toxic chemicals is reduced, as is waste disposal and human protection equipment. Users of the ARMS work cell include Delta Air Lines and the Air Force, which later contracted with USBI for development of a Large Aircraft Paint Stripping system (LARPS). LARPS' advantages are similar to ARMS, and it has enormous potential in military and civil aircraft maintenance. The technology may also be adapted to aircraft painting, aircraft inspection techniques and paint stripping of large objects like ships and railcars.

  14. Aircraft Wake RCS Measurement

    NASA Technical Reports Server (NTRS)

    Gilson, William H.

    1994-01-01

    A series of multi-frequency radar measurements of aircraft wakes at altitudes of 5,000 to 25,00 ft. were performed at Kwajalein, R.M.I., in May and June of 1990. Two aircraft were tested, a Learjet 35 and a Lockheed C-5A. The cross-section of the wake of the Learjet was too small for detection at Kwajalein. The wake of the C-5A, although also very small, was detected and measured at VHF, UHF, L-, S-, and C-bands, at distances behind the aircraft ranging from about one hundred meters to tens of kilometers. The data suggest that the mechanism by which aircraft wakes have detectable radar signatures is, contrary to previous expectations, unrelated to engine exhaust but instead due to turbulent mixing by the wake vortices of pre-existing index of refraction gradients in the ambient atmosphere. These measurements were of necessity performed with extremely powerful and sensitive instrumentation radars, and the wake cross-section is too small for most practical applications.

  15. Aircraft noise prediction

    NASA Astrophysics Data System (ADS)

    Filippone, Antonio

    2014-07-01

    This contribution addresses the state-of-the-art in the field of aircraft noise prediction, simulation and minimisation. The point of view taken in this context is that of comprehensive models that couple the various aircraft systems with the acoustic sources, the propagation and the flight trajectories. After an exhaustive review of the present predictive technologies in the relevant fields (airframe, propulsion, propagation, aircraft operations, trajectory optimisation), the paper addresses items for further research and development. Examples are shown for several airplanes, including the Airbus A319-100 (CFM engines), the Bombardier Dash8-Q400 (PW150 engines, Dowty R408 propellers) and the Boeing B737-800 (CFM engines). Predictions are done with the flight mechanics code FLIGHT. The transfer function between flight mechanics and the noise prediction is discussed in some details, along with the numerical procedures for validation and verification. Some code-to-code comparisons are shown. It is contended that the field of aircraft noise prediction has not yet reached a sufficient level of maturity. In particular, some parametric effects cannot be investigated, issues of accuracy are not currently addressed, and validation standards are still lacking.

  16. Aircraft adaptive learning control

    NASA Technical Reports Server (NTRS)

    Lee, P. S. T.; Vanlandingham, H. F.

    1979-01-01

    The optimal control theory of stochastic linear systems is discussed in terms of the advantages of distributed-control systems, and the control of randomly-sampled systems. An optimal solution to longitudinal control is derived and applied to the F-8 DFBW aircraft. A randomly-sampled linear process model with additive process and noise is developed.

  17. Aircraft Wheel Life Assessment

    DTIC Science & Technology

    1993-07-01

    responsible for a significant amount of aircraft dam - age. Many such wheel failures have been catastrophic, resulting in a sudden loss of tire inflation...Fatigue Crack Growth," Fatigue and Fracture in Engineering Materials and Structures, Vol. 10, 419-428, 1987. Cox, B. N., Pardee , W., and Morris, W. L

  18. Advanced ATC: An aircraft perspective

    NASA Technical Reports Server (NTRS)

    Credeur, Leonard; Williams, David H.; Howell, William E.; Spitzer, Cary R.

    1986-01-01

    The principal operational improvements desired by commercial aircraft operators in the United States are efficient aircraft operations and delay reductions at the major terminals. Efforts underway within the Advanced Transport Operating Systems Program at the Langley Research Center to provide a technology basis for reducing delay while improving aircraft efficiency are discussed. The principal thrust is the development of time-based traffic control concepts which could be used within the framework of the upgraded National Airspace System and which would allow conventionally equipped aircraft to operate in a manner compatible with advanced aircraft.

  19. Turboprop cargo aircraft systems study

    NASA Technical Reports Server (NTRS)

    Muehlbauer, J. C.; Hewell, J. G., Jr.; Lindenbaum, S. P.; Randall, C. C.; Searle, N.; Stone, R. G., Jr.

    1981-01-01

    The effects of using advanced turboprop propulsion systems to reduce the fuel consumption and direct operating costs of cargo aircraft were studied, and the impact of these systems on aircraft noise and noise prints around a terminal area was determined. Parametric variations of aircraft and propeller characteristics were investigated to determine their effects on noiseprint areas, fuel consumption, and direct operating costs. From these results, three aircraft designs were selected and subjected to design refinements and sensitivity analyses. Three competitive turbofan aircraft were also defined from parametric studies to provide a basis for comparing the two types of propulsion.

  20. The AirLand Battle Trojan Horse: The Use of Bypassed Forces to Increase Tactical Depth in the Defense,

    DTIC Science & Technology

    1986-11-19

    ACCESSION NO NT INO.0.1 11 TTL (Infud Seurit Clssifcaton)The AirLand Battle Trojan Horse : The Use of 2 ~RS~4A AUhORS) Bypas-sedForces to Increase Tactical...operations by each of the three types of forces. The AirLand Battle Trojan Horse : The Use of Bypassed Forces to Increase Tactical Depth In The...Russell 1. Goehring Title of Monograph: The AirLand Battle Trojan Horse : The Use ,f Br- -cd Forces to Increase Tactical Depth In The Pe!’en’e

  1. Telemetry carrier ring and support

    NASA Technical Reports Server (NTRS)

    Wakeman, Thomas G. (Inventor)

    1992-01-01

    A telemetry carrier ring for use in a gas turbine engine includes an annular support ring connected to the engine and an annular carrier ring coupled to the support ring, each ring exhibiting different growth characteristics in response to thermal and mechanical loading. The carrier ring is coupled to the support ring by a plurality of circumferentially spaced web members which are relatively thin in an engine radial direction to provide a predetermined degree of radial flexibility. the web members have a circumferential width and straight axial line of action selected to transfer torque and thrust between the support ring and the carrier ring without substantial deflection. The use of the web members with radial flexibility provides compensation between the support ring and the carrier ring since the carrier ring grows at a different rate than the supporting ring.

  2. Flight demonstration of a self repairing flight control system in a NASA F-15 fighter aircraft

    NASA Technical Reports Server (NTRS)

    Urnes, James M.; Stewart, James; Eslinger, Robert

    1990-01-01

    Battle damage causing loss of control capability can compromise mission objectives and even result in aircraft loss. The Self Repairing Flight Control System (SRFCS) flight development program directly addresses this issue with a flight control system design that measures the damage and immediately refines the control system commands to preserve mission potential. The system diagnostics process detects in flight the type of faults that are difficult to isolate post flight, and thus cause excessive ground maintenance time and cost. The control systems of fighter aircraft have the control power and surface displacement to maneuver the aircraft in a very large flight envelope with a wide variation in airspeed and g maneuvering conditions, with surplus force capacity available from each control surface. Digital flight control processors are designed to include built-in status of the control system components, as well as sensor information on aircraft control maneuver commands and response. In the event of failure or loss of a control surface, the SRFCS utilizes this capability to reconfigure control commands to the remaining control surfaces, thus preserving maneuvering response. Correct post-flight repair is the key to low maintainability support costs and high aircraft mission readiness. The SRFCS utilizes the large data base available with digital flight control systems to diagnose faults. Built-in-test data and sensor data are used as inputs to an Onboard Expert System process to accurately identify failed components for post-flight maintenance action. This diagnostic technique has the advantage of functioning during flight, and so is especially useful in identifying intermittent faults that are present only during maneuver g loads or high hydraulic flow requirements. A flight system was developed to test the reconfiguration and onboard maintenance diagnostics concepts on a NASA F-15 fighter aircraft.

  3. Personnel emergency carrier vehicle

    NASA Technical Reports Server (NTRS)

    Owens, Lester J. (Inventor); Fedor, Otto H. (Inventor)

    1987-01-01

    A personnel emergency carrier vehicle is disclosed which includes a vehicle frame supported on steerable front wheels and driven rear wheels. A supply of breathing air is connected to quick connect face mask coupling and umbilical cord couplings for supplying breathing air to an injured worker or attendant either with or without a self-contained atmospheric protection suit for protection against hazardous gases at an accident site. A non-sparking hydraulic motion is utilized to drive the vehicle and suitable direction and throttling controls are provided for controlling the delivery of a hydraulic driving fluid from a pressurized hydraulic fluid accumulator. A steering axis is steerable through a handle to steer the front wheels through a linkage assembly.

  4. 19 CFR 10.183 - Duty-free entry of civil aircraft, aircraft engines, ground flight simulators, parts, components...

    Code of Federal Regulations, 2013 CFR

    2013-04-01

    ... Duty-free entry of civil aircraft, aircraft engines, ground flight simulators, parts, components, and... aircraft, aircraft engines, and ground flight simulators, including their parts, components, and... United States Coast Guard, aircraft, aircraft engines, and ground flight simulators, including...

  5. 19 CFR 10.183 - Duty-free entry of civil aircraft, aircraft engines, ground flight simulators, parts, components...

    Code of Federal Regulations, 2010 CFR

    2010-04-01

    ... Duty-free entry of civil aircraft, aircraft engines, ground flight simulators, parts, components, and... aircraft, aircraft engines, and ground flight simulators, including their parts, components, and... United States Coast Guard, aircraft, aircraft engines, and ground flight simulators, including...

  6. 19 CFR 10.183 - Duty-free entry of civil aircraft, aircraft engines, ground flight simulators, parts, components...

    Code of Federal Regulations, 2014 CFR

    2014-04-01

    ... Duty-free entry of civil aircraft, aircraft engines, ground flight simulators, parts, components, and... aircraft, aircraft engines, and ground flight simulators, including their parts, components, and... United States Coast Guard, aircraft, aircraft engines, and ground flight simulators, including...

  7. 19 CFR 10.183 - Duty-free entry of civil aircraft, aircraft engines, ground flight simulators, parts, components...

    Code of Federal Regulations, 2011 CFR

    2011-04-01

    ... Duty-free entry of civil aircraft, aircraft engines, ground flight simulators, parts, components, and... aircraft, aircraft engines, and ground flight simulators, including their parts, components, and... United States Coast Guard, aircraft, aircraft engines, and ground flight simulators, including...

  8. 19 CFR 10.183 - Duty-free entry of civil aircraft, aircraft engines, ground flight simulators, parts, components...

    Code of Federal Regulations, 2012 CFR

    2012-04-01

    ... Duty-free entry of civil aircraft, aircraft engines, ground flight simulators, parts, components, and... aircraft, aircraft engines, and ground flight simulators, including their parts, components, and... United States Coast Guard, aircraft, aircraft engines, and ground flight simulators, including...

  9. First Commuter Air Carrier Safety Symposium, January 16 - 17, 1980.

    DTIC Science & Technology

    1980-01-01

    year. 96 a n ity; :..’ r " din tli •i 1 Ot’.-, it youi are e:,cirkini or’ an ambitio,:7 ~: ,:a t , >’’’.:, t: :x s . ume1s there can be good servicc...this technological breakthr ough . S )rnp , ; enthusiastic acceptance of these new aircraft by the r , travel ing public is test j’onv 1o the fact...carriers with relatively large markets wnici thi-v could integrate with hubs to form viable economic route system,) s . Tn’e r : -st these substitutions

  10. Airline Transport Pilot, Aircraft Dispatcher, and Flight Navigator. Question Book. Expires September 1, 1991.

    ERIC Educational Resources Information Center

    Federal Aviation Administration (DOT), Washington, DC.

    This question book was developed by the Federal Aviation Administration (FAA) for testing applicants who are preparing for certification as airline transport pilots, aircraft dispatchers, or flight navigators. The publication contains several innovative features that are a departure from previous FAA publications related to air carrier personnel…

  11. Examination of Aircraft Interior Emergency Lighting in a Postcrash Fire Environment.

    DTIC Science & Technology

    1982-06-01

    Evacuation from Air Carrier, (No. AAS-74-3) Adopted 11/13/74. 6. Bukowski , R. W., Instruction Manual for National Bureau of Standards Photo- meteric...Aircraft Cabin, Report No. FAA-NA-79-42, December 1979. 9. Crane, Charles R., Ph.D., Human Tolerance Limit to Elevated Temperature: An Empirical Approach to

  12. Assessment of the application of advanced technologies to subsonic CTOL transport aircraft

    NASA Technical Reports Server (NTRS)

    Graef, J. D.; Sallee, G. P.; Verges, J. T.

    1974-01-01

    Design studies of the application of advanced technologies to future transport aircraft were conducted. These studies were reviewed from the perspective of an air carrier. A fundamental study of the elements of airplane operating cost was performed, and the advanced technologies were ranked in order of potential profit impact. Recommendations for future study areas are given.

  13. 14 CFR Special Federal Aviation... - Rules for use of portable oxygen concentrator systems on board aircraft

    Code of Federal Regulations, 2010 CFR

    2010-01-01

    ... concentrator systems on board aircraft Federal Special Federal Aviation Regulation 106 Aeronautics and Space FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION (CONTINUED) AIR CARRIERS AND OPERATORS FOR... OPERATIONS Pt. 121, SFAR No. 106 Special Federal Aviation Regulation 106—Rules for use of portable...

  14. 14 CFR Special Federal Aviation... - Rules for use of portable oxygen concentrator systems on board aircraft

    Code of Federal Regulations, 2014 CFR

    2014-01-01

    ... concentrator systems on board aircraft Federal Special Federal Aviation Regulation No. 106 Aeronautics and Space FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION (CONTINUED) AIR CARRIERS AND... SUPPLEMENTAL OPERATIONS Pt. 121, SFAR No. 106 Special Federal Aviation Regulation No. 106—Rules for use...

  15. 14 CFR Special Federal Aviation... - Rules for use of portable oxygen concentrator systems on board aircraft

    Code of Federal Regulations, 2013 CFR

    2013-01-01

    ... concentrator systems on board aircraft Federal Special Federal Aviation Regulation No. 106 Aeronautics and Space FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION (CONTINUED) AIR CARRIERS AND... SUPPLEMENTAL OPERATIONS Pt. 121, SFAR No. 106 Special Federal Aviation Regulation No. 106—Rules for use...

  16. 14 CFR Special Federal Aviation... - Rules for use of portable oxygen concentrator systems on board aircraft

    Code of Federal Regulations, 2011 CFR

    2011-01-01

    ... concentrator systems on board aircraft Federal Special Federal Aviation Regulation 106 Aeronautics and Space FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION (CONTINUED) AIR CARRIERS AND OPERATORS FOR... OPERATIONS Pt. 121, SFAR No. 106 Special Federal Aviation Regulation 106—Rules for use of portable...

  17. 14 CFR Special Federal Aviation... - Rules for use of portable oxygen concentrator systems on board aircraft

    Code of Federal Regulations, 2012 CFR

    2012-01-01

    ... concentrator systems on board aircraft Federal Special Federal Aviation Regulation 106 Aeronautics and Space FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION (CONTINUED) AIR CARRIERS AND OPERATORS FOR... OPERATIONS Pt. 121, SFAR No. 106 Special Federal Aviation Regulation 106—Rules for use of portable...

  18. Autonomous aircraft initiative study

    NASA Technical Reports Server (NTRS)

    Hewett, Marle D.

    1991-01-01

    The results of a consulting effort to aid NASA Ames-Dryden in defining a new initiative in aircraft automation are described. The initiative described is a multi-year, multi-center technology development and flight demonstration program. The initiative features the further development of technologies in aircraft automation already being pursued at multiple NASA centers and Department of Defense (DoD) research and Development (R and D) facilities. The proposed initiative involves the development of technologies in intelligent systems, guidance, control, software development, airborne computing, navigation, communications, sensors, unmanned vehicles, and air traffic control. It involves the integration and implementation of these technologies to the extent necessary to conduct selected and incremental flight demonstrations.

  19. Air pollution from aircraft

    NASA Technical Reports Server (NTRS)

    Heywood, J. B.; Fay, J. A.; Chigier, N. A.

    1979-01-01

    Forty-one annotated abstracts of reports generated at MIT and the University of Sheffield are presented along with summaries of the technical projects undertaken. Work completed includes: (1) an analysis of the soot formation and oxidation rates in gas turbine combustors, (2) modelling the nitric oxide formation process in gas turbine combustors, (3) a study of the mechanisms causing high carbon monoxide emissions from gas turbines at low power, (4) an analysis of the dispersion of pollutants from aircraft both around large airports and from the wakes of subsonic and supersonic aircraft, (5) a study of the combustion and flow characteristics of the swirl can modular combustor and the development and verification of NO sub x and CO emissions models, (6) an analysis of the influence of fuel atomizer characteristics on the fuel-air mixing process in liquid fuel spray flames, and (7) the development of models which predict the stability limits of fully and partially premixed fuel-air mixtures.

  20. Aircraft turbofan noise

    NASA Technical Reports Server (NTRS)

    Groeneweg, J. F.; Rice, E. J.

    1983-01-01

    Turbofan noise generation and suppression in aircraft engines are reviewed. The chain of physical processes which connect unsteady flow interactions with fan blades to far field noise is addressed. Mechanism identification and description, duct propagation, radiation and acoustic suppression are discussed. The experimental technique of fan inflow static tests are discussed. Rotor blade surface pressure and wake velocity measurements aid in the determination of the types and strengths of the generation mechanisms. Approaches to predicting or measuring acoustic mode content, optimizing treatment impedance to maximize attenuation, translating impedance into porous wall structure and interpreting far field directivity patterns are illustrated by comparisons of analytical and experimental results. The interdependence of source and acoustic treatment design to minimize far field noise is emphasized. Area requiring further research are discussed and the relevance of aircraft turbofan results to quieting other turbomachinery installations is addressed.

  1. Energy efficient aircraft engines

    NASA Technical Reports Server (NTRS)

    Chamberlin, R.; Miller, B.

    1979-01-01

    The three engine programs that constitute the propulsion portion of NASA's Aircraft Energy Efficiency Program are described, their status indicated, and anticipated improvements in SFC discussed. The three engine programs are: (1) engine component improvement, directed at current engines, (2) energy efficient engine, directed at new turbofan engines, and (3) advanced turboprops, directed at technology for advanced turboprop-powered aircraft with cruise speeds to Mach 0.8. Unique propulsion system interactive ties to the airframe resulting from engine design features to reduce fuel consumption are discussed. Emphasis is placed on the advanced turboprop since it offers the largest potential fuel savings of the three propulsion programs and also has the strongest interactive ties to the airframe.

  2. Energy efficient aircraft engines

    NASA Technical Reports Server (NTRS)

    Chamberlin, R.; Miller, B.

    1979-01-01

    The three engine programs that constitute the propulsion portion of NASA's Aircraft Energy Efficiency Program are described, their status indicated, and anticipated improvements in SFC discussed. The three engine programs are (1) Engine Component Improvement--directed at current engines, (2) Energy Efficiency Engine directed at new turbofan engines, and (3) Advanced Turboprops--directed at technology for advanced turboprop--powered aircraft with cruise speeds to Mach 0.8. Unique propulsion system interactive ties to the airframe resulting from engine design features to reduce fuel consumption are discussed. Emphasis is placed on the advanced turboprop since it offers the largest potential fuel savings of the three propulsion programs and also has the strongest interactive ties to the airframe.

  3. Aircraft Survivability. Fall 2011

    DTIC Science & Technology

    2011-01-01

    Aircraft Survivability Program (JASP) Short Course was held 17-20 May at the Naval Postgraduate School (NPS) in Monterey, CA. 52 students attended the...Postgraduate School where he earned his MBA in Financial Management. Jimmy earned his BS in General Science from the United States Naval Academy...Answering these questions requires credible threat models supported by high -fidelity test characterizations of the MANPADS missile threat. Based on

  4. X-29: Research Aircraft

    NASA Technical Reports Server (NTRS)

    1991-01-01

    A preliminary look at the Ames Dryden Flight Research Center in the context of the X-29 aircraft is provided. The uses of the X-29's 30 deg forward swept wing are examined. The video highlights the historical development of the forward swept wing, and its unique blend of speed, agility, and slow flight potential. The central optimization of the wing, the forward canard, and the rear flaps by an onboard flight computer is also described.

  5. Aircraft Survivability. Summer 2011

    DTIC Science & Technology

    2011-01-01

    Survivability Program Office SUMMER 2011 craShworthineSS & personnel casualties Report Documentation Page Form ApprovedOMB No. 0704-0188 Public...unclassified Standard Form 298 (Rev. 8-98) Prescribed by ANSI Std Z39-18 Aircraft Survivability is published three times a year by the Joint...and stroking seats. The knowledge gained from studying Vietnam crash data was consolidated into the Crash Survival Design Guide (CSDG), which

  6. Electrical Thermometers for Aircraft

    NASA Technical Reports Server (NTRS)

    Peterson, John B; Womack, S H J

    1937-01-01

    Electrical thermometers commonly used on aircraft are the thermoelectric type for measuring engine-cylinder temperatures, the resistance type for measuring air temperatures, and the superheat meters of thermoelectric and resistance types for use on airships. These instruments are described and their advantages and disadvantages enumerated. Methods of testing these instruments and the performance to be expected from each are discussed. The field testing of engine-cylinder thermometers is treated in detail.

  7. Aircraft EMP Isolation Study.

    DTIC Science & Technology

    1980-07-01

    also influence the formation of streamers. If electrons are swept away from the electrode surface , additional electrons must leave the surface , if...presented. The dielectric materials to be used in the proposed solutions are discussed. In order to simulate the electromagnetic pulse (EMP) of a nuclear...structure. Therefore, the flashover to ground of the aircraft structure (at the point of the sharp projection) depends on the amplitude and pulse shape of the

  8. Slotted Aircraft Wing

    NASA Technical Reports Server (NTRS)

    McLean, James D. (Inventor); Witkowski, David P. (Inventor); Campbell, Richard L. (Inventor)

    2006-01-01

    A swept aircraft wing includes a leading airfoil element and a trailing airfoil element. At least one full-span slot is defined by the wing during at least one transonic condition of the wing. The full-span slot allows a portion of the air flowing along the lower surface of the leading airfoil element to split and flow over the upper surface of the trailing airfoil element so as to achieve a performance improvement in the transonic condition.

  9. Geographic Region, Weather, Pilot Age and Air Carrier Crashes: a Case-Control Study

    PubMed Central

    Li, Guohua; Pressley, Joyce C.; Qiang, Yandong; Grabowski, Jurek G.; Baker, Susan P.; Rebok, George W.

    2009-01-01

    Background Information about risk factors of aviation crashes is crucial for developing effective intervention programs. Previous studies assessing factors associated with crash risk were conducted primarily in general aviation, air taxis and commuter air carriers. Methods A matched case-control design was used to examine the associations of geographic region, basic weather condition, and pilot age with the risk of air carrier (14 CFR Part 121) crash involvement. Cases (n=373) were air carrier crashes involving aircraft made by Boeing, McDonnell Douglas, and Airbus, recorded in the National Transportation Safety Board’s aviation crash database during 1983 through 2002, and controls (n=746) were air carrier incidents involving aircraft of the same three makes selected at random from the Federal Aviation Administration’s aviation incident database. Each case was matched with two controls on the calendar year when the index crash occurred. Conditional logistic regression was used for statistical analysis. Results With adjustment for basic weather condition, pilot age, and total flight time, the risk of air carrier crashes in Alaska was more than three times the risk for other regions [adjusted odds ratio (OR) 3.18, 95% confidence interval (CI) 1.35 – 7.49]. Instrument meteorological conditions were associated with an increased risk for air carrier crashes involving pilot error (adjusted OR 2.26, 95% CI 1.15 – 4.44) and a decreased risk for air carrier crashes without pilot error (adjusted OR 0.57, 95% CI 0.40 – 0.87). Neither pilot age nor total flight time was significantly associated with the risk of air carrier crashes. Conclusions The excess risk of air carrier crashes in Alaska and the effect of adverse weather on pilot-error crashes underscore the importance of environmental hazards in flight safety. PMID:19378910

  10. Texas Assoc. of Healthcare Facilities Management Competes in EPAs Sixth Annual Energy Star Battle of the Buildings

    EPA Pesticide Factsheets

    DALLAS - (July 22, 2015) Today, the Environmental Protection Agency (EPA) launched the 2015 Energy Star Battle of the Buildings. With dozens of buildings across the state, the Texas Association of Healthcare Facilities Management is among 125 teams

  11. Dryden B-52 Launch Aircraft in Flight over Dryden

    NASA Technical Reports Server (NTRS)

    1996-01-01

    NASA's venerable B-52 mothership flies over the main building at the Dryden Flight Research Center, Edwards, California. The B-52, used for launching experimental aircraft and for other flight research projects, has been a familiar sight in the skies over Edwards for more than 40 years and has also been both the oldest B-52 still flying and the aircraft with the lowest flight time of any B-52. NASA B-52, Tail Number 008, is an air launch carrier aircraft, 'mothership,' as well as a research aircraft platform that has been used on a variety of research projects. The aircraft, a 'B' model built in 1952 and first flown on June 11, 1955, is the oldest B-52 in flying status and has been used on some of the most significant research projects in aerospace history. Some of the significant projects supported by B-52 008 include the X-15, the lifting bodies, HiMAT (highly maneuverable aircraft technology), Pegasus, validation of parachute systems developed for the space shuttle program (solid-rocket-booster recovery system and the orbiter drag chute system), and the X-38. The B-52 served as the launch vehicle on 106 X-15 flights and flew a total of 159 captive-carry and launch missions in support of that program from June 1959 to October 1968. Information gained from the highly successful X-15 program contributed to the Mercury, Gemini, and Apollo human spaceflight programs as well as space shuttle development. Between 1966 and 1975, the B-52 served as the launch aircraft for 127 of the 144 wingless lifting body flights. In the 1970s and 1980s, the B-52 was the launch aircraft for several aircraft at what is now the Dryden Flight Research Center, Edwards, California, to study spin-stall, high-angle-of attack, and maneuvering characteristics. These included the 3/8-scale F-15/spin research vehicle (SRV), the HiMAT (Highly Maneuverable Aircraft Technology) research vehicle, and the DAST (drones for aerodynamic and structural testing). The aircraft supported the development of

  12. Interaction of Aircraft Wakes From Laterally Spaced Aircraft

    NASA Technical Reports Server (NTRS)

    Proctor, Fred H.

    2009-01-01

    Large Eddy Simulations are used to examine wake interactions from aircraft on closely spaced parallel paths. Two sets of experiments are conducted, with the first set examining wake interactions out of ground effect (OGE) and the second set for in ground effect (IGE). The initial wake field for each aircraft represents a rolled-up wake vortex pair generated by a B-747. Parametric sets include wake interactions from aircraft pairs with lateral separations of 400, 500, 600, and 750 ft. The simulation of a wake from a single aircraft is used as baseline. The study shows that wake vortices from either a pair or a formation of B-747 s that fly with very close lateral spacing, last longer than those from an isolated B-747. For OGE, the inner vortices between the pair of aircraft, ascend, link and quickly dissipate, leaving the outer vortices to decay and descend slowly. For the IGE scenario, the inner vortices ascend and last longer, while the outer vortices decay from ground interaction at a rate similar to that expected from an isolated aircraft. Both OGE and IGE scenarios produce longer-lasting wakes for aircraft with separations less than 600 ft. The results are significant because concepts to increase airport capacity have been proposed that assume either aircraft formations and/or aircraft pairs landing on very closely spaced runways.

  13. Infrared hot carrier diode mixer.

    PubMed

    Aukerman, L W; Erler, J W

    1977-11-01

    Detection of a 54.3-GHz beatnote at 10.6 microm has been observed with a hot carrier diode mixer. The diode consists of a "cat whisker" antenna, which forms an ohmic point contact to n-InAs. The mechanism of this room-temperature detector is described as the "thermoelectric effect" of hot carriers.

  14. 19 CFR 122.64 - Other aircraft.

    Code of Federal Regulations, 2014 CFR

    2014-04-01

    ... 19 Customs Duties 1 2014-04-01 2014-04-01 false Other aircraft. 122.64 Section 122.64 Customs... AIR COMMERCE REGULATIONS Clearance of Aircraft and Permission To Depart § 122.64 Other aircraft. Clearance or permission to depart shall be requested by the aircraft commander or agent for aircraft...

  15. 19 CFR 122.64 - Other aircraft.

    Code of Federal Regulations, 2013 CFR

    2013-04-01

    ... 19 Customs Duties 1 2013-04-01 2013-04-01 false Other aircraft. 122.64 Section 122.64 Customs... AIR COMMERCE REGULATIONS Clearance of Aircraft and Permission To Depart § 122.64 Other aircraft. Clearance or permission to depart shall be requested by the aircraft commander or agent for aircraft...

  16. 19 CFR 122.64 - Other aircraft.

    Code of Federal Regulations, 2012 CFR

    2012-04-01

    ... 19 Customs Duties 1 2012-04-01 2012-04-01 false Other aircraft. 122.64 Section 122.64 Customs... AIR COMMERCE REGULATIONS Clearance of Aircraft and Permission To Depart § 122.64 Other aircraft. Clearance or permission to depart shall be requested by the aircraft commander or agent for aircraft...

  17. 40 CFR 87.6 - Aircraft safety.

    Code of Federal Regulations, 2013 CFR

    2013-07-01

    ... 40 Protection of Environment 21 2013-07-01 2013-07-01 false Aircraft safety. 87.6 Section 87.6... POLLUTION FROM AIRCRAFT AND AIRCRAFT ENGINES General Provisions § 87.6 Aircraft safety. The provisions of... be met within the specified time without creating a hazard to aircraft safety....

  18. 19 CFR 122.64 - Other aircraft.

    Code of Federal Regulations, 2010 CFR

    2010-04-01

    ... 19 Customs Duties 1 2010-04-01 2010-04-01 false Other aircraft. 122.64 Section 122.64 Customs... AIR COMMERCE REGULATIONS Clearance of Aircraft and Permission To Depart § 122.64 Other aircraft. Clearance or permission to depart shall be requested by the aircraft commander or agent for aircraft...

  19. 40 CFR 87.6 - Aircraft safety.

    Code of Federal Regulations, 2014 CFR

    2014-07-01

    ... 40 Protection of Environment 20 2014-07-01 2013-07-01 true Aircraft safety. 87.6 Section 87.6... POLLUTION FROM AIRCRAFT AND AIRCRAFT ENGINES General Provisions § 87.6 Aircraft safety. The provisions of... be met within the specified time without creating a hazard to aircraft safety....

  20. 19 CFR 122.64 - Other aircraft.

    Code of Federal Regulations, 2011 CFR

    2011-04-01

    ... 19 Customs Duties 1 2011-04-01 2011-04-01 false Other aircraft. 122.64 Section 122.64 Customs... AIR COMMERCE REGULATIONS Clearance of Aircraft and Permission To Depart § 122.64 Other aircraft. Clearance or permission to depart shall be requested by the aircraft commander or agent for aircraft...

  1. Mission management aircraft operations manual

    NASA Technical Reports Server (NTRS)

    1992-01-01

    This manual prescribes the NASA mission management aircraft program and provides policies and criteria for the safe and economical operation, maintenance, and inspection of NASA mission management aircraft. The operation of NASA mission management aircraft is based on the concept that safety has the highest priority. Operations involving unwarranted risks will not be tolerated. NASA mission management aircraft will be designated by the Associate Administrator for Management Systems and Facilities. NASA mission management aircraft are public aircraft as defined by the Federal Aviation Act of 1958. Maintenance standards, as a minimum, will meet those required for retention of Federal Aviation Administration (FAA) airworthiness certification. Federal Aviation Regulation Part 91, Subparts A and B, will apply except when requirements of this manual are more restrictive.

  2. Advanced aircraft for atmospheric research

    NASA Technical Reports Server (NTRS)

    Russell, P.; Wegener, S.; Langford, J.; Anderson, J.; Lux, D.; Hall, D. W.

    1991-01-01

    The development of aircraft for high-altitude research is described in terms of program objectives and environmental, technological limitations, and the work on the Perseus A aircraft. The need for these advanced aircraft is proposed in relation to atmospheric science issues such as greenhouse trapping, the dynamics of tropical cyclones, and stratospheric ozone. The implications of the study on aircraft design requirements is addressed with attention given to the basic categories of high-altitude, long-range, long-duration, and nap-of-the-earth aircraft. A strategy is delineated for a platform that permits unique stratospheric measurements and is a step toward a more advanced aircraft. The goal of Perseus A is to carry scientific air sampling payloads weighing at least 50 kg to altitudes of more than 25 km. The airfoils are designed for low Reynolds numbers, the structural weight is very low, and the closed-cycle power plant runs on liquid oxygen.

  3. Aircraft cockpit vision: Math model

    NASA Technical Reports Server (NTRS)

    Bashir, J.; Singh, R. P.

    1975-01-01

    A mathematical model was developed to describe the field of vision of a pilot seated in an aircraft. Given the position and orientation of the aircraft, along with the geometrical configuration of its windows, and the location of an object, the model determines whether the object would be within the pilot's external vision envelope provided by the aircraft's windows. The computer program using this model was implemented and is described.

  4. Radar Detectability of Light Aircraft

    DTIC Science & Technology

    1976-04-01

    the aircraft is mounted on a structure that enables the viewing angle (aspect) presented to the radar to be varied. For each aircraft type, the RCS...environment; there are no spurious reflections from the ground or from the supporting structure ; and the effects of propeller rotation, small aircraft...motions due to c-ntrol action or atmospheric turbulence, and structural deflections due to inertial and aerodynamic loading, are properly represented

  5. Disorienting effects of aircraft catapult launchings: III. Cockpit displays and piloting performance.

    PubMed

    Cohen, M M

    1977-09-01

    Accelerations closely approximating those encountered in catapult launchings of carrier-based aircraft were generated on the Naval Air Development Center's human centrifuge Dynamic Flight Simulator. Flight instruments, controls, and flight dynamics of an A-7 aircraft were provided to four experienced Naval Aviators, who exercised closed-loop control of a simulated climbout immediately after they were exposed to the accelerations. Four experimental conditions were employed for each aviator: 1) no operational flight instruments, 2) conventional flight instruments, 3) a single carrier takeoff director display operating concurrently. Measures of flight parameters, including indicated airspeed, angle of attack, rate of climb, altitude, pitch attitude, and pitch trim adjustment were monitored throughout the simulation. Subjective reactions and piloting performance were examined under each of the four conditions. Results indicate that the carrier takeoff director display significantly reduced pilot workload and enhanced performance during the climbout.

  6. 14 CFR Section 04 - Air Carrier Groupings

    Code of Federal Regulations, 2010 CFR

    2010-01-01

    ... 14 Aeronautics and Space 4 2010-01-01 2010-01-01 false Air Carrier Groupings Section 04 Section 04... REGULATIONS UNIFORM SYSTEM OF ACCOUNTS AND REPORTS FOR LARGE CERTIFICATED AIR CARRIERS Section 04 Air Carrier Groupings (a) All large certificated air carriers are placed into three basic air carrier groupings...

  7. 14 CFR Section 04 - Air Carrier Groupings

    Code of Federal Regulations, 2011 CFR

    2011-01-01

    ... 14 Aeronautics and Space 4 2011-01-01 2011-01-01 false Air Carrier Groupings Section 04 Section 04... REGULATIONS UNIFORM SYSTEM OF ACCOUNTS AND REPORTS FOR LARGE CERTIFICATED AIR CARRIERS Section 04 Air Carrier Groupings (a) All large certificated air carriers are placed into three basic air carrier groupings...

  8. Optically induced free carrier light modulator

    NASA Technical Reports Server (NTRS)

    Gruber, C. L.; Richards, W. E.

    1969-01-01

    Signal carrier laser beam is optically modulated by a second laser beam of different frequency acting on a free carrier source to which the signal carrier laser is directed. The second laser beam affects the transmission characteristics of the free carrier source to light from the signal carrier laser, thus modulating it.

  9. Intelligent aircraft/airspace systems

    NASA Technical Reports Server (NTRS)

    Wangermann, John P.

    1995-01-01

    Projections of future air traffic predict at least a doubling of the number of revenue passenger miles flown by the year 2025. To meet this demand, an Intelligent Aircraft/Airspace System (IAAS) has been proposed. The IAAS operates on the basis of principled negotiation between intelligent agents. The aircraft/airspace system today consists of many agents, such as airlines, control facilities, and aircraft. All the agents are becoming increasingly capable as technology develops. These capabilities should be exploited to create an Intelligent Aircraft/Airspace System (IAAS) that would meet the predicted traffic levels of 2005.

  10. Scheduling of an aircraft fleet

    NASA Technical Reports Server (NTRS)

    Paltrinieri, Massimo; Momigliano, Alberto; Torquati, Franco

    1992-01-01

    Scheduling is the task of assigning resources to operations. When the resources are mobile vehicles, they describe routes through the served stations. To emphasize such aspect, this problem is usually referred to as the routing problem. In particular, if vehicles are aircraft and stations are airports, the problem is known as aircraft routing. This paper describes the solution to such a problem developed in OMAR (Operative Management of Aircraft Routing), a system implemented by Bull HN for Alitalia. In our approach, aircraft routing is viewed as a Constraint Satisfaction Problem. The solving strategy combines network consistency and tree search techniques.

  11. NASA research in aircraft propulsion

    NASA Technical Reports Server (NTRS)

    Beheim, M. A.

    1982-01-01

    A broad overview of the scope of research presently being supported by NASA in aircraft propulsion is presented with emphasis on Lewis Research Center activities related to civil air transports, CTOL and V/STOL systems. Aircraft systems work is performed to identify the requirements for the propulsion system that enhance the mission capabilities of the aircraft. This important source of innovation and creativity drives the direction of propulsion research. In a companion effort, component research of a generic nature is performed to provide a better basis for design and provides an evolutionary process for technological growth that increases the capabilities of all types of aircraft. Both are important.

  12. A Near Term Approach to Embedded Training: Battle Command Visualization 101

    DTIC Science & Technology

    2006-05-01

    U.S. Army Research Institute for the Behavioral and Social Sciences Research Report 1853 A Near Term Approach to Embedded Training: Battle Command...Breidenbach Northrop Grumman Carl W. Lickteig U.S. Army Research Institute May 2006 A .......- fnr n, hlip rxlq_•p . distribution is unlimited. 20060614041...U.S. Army Research Institute for the Behavioral and Social Sciences A Directorate of the Department of the Army Deputy Chief of Staff, G1 Authorized

  13. Budget battle looms. Clinton uses fraud fines, user fees to pay for programs.

    PubMed

    Gardner, J

    1998-02-09

    President Clinton ignited a new money battle for providers last week as he proposed an activist healthcare agenda in his proposal to balance the federal budget in the next fiscal year. In his $1.733 trillion fiscal 1999 spending plan, Clinton proposed that providers and health plans pay $659.2 million in new user fees to fund expanded provider audits, certification surveys and a host of other HCFA activities.

  14. Joint Battle Command - Platform (JBC-P) Multi-Service Operational Test and Evaluation Report

    DTIC Science & Technology

    2015-01-01

    a low success rate in interrogating radio frequency identification ( RFID ) tags. JBC-P Log allowed operators to create duplicate RFID tags that...Identification ( RFID ) tag interrogation, and reporting and message exchange with the Battle Command Sustainment Support System (BCS3). The JBC-P Log provides...celestial or terrestrial), which increases network robustness during mission operations.  JBC-P Log Capability– JBC-P Log provides RFID tag

  15. Tactical Order of Battle: A State-of-the-Art Survey

    DTIC Science & Technology

    1975-10-01

    German Army, wrote in his well known treatise On War: "Chapter V. Order of Battle of an Army. 12Riling, J. R. Baron von Steuben and His Regulations...has been: "How good is my opponent?" The question has been asked in many ways and with many differem, adjectives and adverbs : fighting value...encountered In estimating German unit Combat Effectiveness during Third Army’s push beyond the Rhine. His situation map usually carried so many fragmentary

  16. Joint Chemical Defense for the Rear Battle: Main Operating Bases in NATO’s Central Region

    DTIC Science & Technology

    1988-04-01

    Specifically , the Air Force needs to develop a doctrine publications set to support air base operations the way Army Field Manuals 3-3. 3-4, 3-5, and 3...operational suitability of existing doctrine for joint, fiad site CUD opeoations. The Appendix will list specific problems using the following format...eyes and respiratory tract, a two-piece (jacket and pants) permeable overgarment (commonly called the Battle Dress Overgarment or BDO ) to protect the

  17. Non-battle Craniomaxillofacial Injuries from U.S. Military Operations

    DTIC Science & Technology

    2013-01-01

    Paper received 26 November 2012 Accepted 21 January 2013 Keywords: Craniomaxillofacial injury Non-battle injury Blunt trauma MVC a b s t r a c t...characterized predominantly by blunt trauma, with mechanisms including motor vehicle collisions ( MVCs ) (37%), falls and other blunt trauma (both 20%). This...devices (IEDs) and rocket propelled grenades (RPGs)) (88%), ballistics (7%) and MVCs (2%). All injury mechanisms were statistically different between

  18. Global Comparison of Warring Groups in 2002–2007: Fatalities from Targeting Civilians vs. Fighting Battles

    PubMed Central

    Hicks, Madelyn Hsiao-Rei; Lee, Uih Ran; Sundberg, Ralph; Spagat, Michael

    2011-01-01

    Background Warring groups that compete to dominate a civilian population confront contending behavioral options: target civilians or battle the enemy. We aimed to describe degrees to which combatant groups concentrated lethal behavior into intentionally targeting civilians as opposed to engaging in battle with opponents in contemporary armed conflict. Methodology/Principal Findings We identified all 226 formally organized state and non-state groups (i.e. actors) that engaged in lethal armed conflict during 2002–2007: 43 state and 183 non-state. We summed civilians killed by an actor's intentional targeting with civilians and combatants killed in battles in which the actor was involved for total fatalities associated with each actor, indicating overall scale of armed conflict. We used a Civilian Targeting Index (CTI), defined as the proportion of total fatalities caused by intentional targeting of civilians, to measure the concentration of lethal behavior into civilian targeting. We report actor-specific findings and four significant trends: 1.) 61% of all 226 actors (95% CI 55% to 67%) refrained from targeting civilians. 2.) Logistic regression showed actors were more likely to have targeted civilians if conflict duration was three or more years rather than one year. 3.) In the 88 actors that targeted civilians, multiple regressions showed an inverse correlation between CTI values and the total number of fatalities. Conflict duration of three or more years was associated with lower CTI values than conflict duration of one year. 4.) When conflict scale and duration were accounted for, state and non-state actors did not differ. We describe civilian targeting by actors in prolonged conflict. We discuss comparable patterns found in nature and interdisciplinary research. Conclusions/Significance Most warring groups in 2002–2007 did not target civilians. Warring groups that targeted civilians in small-scale, brief conflict concentrated more lethal behavior into

  19. Dryden B-52 Launch Aircraft on Edwards AFB Runway

    NASA Technical Reports Server (NTRS)

    1996-01-01

    NASA's venerable workhorse, the B-52 mothership, rolls out on the Edwards AFB runway after a test flight in 1996. Over the course of more than 40 years, the B-52 launched numerous experimental aircraft, ranging from the X-15 to the X-38, and was also used as a flying testbed for a variety of other research projects. NASA B-52, Tail Number 008, is an air launch carrier aircraft, 'mothership,' as well as a research aircraft platform that has been used on a variety of research projects. The aircraft, a 'B' model built in 1952 and first flown on June 11, 1955, is the oldest B-52 in flying status and has been used on some of the most significant research projects in aerospace history. Some of the significant projects supported by B-52 008 include the X-15, the lifting bodies, HiMAT (highly maneuverable aircraft technology), Pegasus, validation of parachute systems developed for the space shuttle program (solid-rocket-booster recovery system and the orbiter drag chute system), and the X-38. The B-52 served as the launch vehicle on 106 X-15 flights and flew a total of 159 captive-carry and launch missions in support of that program from June 1959 to October 1968. Information gained from the highly successful X-15 program contributed to the Mercury, Gemini, and Apollo human spaceflight programs as well as space shuttle development. Between 1966 and 1975, the B-52 served as the launch aircraft for 127 of the 144 wingless lifting body flights. In the 1970s and 1980s, the B-52 was the launch aircraft for several aircraft at what is now the Dryden Flight Research Center, Edwards, California, to study spin-stall, high-angle-of attack, and maneuvering characteristics. These included the 3/8-scale F-15/spin research vehicle (SRV), the HiMAT (Highly Maneuverable Aircraft Technology) research vehicle, and the DAST (drones for aerodynamic and structural testing). The aircraft supported the development of parachute recovery systems used to recover the space shuttle solid rocket

  20. Dryden B-52 Launch Aircraft on Dryden Ramp

    NASA Technical Reports Server (NTRS)

    1996-01-01

    NASA's venerable B-52 mothership sits on the ramp in front of the Dryden Flight Research Center, Edwards, California. Over the course of more than 40 years, the B-52 launched numerous experimental aircraft, ranging from the X-15 to the X-38, and was also used as a flying testbed for a variety of other research projects. NASA B-52, Tail Number 008, is an air launch carrier aircraft, 'mothership,' as well as a research aircraft platform that has been used on a variety of research projects. The aircraft, a 'B' model built in 1952 and first flown on June 11, 1955, is the oldest B-52 in flying status and has been used on some of the most significant research projects in aerospace history. Some of the significant projects supported by B-52 008 include the X-15, the lifting bodies, HiMAT (highly maneuverable aircraft technology), Pegasus, validation of parachute systems developed for the space shuttle program (solid-rocket-booster recovery system and the orbiter drag chute system), and the X-38. The B-52 served as the launch vehicle on 106 X-15 flights and flew a total of 159 captive-carry and launch missions in support of that program from June 1959 to October 1968. Information gained from the highly successful X-15 program contributed to the Mercury, Gemini, and Apollo human spaceflight programs as well as space shuttle development. Between 1966 and 1975, the B-52 served as the launch aircraft for 127 of the 144 wingless lifting body flights. In the 1970s and 1980s, the B-52 was the launch aircraft for several aircraft at what is now the Dryden Flight Research Center, Edwards, California, to study spin-stall, high-angle-of attack, and maneuvering characteristics. These included the 3/8-scale F-15/spin research vehicle (SRV), the HiMAT (Highly Maneuverable Aircraft Technology) research vehicle, and the DAST (drones for aerodynamic and structural testing). The aircraft supported the development of parachute recovery systems used to recover the space shuttle solid rocket