Plume Impingement Analysis for the European Service Module Propulsion System
NASA Technical Reports Server (NTRS)
Yim, John Tamin; Sibe, Fabien; Ierardo, Nicola
2014-01-01
Plume impingement analyses were performed for the European Service Module (ESM) propulsion system Orbital Maneuvering System engine (OMS-E), auxiliary engines, and reaction control system (RCS) engines. The heat flux from plume impingement on the solar arrays and other surfaces are evaluated. This information is used to provide inputs for the ESM thermal analyses and help determine the optimal configuration for the RCS engines.
Expedition One crew in Russian with Service Module
2000-07-14
Photographic documentation of Expedition One crew in Russia with Service Module. Views include: The three crew members for ISS Expedition One train with computers on the trainer / mockup for the Zvezda Service Module. From the left are cosmonauts Yuri Gidzenko, Soyuz commander; and Sergei Krikalev, flight engineer; and astronaut William Shepherd, mission commander. The session took place at the Gagarin Cosmonaut Training Center in Russia (18628). View looking toward the hatch inside the Zvezda Service Module trainer / mockup at the Gagarin Cosmonaut Training Center in Russia (18629). A wide shot of the Zvezda Service Module trainer / mockup, with the transfer compartment in the foreground (18630). Side view of the Zvezda Service Module (18631). An interior shot of the Zarya / Functional Cargo Bay (FGB) trainer / mockup (18632). Astronaut Scott Kelly, director of operations - Russia, walks through a full scale trainer / mockup for the Zvezda Service Module at the Gagarin Cosmonaut Training Center in Russia (18633). Astronaut William Shepherd (right) mission commander for ISS Expedition One, and Sergei Krikalev, flight engineer, participate in a training session in a trainer / mockup of the Zvezda Service Module (18634).
Tyurin and Williams in Zvezda Service module
2007-04-21
ISS014-E-19924 (21 April 2007) --- Cosmonaut Mikhail Tyurin (left), Expedition 14 flight engineer representing Russia's Federal Space Agency, and astronaut Sunita L. Williams, Expedition 15 flight engineer, drink beverages as they pose for a photo in the Zvezda Service Module of the International Space Station.
Tyurin and Voss perform maintenance on the TVIS treadmill in the Service Module
2001-08-19
ISS003-E-5200 (19 August 2001) --- Cosmonaut Mikhail Tyurin (left), Expedition Three flight engineer representing Rosaviakosmos, and astronaut James S. Voss, Expedition Two flight engineer, perform maintenance in the Zvezda Service Module on the International Space Station (ISS). This image was taken with a digital still camera.
Voss with soldering tool in Service Module
2001-03-28
ISS002-E-5068 (28 March 2001) --- Astronaut James S. Voss, Expedition Two flight engineer, prepares to use a soldering tool for a maintenance task in the Zvezda Service Module onboard the International Space Station (ISS). Astronaut Susan J. Helms, flight engineer, is in the background. The image was recorded with a digital still camera.
Apollo 11 Command Service Module
NASA Technical Reports Server (NTRS)
1969-01-01
A close-up view of the Apollo 11 command service module ready to be mated with the spacecraft LEM adapter of the third stage. The towering 363-foot Saturn V was a multi-stage, multi-engine launch vehicle standing taller than the Statue of Liberty. Altogether, the Saturn V engines produced as much power as 85 Hoover Dams.
Integrated orbital servicing study follow-on. Volume 3: Engineering test unit and controls
NASA Technical Reports Server (NTRS)
1978-01-01
A one-g servicing demonstration system which can be used to investigate and develop, in a real time hands-on situation, a wide variety of the mechanism and control system aspects of orbital servicing in the form of module exchange is described including the engineering test unit and the servicer servo drive console. A series of recommendations for future work is given concerning the control problem and more efficient module exchanges, mechanical elements, and electronics.
1968-01-01
This is a cutaway illustration of the Saturn V service module configuration. Packed with plumbing and tanks, the service module was the command module's constant companion until just before reentry. All components not needed during the last few minutes of flight, and therefore requiring no protection against reentry heat, were transported in this module. It carried oxygen for most of the trip, fuel cells to generate electricity (along with the oxygen and hydrogen to run them); small engines to control pitch, roll, and yaw; and a large engine to propel the spacecraft into, and out of, lunar orbit.
Parmitano with checklist in Service module
2013-11-08
ISS037-E-028305 (8 Nov. 2013) --- European Space Agency astronaut Luca Parmitano, Expedition 37 flight engineer, reads a procedures checklist in the Zvezda Service Module of the International Space Station.
NASA Technical Reports Server (NTRS)
Millard, Jon
2014-01-01
The European Space Agency (ESA) has entered into a partnership with the National Aeronautics and Space Administration (NASA) to develop and provide the Service Module (SM) for the Orion Multipurpose Crew Vehicle (MPCV) Program. The European Service Module (ESM) will provide main engine thrust by utilizing the Space Shuttle Program Orbital Maneuvering System Engine (OMS-E). Thrust Vector Control (TVC) of the OMS-E will be provided by the Orbital Maneuvering System (OMS) TVC, also used during the Space Shuttle Program. NASA will be providing the OMS-E and OMS TVC to ESA as Government Furnished Equipment (GFE) to integrate into the ESM. This presentation will describe the OMS-E and OMS TVC and discuss the implementation of the hardware for the ESM.
Apollo-Lunar Orbital Rendezvous Technique
NASA Technical Reports Server (NTRS)
1963-01-01
The film shows artists rendition of the spacecrafts, boosters, and flight of the Apollo lunar missions. The Apollo spacecraft will consist of three modules: the manned Command Module; the Service Module, which contains propulsion systems; and the Lunar Excursion Module (LEM) to carry astronauts to the moon and back to the Command and Service Modules. The spacecraft will be launched via a three-stage Saturn booster. The first stage will provide 7.5 million pounds of thrust from five F-1 engines for liftoff and initial powered flight. The second stage will develop 1 million pounds of thrust from five J-2 engines to boost the spacecraft almost into Earth orbit. Immediately after ignition of the second stage, the Launch Escape System will be jettisoned. A single J-2 engine in the S4B stage will provide 200,000 pounds of thrust to place the spacecraft in an earth parking orbit. It also will be used to propel the spacecraft into a translunar trajectory, then it will separate from the Apollo Modules. Onboard propulsion systems will be used to insert the spacecraft into lunar orbit. Two astronauts will enter the LEM, which will separate from the command and service modules. The LEM will go into elliptical orbit and prepare for landing. The LEM will lift off of the Moon's surface to return to the Command and Service Modules, and most likely be left in lunar orbit. After leaving the Moon's orbit, and shortly before entering Earth's orbit, the Service Module will be ejected. The Command Module will be oriented for reentry into the Earth's atmosphere. A drogue parachute will deploy at approximately 50,000 feet, followed by the main parachute system for touchdown.
1970-04-01
Apollo 13 onboard photo: This view of the severely damaged Apollo 13 Service Module was photographed from the Lunar Module/Command Module following the jettison of the Service Module. As seen here, an entire panel of the Service Module was blown away by the apparent explosion of oxygen tank number two located in Sector 4 of the Service Module. Two of the three fuel cells are visible just forward (above) the heavily damaged area. Three fuel cells, two oxygen tanks, and two hydrogen tanks, are located in Sector 4. The damaged area is located above the S-band high gain anterna. Nearest the camera is the Service Propulsion System (SPS) engine and nozzle. The damage to the Service Module caused the Apollo 13 crewmen to use the Lunar Module as a lifeboat. The Lunar Module was jettisoned by the Command Module just prior to Earth re-entry.
ERIC Educational Resources Information Center
Rains, Larry
This module is the third of nine modules in the competency-based Missouri Auto Mechanics Curriculum Guide. Six units cover: fuel supply systems; carburetion; carburetor service; gasoline engine electronic fuel injection; diesel fuel injection; and exhaust systems and turbochargers. Introductory materials include a competency profile and…
Voss in hatch at aft end of Service module
2001-03-22
ISS002-E-5702 (22 March 2001) --- Astronaut James S. Voss, Expedition Two flight engineer, translates through the forward hatch of the Zvezda Service Module. The image was recorded with a digital still camera.
Magnus Food Prep in Service Module (SM)
2009-01-07
ISS018-E-018423 (7 Jan. 2009) --- Astronaut Sandra Magnus, Expedition 18 flight engineer, poses for a photo while holding food pouches near the galley in the Zvezda Service Module of the International Space Station.
Barratt with TVIS in Service module
2009-04-23
ISS019-E-009818 (23 April 2009) --- Astronaut Michael Barratt, Expedition 19/20 flight engineer, performs in-flight maintenance on the Treadmill Vibration Isolation System (TVIS) in the Zvezda Service Module of the International Space Station.
Barratt with TVIS in Service module
2009-04-23
ISS019-E-009857 (23 April 2009) --- Astronaut Michael Barratt, Expedition 19/20 flight engineer, performs in-flight maintenance on the Treadmill Vibration Isolation System (TVIS) in the Zvezda Service Module of the International Space Station.
Barratt with TVIS in Service module
2009-04-23
ISS019-E-009840 (23 April 2009) --- Astronaut Michael Barratt, Expedition 19/20 flight engineer, performs in-flight maintenance on the Treadmill Vibration Isolation System (TVIS) in the Zvezda Service Module of the International Space Station.
Barratt with TVIS in Service module
2009-04-23
ISS019-E-009856 (23 April 2009) --- Astronaut Michael Barratt, Expedition 19/20 flight engineer, performs in-flight maintenance on the Treadmill Vibration Isolation System (TVIS) in the Zvezda Service Module of the International Space Station.
Barratt with TVIS in Service module
2009-04-23
ISS019-E-009819 (23 April 2009) --- Astronaut Michael Barratt, Expedition 19/20 flight engineer, performs in-flight maintenance on the Treadmill Vibration Isolation System (TVIS) in the Zvezda Service Module of the International Space Station.
Voss in Service module with cycle ergometer
2001-03-23
ISS002-E-5732 (23 March 2001) --- James S. Voss, Expedition Two flight engineer, prepares to exercise on the cycle ergometer in the Zvezda Service Module. The image was taken with a digital still camera.
View of damaged Apollo 13 Service Module from the Lunar/Command Modules
1970-04-17
AS13-58-8464 (17 April 1970) --- This view of the severely damaged Apollo 13 Service Module (SM) was photographed from the Lunar Module/Command Module (LM/CM) following SM jettisoning. Nearest the camera is the Service Propulsion System (SPS) engine and nozzle. An entire SM panel was blown away by the apparent explosion of oxygen tank number two located in Sector 4 of the SM. The apparent rupture of the oxygen tank caused the Apollo 13 crew men to use the Lunar Module (LM) as a "lifeboat".
ISS Expedition 18 Food Prep in Service Module (SM)
2009-01-01
ISS018-E-017005 (1 Jan. 2009) --- Astronaut Sandra Magnus, Expedition 18 flight engineer, poses for a photo with food which she prepared at the galley in the Zvezda Service Module of the International Space Station.
Volkov exercises on TVIS in Service Module
2011-11-08
ISS029-E-040701 (8 Nov. 2011) --- Russian cosmonaut Sergei Volkov, Expedition 29 flight engineer, equipped with a bungee harness, exercises on the Treadmill Vibration Isolation System (TVIS) in the Zvezda Service Module of the International Space Station.
Kotov with Cryogem-03 refrigerator in the Zvezda Service module
2007-04-01
ISS014-E-19179 (April 2007) --- Cosmonaut Oleg V. Kotov, Expedition 15 flight engineer representing Russia's Federal Space Agency, works with a test sample in the Zvezda Service Module of the International Space Station.
Kotov with Cryogem-03 refrigerator in the Zvezda Service module
2007-04-01
ISS014-E-19178 (April 2007) --- Cosmonaut Oleg V. Kotov, Expedition 15 flight engineer representing Russia's Federal Space Agency, works with a Cryogem-03 refrigerator in the Zvezda Service Module of the International Space Station.
NASA Technical Reports Server (NTRS)
Lobb, J. D., Jr.
1978-01-01
Plume impingement effects of the service module reaction control system thruster firings were studied to determine if previous flight experience would support the current plume impingement model for the orbiter reaction control system engines. The orbiter reaction control system is used for rotational and translational maneuvers such as those required during rendezvous, braking, docking, and station keeping. Therefore, an understanding of the characteristics and effects of the plume force fields generated by the reaction control system thruster firings were examined to develop the procedures for orbiter/payload proximity operations.
Tyurin in Zvezda Service module
2007-03-01
ISS014-E-15711 (1 March 2007) --- Cosmonaut Mikhail Tyurin, Expedition 14 flight engineer representing Russia's Federal Space Agency, disconnects a SKV1 heat exchanger unit during in-flight maintenance (IFM) in the Zvezda Service Module of the International Space Station.
Wakata with TVIS in Service module
2009-04-23
ISS019-E-009824 (23 April 2009) --- Japan Aerospace Exploration Agency (JAXA) astronaut Koichi Wakata, Expedition 19/20 flight engineer, performs in-flight maintenance on the Treadmill Vibration Isolation System (TVIS) in the Zvezda Service Module of the International Space Station.
Wakata with TVIS in Service module
2009-04-23
ISS019-E-009853 (23 April 2009) --- Japan Aerospace Exploration Agency (JAXA) astronaut Koichi Wakata, Expedition 19/20 flight engineer, performs in-flight maintenance on the Treadmill Vibration Isolation System (TVIS) in the Zvezda Service Module of the International Space Station.
Barratt with TVIS in Service module
2009-04-22
ISS019-E-009491 (22 April 2009) --- Astronaut Michael Barratt, Expedition 19/20 flight engineer, poses for a photo with the Treadmill Vibration Isolation System (TVIS) during in-flight maintenance operations in the Zvezda Service Module of the International Space Station.
Williams with TVIS hardware in Zvezda Service module
2007-02-26
ISS014-E-15136 (26 Feb. 2007) --- Astronaut Sunita L. Williams, Expedition 14 flight engineer, performs maintenance work on the Treadmill Vibration Isolation System (TVIS) during routine in-flight maintenance (IFM) in the Zvezda Service Module of the International Space Station.
Multiple Learning Strategies Project. Small Engine Repair Service. [Regular Vocational. Vol. 2.
ERIC Educational Resources Information Center
Pitts, Jim; And Others
This instructional package is one of two designed for use by regular vocational students in the vocational area of small engine repair service. Contained in this document are forty-nine learning modules organized into eleven units: test equipment; motorcycle; engine removal and replacement; machining; tune-ups; short blocks; storage; filling out…
Expedition Two crew share dessert in Zvezda module
2001-06-10
ISS002-E-6534 (10 June 2001) --- Expedition Two crewmembers Yury V. Usachev (left), mission commander, James S. Voss, flight engineer, and Susan J. Helms, flight engineer, share a dessert in the Zvezda Service Module. Usachev represents Rosaviakosmos. The image was recorded with a digital still camera.
Krikalev in Service module with tools
2001-03-30
ISS01-E-5150 (December 2000) --- Cosmonaut Sergei K. Krikalev, Expedition One flight engineer, retrieves a tool during an installation and set-up session in the Zvezda service module aboard the International Space Station (ISS). The picture was recorded with a digital still camera.
Voss with soldering tool in Service Module
2001-03-28
ISS002-E-5069 (28 March 2001) --- Astronaut James S. Voss, Expedition Two flight engineer, uses a soldering tool for a maintenance task in the Zvezda Service Module onboard the International Space Station (ISS). The image was recorded with a digital still camera.
DIESEL ENGINE SYSTEMS. AGRICULTURAL MACHINERY--SERVICE OCCUPATIONS, MODULE NUMBER 15.
ERIC Educational Resources Information Center
Ohio State Univ., Columbus. Center for Vocational and Technical Education.
ONE OF A SERIES DESIGNED TO HELP TEACHERS PREPARE POSTSECONDARY STUDENTS FOR AGRICULTURAL MACHINERY SERVICE OCCUPATIONS AS PARTS MEN, MECHANICS, MECHANIC'S HELPERS, AND SERVICE SUPERVISORS, THIS GUIDE AIMS TO DEVELOP STUDENT UNDERSTANDING OF THE CONSTRUCTION AND OPERATING PRINCIPLES OF DIESEL ENGINES. IT WAS DEVELOPED BY A NATIONAL TASK FORCE ON…
Multiple Learning Strategies Project. Small Engine Repair Service. Regular Vocational. [Vol. 1.
ERIC Educational Resources Information Center
Pitts, Jim; And Others
This instructional package is one of two designed for use by regular vocational students in the vocational area of small engine repair service. Contained in this document are forty-four learning modules organized into ten units: engine block; air cleaner; starters; fuel tanks; lines, filters, and pumps; carburetors; electrical; magneto systems;…
Remembering the Giants: Apollo Rocket Propulsion Development
NASA Technical Reports Server (NTRS)
Fisher, Steven C. (Editor); Rahman, Shamim A. (Editor)
2009-01-01
Topics discussed include: Rocketdyne - F-1 Saturn V First Stage Engine; Rocketdyne - J-2 Saturn V 2nd & 3rd Stage Engine; Rocketdyne - SE-7 & SE-8 Engines; Aerojet - AJ10-137 Apollo Service Module Engine; Aerojet - Attitude Control Engines; TRW - Lunar Descent Engine; and Rocketdyne - Lunar Ascent Engine.
Voss with coffee and snack in Service Module
2001-04-12
ISS002-E-5532 (12 April 2001) --- Astronaut James S. Voss, Expedition Two flight engineer, has a coffee and a snack at the table in the Zvezda / Service Module of the International Space Station (ISS). This image was recorded with a digital still camera.
Helms and Voss in Service Module
2001-04-10
ISS002-E-5335 (10 April 2001) --- Astronaut Susan J. Helms (left and astronaut James S. Voss, both Expedition Two flight engineers, pose for a photograph aboard the Zvezda/Service Module of the International Space Station (ISS). This image was recorded with a digital still camera.
Orion Service Module Reaction Control System Plume Impingement Analysis Using PLIMP/RAMP2
NASA Technical Reports Server (NTRS)
Wang, Xiao-Yen J.; Gati, Frank; Yuko, James R.; Motil, Brian J.; Lumpkin, Forrest E.
2009-01-01
The Orion Crew Exploration Vehicle Service Module Reaction Control System engine plume impingement was computed using the plume impingement program (PLIMP). PLIMP uses the plume solution from RAMP2, which is the refined version of the reacting and multiphase program (RAMP) code. The heating rate and pressure (force and moment) on surfaces or components of the Service Module were computed. The RAMP2 solution of the flow field inside the engine and the plume was compared with those computed using GASP, a computational fluid dynamics code, showing reasonable agreement. The computed heating rate and pressure using PLIMP were compared with the Reaction Control System plume model (RPM) solution and the plume impingement dynamics (PIDYN) solution. RPM uses the GASP-based plume solution, whereas PIDYN uses the SCARF plume solution. Three sets of the heating rate and pressure solutions agree well. Further thermal analysis on the avionic ring of the Service Module showed that thermal protection is necessary because of significant heating from the plume.
OA-7 Mate Service Module to Cargo Module
2017-02-14
In the Space Station Processing Facility at NASA's Kennedy Space Center in Florida, technicians and engineers mate a Cygnus spacecraft's pressurized cargo module to its service module. Cygnus is being prepared to deliver thousands of pounds of supplies, equipment and scientific research materials on the Orbital ATK CRS-7 mission to the International Space Station. Scheduled to launch on March 19, 2017, the commercial resupply services mission will lift off atop a United Launch Alliance Atlas V rocket from Space launch Complex 41 at Cape Canaveral Air Force Station.
ERIC Educational Resources Information Center
Ohio State Univ., Columbus. Center for Vocational and Technical Education.
ONE OF A SERIES DESIGNED TO HELP TEACHERS PREPARE POSTSECONDARY STUDENTS FOR THE AGRICULTURAL MACHINERY SERVICE OCCUPATIONS AS PARTS MEN, MECHANICS, MECHANIC'S HELPERS, OR SERVICE SUPERVISORS, THIS GUIDE AIMS TO DEVELOP STUDENT COMPETENCY IN THE ADJUSTMENT, MAINTENANCE, AND REPAIR OF SMALL GASOLINE ENGINES. IT WAS DEVELOPED BY A NATIONAL TASK…
2009-02-12
ISS018-E-030101 (12 Feb. 2009) --- Astronaut Sandra Magnus, Expedition 18 flight engineer, equipped with a bungee harness, exercises on the Treadmill Vibration Isolation System (TVIS) in the Zvezda Service Module of the International Space Station.
2009-02-12
ISS018-E-030096 (12 Feb. 2009) --- Astronaut Sandra Magnus, Expedition 18 flight engineer, equipped with a bungee harness, exercises on the Treadmill Vibration Isolation System (TVIS) in the Zvezda Service Module of the International Space Station.
Voss in Service module with cycle ergometer
2001-03-23
ISS002-E-5734 (23 March 2001) --- Astronaut James S. Voss, Expedition Two flight engineer, gives his arms and upper body a workout with the bicycle ergometer facility in the Zvezda Service Module aboard the International Space Station (ISS). The image was recorded with a digital still camera.
Helms and Usachev with checklist in Service Module
2001-05-16
ISS002-E-7605 (16 May 2001) --- Susan J. Helms, flight engineer, and Yury V. Usachev of Rosaviakosmos, mission commander, read over procedures at the computer workstation in the Zvezda Service Module during the Expedition Two mission. The image was taken with a digital still camera.
Automotive Modules. Vocational Behavioral Objectives: A Guide for Individualizing Instruction.
ERIC Educational Resources Information Center
Westinghouse Learning Corp., New York, NY.
The curriculum guide deals with automotive repair skills at the secondary level of vocational education and industrial arts. It addresses the subject in behavioral terms, as prominent components of the career education concept. Presenting four skill modules, auto body repair, gas engine repair, service, and diesel engine mechanics, the objectives…
ERIC Educational Resources Information Center
Pitts, Jim; And Others
This instructional package, one of two designed for low reader-educable mentally impaired students, focuses on the vocational area of small engine repair service. (Low readers are identified as those reading at a 3-6 grade level.) Contained in this document are forty-three learning modules organized into nine units: engine block; air cleaner;…
Voss in Service Module with apples
2001-03-22
ISS002-E-5710 (22 March 2001) --- Astronaut James S. Voss, Expedition Two flight engineer, appears to be trying to decide between two colors or two species of apples as he ponders them in the Zvezda Service Module on the International Space Station (ISS). This photo was taken with a digital still camera.
PZEh-MO-8/Body Mass Measurement in Service Module
2009-05-06
ISS019-E-014222 (6 May 2009) --- Japan Aerospace Exploration Agency (JAXA) astronaut Koichi Wakata, Expedition 19/20 flight engineer, uses the IM mass measurement device to perform the PZEh-MO-8/Body Mass Measurement Russian biomedical routine assessments in the Zvezda Service Module of the International Space Station.
PZEh-MO-8/Body Mass Measurement in Service Module
2009-05-06
ISS019-E-014216 (6 May 2009) --- Japan Aerospace Exploration Agency (JAXA) astronaut Koichi Wakata, Expedition 19/20 flight engineer, uses the IM mass measurement device to perform the PZEh-MO-8/Body Mass Measurement Russian biomedical routine assessments in the Zvezda Service Module of the International Space Station.
Voss with docking probe in Service module
2001-05-30
ISS002-E-6478 (30 May 2001) --- James S. Voss, Expedition Two flight engineer, handles a spacecraft docking probe in the Service Module. The docking probe assists with the docking of the Soyuz and Progress vehicles to the International Space Station. The image was taken with a digital still camera.
2005-08-05
S114-E-7139 (5 August 2005) --- Astronaut Eileen M. Collins, STS-114 commander, floats in the Zvezda Service Module of the International Space Station while Space Shuttle Discovery was docked to the Station. Astronaut John L. Phillips, Expedition 11 NASA Space Station science officer and flight engineer, is visible at bottom right.
Helms eats apple and carrot stick in Service module
2001-04-21
ISS002-E-5357 (21 April 2001) --- Just hours before the arrival of the STS-100/Endeavour crew, astronaut Susan J. Helms, Expedition Two flight engineer, enjoys a brief snack in the Zvezda Service Module on the International Space Station (ISS). The image was recorded with a digital still camera.
2014-04-01
engine mechanic, selects a compressor blade to install in the core module of an F-16 jet engine. DLA Aviation has partnered with Air Force customers to...Support 9 Supporting the Fleet 14 Air Force Support 18 Beyond the Military Services 22 SERVICE TEAMS Side-by-Side Support Chemical Management Services...Marine Corps ordnance technicians load a missile at Kunsan Air Base, South Korea. Service members from the different military branches often work
1968-12-02
S68-51306 (December 1968) --- North American Rockwell artist's concept illustrating a phase of the scheduled Apollo 8 lunar orbit mission. Here, the Apollo 8 spacecraft lunar module adapter (SLA) panels, which have supported the Command and Service Modules, are jettisoned. This is done by astronauts firing the service module reaction control engines. A signal simultaneously deploys and jettisons the panels, separating the spacecraft from the SLA and deploying the high gain (deep space) antenna.
Williams with TVIS hardware in Zvezda Service module
2007-02-27
ISS014-E-15349 (27 Feb. 2007) --- Assisted by the weightlessness of space, astronaut Sunita L. Williams, Expedition 14 flight engineer, hoists the Treadmill Vibration Isolation System (TVIS). She took a moment to pose for a photo during routine in-flight maintenance (IFM) on TVIS in the Zvezda Service Module of the International Space Station.
Barratt during Soyuz descent training in Service Module
2009-07-06
ISS020-E-017368 (6 July 2009) --- NASA astronaut Michael Barratt, Expedition 20 flight engineer, uses a computer at the TORU teleoperated control system in the Zvezda Service Module of the International Space Station while conducting Soyuz descent training to maintain proficiency on systems used for entry and landing in the Soyuz vehicle.
Orion Service Module Reaction Control System Plume Impingement Analysis Using PLIMP/RAMP2
NASA Technical Reports Server (NTRS)
Wang, Xiao-Yen; Lumpkin, Forrest E., III; Gati, Frank; Yuko, James R.; Motil, Brian J.
2009-01-01
The Orion Crew Exploration Vehicle Service Module Reaction Control System engine plume impingement was computed using the plume impingement program (PLIMP). PLIMP uses the plume solution from RAMP2, which is the refined version of the reacting and multiphase program (RAMP) code. The heating rate and pressure (force and moment) on surfaces or components of the Service Module were computed. The RAMP2 solution of the flow field inside the engine and the plume was compared with those computed using GASP, a computational fluid dynamics code, showing reasonable agreement. The computed heating rate and pressure using PLIMP were compared with the Reaction Control System plume model (RPM) solution and the plume impingement dynamics (PIDYN) solution. RPM uses the GASP-based plume solution, whereas PIDYN uses the SCARF plume solution. Three sets of the heating rate and pressure solutions agree well. Further thermal analysis on the avionic ring of the Service Module was performed using MSC Patran/Pthermal. The obtained temperature results showed that thermal protection is necessary because of significant heating from the plume.
ARTIST CONCEPT - APOLLO XI - LUNAR SURFACE
1969-07-11
S69-39011 (July 1969) --- TRW Incorporated's artist concept depicting the Apollo 11 Lunar Module (LM) descending to the surface of the moon. Inside the LM will be astronauts Neil A. Armstrong, commander, and Edwin E. Aldrin Jr., lunar module pilot. Astronaut Michael Collins, command module pilot, will remain with the Command and Service Modules (CSM) in lunar orbit. TRW's LM descent engine will brake Apollo 11's descent to the lunar surface. The throttle-able rocket engine will be fired continuously the last 10 miles of the journey to the moon, slowing the LM to a speed of two miles per hour at touchdown. TRW Incorporated designed and built the unique engine at Redondo Beach, California under subcontract to the Grumman Aircraft Engineering Corporation, Bethpage, New York, the LM prime contractor.
Thermal Analysis on Plume Heating of the Main Engine on the Crew Exploration Vehicle Service Module
NASA Technical Reports Server (NTRS)
Wang, Xiao-Yen J.; Yuko, James R.
2007-01-01
The crew exploration vehicle (CEV) service module (SM) main engine plume heating is analyzed using multiple numerical tools. The chemical equilibrium compositions and applications (CEA) code is used to compute the flow field inside the engine nozzle. The plume expansion into ambient atmosphere is simulated using an axisymmetric space-time conservation element and solution element (CE/SE) Euler code, a computational fluid dynamics (CFD) software. The thermal analysis including both convection and radiation heat transfers from the hot gas inside the engine nozzle and gas radiation from the plume is performed using Thermal Desktop. Three SM configurations, Lockheed Martin (LM) designed 604, 605, and 606 configurations, are considered. Design of multilayer insulation (MLI) for the stowed solar arrays, which is subject to plume heating from the main engine, among the passive thermal control system (PTCS), are proposed and validated.
Reiter cuts Tyurins hair in the Zvezda Service module
2006-11-05
ISS014-E-07174 (5 Nov. 2006) --- European Space Agency (ESA) astronaut Thomas Reiter, Expedition 14 flight engineer, cuts the hair of cosmonaut Mikhail Tyurin, flight engineer representing Russia's Federal Space Agency, in the Unity node of the International Space Station. Reiter used hair clippers fashioned with a vacuum device to prevent freshly cut hair from being scattered throughout the module.
Voss with video camera in Service Module
2001-04-08
ISS002-E-5329 (08 April 2001) --- Astronaut James S. Voss, Expedition Two flight engineer, sets up a video camera on a mounting bracket in the Zvezda / Service Module of the International Space Station (ISS). A 35mm camera and a digital still camera are also visible nearby. This image was recorded with a digital still camera.
2001-03-31
ISS002-E-5084 (31 March 2001) --- Astronaut James S. Voss, Expedition Two flight engineer, floats in the Zvezda Service Module onboard the International Space Station (ISS). Voss, along with astronaut Susan J. Helms and cosmonaut Yury V. Usachev of Rosaviakosmos, recently replaced the initial three-member crew onboard the orbital outpost. The image was taken with a digital still camera.
2006-11-03
ISS014-E-07138 (3 Nov. 2006) --- Cosmonaut Mikhail Tyurin, Expedition 14 flight engineer representing Russia's Federal Space Agency, installs and connects onboard equipment control system cables in the Zvezda Service Module of the International Space Station.
Servicers system demonstration plan and capability development
NASA Technical Reports Server (NTRS)
Bulboaca, M. A.; Cuseo, J. A.; Derocher, W. L., Jr.; Maples, R. W.; Reynolds, P. C.; Sterrett, R. A.
1985-01-01
A plan for the demonstration of the exchange of Multi-Mission Modular Spacecraft (MMS) modules using the servicer mechanism Engineering Test Unit (ETU) was prepared and executed. The plan included: establishment of requirements, conceptual design, selection of MMS spacecraft mockup configuration, selection of MMS module mockup configuration, evaluation of adequacy of ETU load capability, and selection of a stowage rack arrangement. The MMS module exchange demonstration mockup equipment was designed, fabricated, checked out, shipped, installed, and demonstrated.
Short-term performance deterioration in JT9D-7A(SP) engine 695743
NASA Technical Reports Server (NTRS)
Bouchard, R. J.; Beyerly, W. R.; Sallee, G. P.
1978-01-01
The level of performance deterioration that occurred during early service was studied and also the contribution of each engine module to the overall level of engine performance deterioration. To assist in the distribution of the performance losses to the module level, testing with expanded experimental instrumentation was accomplished to permit direct measurement of module performance. An analytical teardown of the engine was accomplished to permit assignment of module performance losses to individual mechanical damage mechanisms including blade and seal wear, roughness, and thermal distortion of turbine parts. The results of the testing show that the engine deteriorated 1.5 percent in thrust specific fuel consumption from its performance when new. Initial testing, which included water washing, showed that 0.2 percent in performance deterioration was due to surface contamination (dirt) and 0.1 percent was due to drift of the engine vane control system, leaving 1.2 percent in basic TSFC deterioration. This 1.2 percent TSFC loss was distributed among the engine modules with 0.6 percent caused by clearance changes, 0.4 percent loss due to thermal distortion, and 0.2 percent loss due to increased roughness of the fan and low-pressure compressor airfoils.
Aerospace Engineer Lizalyn Smith
2017-01-09
Portrait of Orion Service Module Spacecraft Adapter Jettisonable (SAJ) Hardware Lead Engineer Lizalyn Smith. Ms. Smith participated in various 'Hidden Figures to Modern Figures' events sponsored by NASA Glenn Research Center to encourage students to pursue STEM-based careers.
View of damaged Apollo 13 Service Module from the Lunar/Command Modules
1970-04-17
This view of the damaged Apollo 13 Service Module (SM) was photographed from the Lunar Module/Command Module following SM jettisoning. As seen here, an entire panel on the SM was blown away by the apparent explosion of oxygen tank number two located in Sector 4 of the SM. Two of the three fuel cells are visible just forward (above) the heavily damaged area. Three fuel cells, two oxygen tanks, and two hydrogen tanks are locate in Sector 4. The damaged area is located above the S-band high gain antenna. Nearest the camera is the Service Propulsion System (SPS) engine and nozzle. The damage to the SM caused the Apollo 13 crewmen to use the Lunar Module (LM) as a "lifeboat". The LM was jettisoned just prior to Earth reentry by the Command Module.
Haignere works in the Service Module during Expedition Three
2001-10-23
ISS003-E-6855 (23-31 October 2001) --- French Flight Engineer Claudie Haignere, works in the Zvezda Service Module on the International Space Station (ISS). Haignere represents ESA, carrying out a flight program for CNES, the French Space Agency, under a commercial contract with the Russian Aviation and Space Agency. This image was taken with a digital still camera.
ERIC Educational Resources Information Center
White, Debi; And Others
This instructional package, one of two designed for low reader-educable mentally impaired students, focuses on the vocational area of small engine repair service. (Low readers are identified as those at a reading level of grades 3-6.) Contained in this document are fifty learning modules organized into twelve units: sharpening and grinding mowers;…
Phillips with probe-and-cone docking mechanism (StM) in the Zvezda module
2005-06-19
ISS011-E-09205 (19 June 2005) --- Astronaut John L. Phillips, Expedition 11 NASA ISS science officer and flight engineer, works on the dismantled probe-and-cone docking mechanism from the Progress 18 spacecraft in the Zvezda Service Module of the International Space Station (ISS). The Progress docked to the aft port of the Service Module at 7:42 p.m. (CDT) as the two spacecraft flew approximately 225 statute miles, above a point near Beijing, China.
Romanenko looks through a Rodnik Tank in the SM
2012-12-31
ISS034-E-010446 (31 Dec. 2012) --- Russian cosmonaut Roman Romanenko, Expedition 34 flight engineer, looks through a Rodnik tank in the Zvezda Service Module of the International Space Station. Romanenko performed a water transfer from a Rodnik tank in the Progress to a Rodnik tank in the Zvezda Service Module. Note the multiple refractions of the cosmonaut?s head and shoulders in the bubbles.
Voss with globe in Service module
2001-04-08
ISS002-E-5136 (8 April 2001) --- Astronaut James S. Voss, Expedition Two flight engineer, holds a globe to be used for assistance in Earth observation duties. Voss is in the Zvezda Service Module aboard the International Space Station (ISS), where's he been working for several weeks along with cosmonaut Yury V. Usachev of Rosaviakosmos and astronaut Susan J. Helms. The image was recorded with a digital still camera.
2008-10-15
ISS017-E-018411 (15 Oct. 2008) --- Russian Federal Space Agency cosmonaut Yury Lonchakov, Expedition 18 flight engineer, looks over a procedures checklist while holding Space Science P/L Crystallizer Module-1 experiment hardware in the Zvezda Service Module of the International Space Station.
1967-03-01
The Saturn V configuration is shown in inches and meters as illustrated by the Boeing Company. The Saturn V vehicle consisted of three stages: the S-IC (first) stage powered by five F-1 engines, the S-II (second) stage powered by five J-2 engines, the S-IVB (third) stage powered by one J-2 engine. A top for the first three stages was designed to contain the instrument unit, the guidance system, the Apollo spacecraft, and the escape system. The Apollo spacecraft consisted of the lunar module, the service module, and the command module. The Saturn V was designed perform lunar and planetary missions and it was capable of placing 280,000 pounds into Earth orbit.
Crew Training - Apollo 9 - Grumman Aircraft Eng. Corp. (GAEC)
1969-01-25
S69-17615 (25 Jan. 1969) --- Astronaut Russell L. Schweickart, lunar module pilot of the Apollo 9 prime crew, participates in a press conference at the Grumman Aircraft Engineering Corporation. Grumman is the contractor to NASA for the Lunar Module. Schweickart is holding a model of a docked Lunar Module/Command and Service Modules. The Apollo 9 mission will evaluate spacecraft lunar module systems performance during manned Earth-orbital flight.
Wakata haircut in the Service Module (SM)
2009-04-04
ISS018-E-044607 (4 April 2009) --- Japan Aerospace Exploration Agency (JAXA) astronaut Koichi Wakata, Expedition 18/19 flight engineer, returns scissors and hair clippers to their storage bag after trimming his hair in the Zarya module of the International Space Station.
Voss on TVIS equipment in Zvezda module
2001-05-15
ISS002-E-06677 (15 May 2001) --- James S. Voss, Expedition Two flight engineer, wearing a safety harness, exercises on the Treadmill Vibration Isolation System (TVIS) equipment in the Zvezda Service Module. This image was taken with a digital still camera.
Kononenko uses laptop computer in the SM Transfer Compartment
2012-03-21
ISS030-E-161167 (21 March 2012) --- Russian cosmonaut Oleg Kononenko, Expedition 30 flight engineer, uses a computer in the transfer compartment of the International Space Station?s Zvezda Service Module. Russia's Zarya module is visible in the background.
Orion Service Module Umbilical (OSMU) Testing Complete
2016-10-19
Testing of the Orion Service Module Umbilical (OSMU) was completed at the Launch Equipment Test Facility at NASA’s Kennedy Space Center in Florida. The OSMU was attached to Vehicle Motion Simulator 1 for a series of simulated launch tests to validate it for installation on the mobile launcher. Patrick Simpkins, director of Engineering, speaks to the test team during an event to mark the end of testing. The mobile launcher tower will be equipped with a number of lines, called umbilicals that will connect to the Space Launch System rocket and Orion spacecraft for Exploration Mission-1 (EM-1). The OSMU will be located high on the mobile launcher tower and, prior to launch, will transfer liquid coolant for the electronics and air for the Environmental Control System to the Orion service module that houses these critical systems to support the spacecraft. Kennedy's Engineering Directorate is providing support to the Ground Systems Development and Operations Program for testing of the OSMU. EM-1 is scheduled to launch in 2018.
Consideration of adding a commercial module to the International Space Station
NASA Astrophysics Data System (ADS)
Friefeld, J.; Fugleberg, D.; Patel, J.; Subbaraman, G.
1999-01-01
The National Aeronautics and Space Administration (NASA) is currently assembling the International Space Station in Low Earth Orbit. One of NASA's program objectives is to encourage space commercialization. Through NASA's Engineering Research and Technology Development program, Boeing is conducting a study to ascertain the feasibility of adding a commercial module to the International Space Station. This module (facility) that can be added, following on-orbit assembly is described. The facility would have the capability to test large, engineering scale payloads in a space environment. It would also have the capability to provide services to co-orbiting space vehicles as well as gathering data for commercial terrestrial applications. The types of industries to be serviced are described as are some of the technical and business considerations that need to be addressed in order to achieve commercial viability.
Wakata haircut in the Service Module (SM)
2009-04-04
ISS018-E-044602 (4 April 2009) --- Japan Aerospace Exploration Agency (JAXA) astronaut Koichi Wakata, Expedition 18/19 flight engineer, trims his hair in the Zarya module of the International Space Station, using scissors and a vacuum device to garner freshly cut hair.
Tyurin gives Culbertson a haircut in the Service Module during Expedition Three
2001-09-22
ISS003-E-5901 (22 September 2001) --- Astronaut Frank L. Culbertson, Jr. (right), Expedition Three mission commander, holds a vacuum device the crew has fashioned to garner freshly cut hair floating freely, as Mikhail Tyurin cuts his hair in the Zvezda Service Module on the International Space Station (ISS). Tyurin is a flight engineer representing Rosaviakosmos. This image was taken with a digital still camera.
Tyurin gives Dezhurov a haircut in the Service Module during Expedition Three
2001-09-22
ISS003-E-5891 (22 September 2001) --- Cosmonauts Mikhail Tyurin (left) and Vladimir N. Dezhurov, Expedition Three flight engineers representing Rosaviakosmos, take turns cutting each others hair in the Zvezda Service Module on the International Space Station (ISS). Dezhurov holds a vacuum device the crew has fashioned to garner freshly cut hair floating freely. This image was taken with a digital still camera.
Tyurin gives Culbertson a haircut in the Service Module during Expedition Three
2001-09-22
ISS003-E-5896 (22 September 2001) --- Astronaut Frank L. Culbertson, Jr. (right), Expedition Three mission commander, holds a vacuum device the crew has fashioned to garner freshly cut hair floating freely, as Mikhail Tyurin cuts his hair in the Zvezda Service Module on the International Space Station (ISS). Tyurin is a flight engineer representing Rosaviakosmos. This image was taken with a digital still camera.
MATRYOSHKA-R (RBO-3-2) Radiation Suite in the Service Module (SM)
2009-03-14
ISS018-E-040944 (18 March 2009) --- Cosmonaut Yury Lonchakov, Expedition 18 flight engineer, works with the European Matroshka-R Phantom experiment in the Zvezda Service Module of the International Space Station while Space Shuttle Discovery (STS-119) remains docked with the station. Matroshka, the name for the traditional Russian set of nestling dolls, is an antroph-amorphous model of a human torso designed for radiation studies.
MATRYOSHKA-R (RBO-3-2) radiation suite in service module (SM)
2009-03-18
ISS018-E-040992 (18 March 2009) --- Cosmonaut Yury Lonchakov, Expedition 18 flight engineer, works with the European Matroshka-R Phantom experiment in the Zvezda Service Module of the International Space Station while Space Shuttle Discovery (STS-119) remains docked with the station. Matroshka, the name for the traditional Russian set of nestling dolls, is an antroph-amorphous model of a human torso designed for radiation studies.
Performance deterioration based on existing (historical) data; JT9D jet engine diagnostics program
NASA Technical Reports Server (NTRS)
Sallee, G. P.
1978-01-01
The results of the collection and analysis of historical data pertaining to the deterioration of JT9D engine performance are presented. The results of analyses of prerepair and postrepair engine test stand performance data from a number of airlines to establish the individual as well as average losses in engine performance with respect to service use are included. Analysis of the changes in mechanical condition of parts, obtained by inspection of used gas-path parts of varying age, allowed preliminary assessments of component performance deterioration levels and identification of the causitive factors. These component performance estimates, refined by data from special engine back-to-back testing related to module performance restoration, permitted the development of preliminary models of engine component/module performance deterioration with respect to usage. The preliminary assessment of the causes of module performance deterioration and the trends with usage are explained, along with the role each module plays in overall engine performance deterioration. Preliminary recommendations with respect to operating and maintenance practices which could be adopted to control the level of performance deterioration are presented. The needs for additional component sensitivity testing as well as outstanding issues are discussed.
Wakata haircut in the Service Module (SM)
2009-04-04
ISS018-E-044596 (4 April 2009) --- Japan Aerospace Exploration Agency (JAXA) astronaut Koichi Wakata, Expedition 18/19 flight engineer, trims his hair in the Zarya module of the International Space Station, using hair clippers fashioned with a vacuum device to garner freshly cut hair.
Small Engine Repair Modules (Workbook) = Reparacion de Motores Pequenos (Guia de Trabajo)
ERIC Educational Resources Information Center
New York State Dept. of Correctional Services, Albany.
This package contains an English-Language set of task procedure sheets dealing with small-engine repair and a Spanish translation of the same material. Addressed in the individual sections of the manual are the following aspects of engine tune-up, reconditioning, and troubleshooting: servicing air cleaners; cleaning gas tanks, fuel lines, and fuel…
NASA Technical Reports Server (NTRS)
Li, Chung-Sheng (Inventor); Smith, John R. (Inventor); Chang, Yuan-Chi (Inventor); Jhingran, Anant D. (Inventor); Padmanabhan, Sriram K. (Inventor); Hsiao, Hui-I (Inventor); Choy, David Mun-Hien (Inventor); Lin, Jy-Jine James (Inventor); Fuh, Gene Y. C. (Inventor); Williams, Robin (Inventor)
2004-01-01
Methods and apparatus for providing a multi-tier object-relational database architecture are disclosed. In one illustrative embodiment of the present invention, a multi-tier database architecture comprises an object-relational database engine as a top tier, one or more domain-specific extension modules as a bottom tier, and one or more universal extension modules as a middle tier. The individual extension modules of the bottom tier operationally connect with the one or more universal extension modules which, themselves, operationally connect with the database engine. The domain-specific extension modules preferably provide such functions as search, index, and retrieval services of images, video, audio, time series, web pages, text, XML, spatial data, etc. The domain-specific extension modules may include one or more IBM DB2 extenders, Oracle data cartridges and/or Informix datablades, although other domain-specific extension modules may be used.
Flight Engineer Budarin uses a laptop computer in the SM during Expedition Six
2003-03-21
ISS006-E-45279 (21 March 2003) --- Cosmonaut Nikolai M. Budarin, Expedition Six flight engineer, uses a computer as he talks on a communication system in the Zvezda Service Module on the International Space Station (ISS). Budarin represents Rosaviakosmos.
Flight Engineer Budarin is changing a part in the water recycling system in the SM
2003-03-21
ISS006-E-45275 (21 March 2003) --- Cosmonaut Nikolai M. Budarin, Expedition Six flight engineer, holds a piece of hardware near a worktable in the Zvezda Service Module on the International Space Station (ISS). Budarin represents Rosaviakosmos.
MATRYOSHKA-R (RBO-3-2) Radiation Suite in the Service Module (SM)
2009-03-14
ISS018-E-040939 (18 March 2009) --- Cosmonaut Yury Lonchakov, Expedition 18 flight engineer, prepares to work with the European Matroshka-R Phantom experiment in the Zvezda Service Module of the International Space Station while Space Shuttle Discovery (STS-119) remains docked with the station. Matroshka, the name for the traditional Russian set of nestling dolls, is an antroph-amorphous model of a human torso designed for radiation studies.
Culbertson and Haignere work in the Service Module during Expedition Three
2001-10-23
ISS003-E-6854 (23-31 October 2001) --- Astronaut Frank L. Culbertson, Jr. (left), Expedition Three mission commander, and French Flight Engineer Claudie Haignere, work in the Zvezda Service Module on the International Space Station (ISS). Haignere represents ESA, carrying out a flight program for CNES, the French Space Agency, under a commercial contract with the Russian Aviation and Space Agency. This image was taken with a digital still camera.
Kotov works with Plasma Crystal-3 Experiment in the SM during Expedition 22
2010-01-25
ISS022-E-035438 (25 Jan. 2010) --- Russian cosmonaut Oleg Kotov, Expedition 22 flight engineer, uses a computer while servicing the Plasma Crystal-3 experiment in the Zvezda Service Module of the International Space Station.
Kotov works with Plasma Crystal-3+ Experiment in the SM during Expedition 22
2010-01-28
ISS022-E-040615 (28 Jan. 2010) --- Russian cosmonaut Oleg Kotov, Expedition 22 flight engineer, uses a computer while servicing the Plasma Crystal-3 experiment in the Zvezda Service Module of the International Space Station.
The Apollo spacecraft: A chronology, volume 3, 1 October 1964 - 20 January 1966
NASA Technical Reports Server (NTRS)
Brooks, C. G.; Ertel, I. D.
1976-01-01
The development of the Apollo spacecraft is traced along with that of Saturn V. Emphasis is placed on the detailed engineering design and exhaustive testing performed to qualify both the command and service modules and the lunar module for manned flight.
Tyurin and Reiter in the Zvezda Module
2006-11-03
ISS014-E-07142 (3 Nov. 2006) --- Cosmonaut Mikhail Tyurin (foreground) representing Russia's Federal Space Agency, and European Space Agency (ESA) astronaut Thomas Reiter, both Expedition 14 flight engineers, install and connect onboard equipment control system cables in the Zvezda Service Module of the International Space Station.
Applied Physics Modules Selected for Electrical and Electronic Technologies.
ERIC Educational Resources Information Center
Waring, Gene
Designed for individualized use in an applied physics course in postsecondary vocational-technical education, this series of twenty-three learning modules is equivalent to the content of two quarters of a five-credit hour class in electrical technology, electronic service technology, electronic engineering technology, or electromechanical…
Successful MPPF Pneumatics Verification and Validation Testing
2017-03-28
Engineers and technicians completed verification and validation testing of several pneumatic systems inside and outside the Multi-Payload Processing Facility (MPPF) at NASA's Kennedy Space Center in Florida. In view is the service platform for Orion spacecraft processing. The MPPF will be used for offline processing and fueling of the Orion spacecraft and service module stack before launch. Orion also will be de-serviced in the MPPF after a mission. The Ground Systems Development and Operations Program (GSDO) is overseeing upgrades to the facility. The Engineering Directorate led the recent pneumatic tests.
Successful MPPF Pneumatics Verification and Validation Testing
2017-03-28
Engineers and technicians completed verification and validation testing of several pneumatic systems inside and outside the Multi-Payload Processing Facility (MPPF) at NASA's Kennedy Space Center in Florida. In view is the top level of the service platform for Orion spacecraft processing. The MPPF will be used for offline processing and fueling of the Orion spacecraft and service module stack before launch. Orion also will be de-serviced in the MPPF after a mission. The Ground Systems Development and Operations Program (GSDO) is overseeing upgrades to the facility. The Engineering Directorate led the recent pneumatic tests.
78 FR 23231 - 36(b)(1) Arms Sales Notification
Federal Register 2010, 2011, 2012, 2013, 2014
2013-04-18
...) Description and Quantity or Quantities of Articles or Services under Consideration for Purchase: 60 Active... equipment items, GEM-V GPS airborne receiver module, and communication security, software development... documents, U.S. Government and contract engineering and logistical personnel services, and other related...
View of damaged Apollo 13 Service Module from the Lunar/Command Modules
1970-04-17
AS13-59-8501 (17 April 1970) --- This view of the severely damaged Apollo 13 Service Module (SM) was photographed from the Lunar Module/Command Module (LM/CM) following SM jettisoning. As seen here, an entire panel on the SM was blown away by the apparent explosion of oxygen tank number two located in Sector 4 of the SM. Two of the three fuel cells are visible just forward (above) the heavily damaged area. Three fuel cells, two oxygen tanks, and two hydrogen tanks are located in Sector 4. The damaged area is located above the S-Band high gain antenna. Nearest the camera is the Service Propulsion System (SPS) engine and nozzle. The damage to the SM caused the Apollo 13 crew men to use the LM as a "lifeboat." The LM was jettisoned just prior to Earth re-entry by the CM.
AUTOMOTIVE DIESEL MAINTENANCE 2. UNIT XX, TROUBLESHOOTING ELECTRICAL SYSTEMS.
ERIC Educational Resources Information Center
Minnesota State Dept. of Education, St. Paul. Div. of Vocational and Technical Education.
THIS MODULE OF A 25-MODULE COURSE IS DESIGNED TO ACQUAINT THE TRAINEE WITH TROUBLESHOOTING PROCEDURES FOR DIESEL ENGINE ELECTRICAL SYSTEMS. TOPICS ARE (1) TROUBLESHOOTING ELECTRICAL SYSTEMS (INTRODUCTION), (2) TOOLS AND INSTRUMENTS FOR TROUBLESHOOTING, (3) THE BATTERY, (4) PERIODIC BATTERY SERVICING, (5) THE DC CHARGING SYSTEM, (6) PERIODIC…
Diesel Fundamentals. Teacher Edition (Revised).
ERIC Educational Resources Information Center
Clark, Elton; And Others
This module is one of a series of teaching guides that cover diesel mechanics. The module contains 4 sections and 19 units. Section A--Orientation includes the following units: introduction to diesel mechanics and shop safety; basic shop tools; test equipment and service tools; fasteners; bearings; and seals. Section B--Engine Principles and…
Swanson uses the BMMD in the SM
2014-03-31
ISS039-E-008066 (30 March 2014) --- NASA astronaut Steve Swanson, Expedition 39 flight engineer, participates in body mass measurement/Russian biomedical routine assessments in the Zvezda Service Module of the International Space Station. Looking on is Russian cosmonaut Alexander Skvortsov, flight engineer representing the Russian Federal Space Agency (Roscosmos).
NASA Technical Reports Server (NTRS)
Ascoli, Peter A.; Haddock, Michael H.
2014-01-01
An Orion Crew Module Service Module Structural Weight and Center of Gravity Simulator and a Vehicle Motion Simulator Hoist Structure for Orion Service Module Umbilical Testing were designed during a summer 2014 internship in Kennedy Space Centers Structures and Mechanisms Design Branch. The simulator is a structure that supports ballast, which will be integrated into an existing Orion mock-up to simulate the mass properties of the Exploration Mission-1 flight vehicle in both fueled and unfueled states. The simulator mimics these configurations through the use of approximately 40,000 lbf of steel and water ballast, and a steel support structure. Draining four water tanks, which house the water ballast, transitions the simulator from the fueled to unfueled mass properties. The Ground Systems Development and Operations organization will utilize the simulator to verify and validate equipment used to maneuver and transport the Orion spacecraft in its fueled and unfueled configurations. The second design comprises a cantilevered tripod hoist structure that provides the capability to position a large Orion Service Module Umbilical in proximity to the Vehicle Motion Simulator. The Ground Systems Development and Operations organization will utilize the Vehicle Motion Simulator, with the hoist structure attached, to test the Orion Service Module Umbilical for proper operation prior to installation on the Mobile Launcher. Overall, these two designs provide NASA engineers viable concepts worthy of fabricating and placing into service to prepare for the launch of Orion in 2017.
FSS (Fluid Servicer System) from the Kibo module to the ESA COL
2009-07-08
ISS020-E-017933 (8 July 2009) --- Japan Aerospace Exploration Agency (JAXA) astronaut Koichi Wakata, Expedition 20 flight engineer, works with the Fluid Servicing System (FSS) and the Fluid Control Pump Assembly (FCPA) in the Columbus laboratory of the International Space Station.
Progress 23 supply vehicle approach
2006-10-26
ISS014-E-06544 (26 Oct. 2006) --- Backdropped by a blue and white Earth, an unpiloted Progress supply vehicle approaches the International Space Station. Progress docked to the aft port of the Zvezda Service Module at 9:29 a.m. (CDT) on Oct. 26. The spacecraft used the automated Kurs system to dock at the aft port of the Zvezda service module. Expedition 14 flight engineer Mikhail Tyurin stood by at the manual Toru docking system controls, but the automated system functioned as designed and manual intervention was not needed.
Web-based Traffic Noise Control Support System for Sustainable Transportation
NASA Astrophysics Data System (ADS)
Fan, Lisa; Dai, Liming; Li, Anson
Traffic noise is considered as one of the major pollutions that will affect our communities in the future. This paper presents a framework of web-based traffic noise control support system (WTNCSS) for a sustainable transportation. WTNCSS is to provide the decision makers, engineers and publics a platform to efficiently access the information, and effectively making decisions related to traffic control. The system is based on a Service Oriented Architecture (SOA) which takes the advantages of the convenience of World Wide Web system with the data format of XML. The whole system is divided into different modules such as the prediction module, ontology-based expert module and dynamic online survey module. Each module of the system provides a distinct information service to the decision support center through the HTTP protocol.
Successful MPPF Pneumatics Verification and Validation Testing
2017-03-28
Engineers and technicians completed verification and validation testing of several pneumatic systems inside and outside the Multi-Payload Processing Facility (MPPF) at NASA's Kennedy Space Center in Florida. In view is the service platform for Orion spacecraft processing. To the left are several pneumatic panels. The MPPF will be used for offline processing and fueling of the Orion spacecraft and service module stack before launch. Orion also will be de-serviced in the MPPF after a mission. The Ground Systems Development and Operations Program (GSDO) is overseeing upgrades to the facility. The Engineering Directorate led the recent pneumatic tests.
1969-01-01
A close-up view of the Apollo 11 command service module ready to be mated with the spacecraft LEM adapter of the third stage. The towering 363-foot Saturn V was a multi-stage, multi-engine launch vehicle standing taller than the Statue of Liberty. Altogether, the Saturn V engines produced as much power as 85 Hoover Dams.
Curricular Improvements through Computation and Experiment Based Learning Modules
ERIC Educational Resources Information Center
Khan, Fazeel; Singh, Kumar
2015-01-01
Engineers often need to predict how a part, mechanism or machine will perform in service, and this insight is typically achieved thorough computer simulations. Therefore, instruction in the creation and application of simulation models is essential for aspiring engineers. The purpose of this project was to develop a unified approach to teaching…
1970-04-17
AS13-59-8500A (17 April 1970) --- This view of the severely damaged Apollo 13 Service Module (SM) was photographed from the Lunar Module/Command Module (LM/CM) following SM jettisoning. As seen in this cropped image, enlarged to provide a close-up view of the damaged area, an entire panel on the SM was blown away by the apparent explosion of oxygen tank number two located in Sector 4 of the SM. Two of the three fuel cells are visible just forward (above) the heavily damaged area. Three fuel cells, two oxygen tanks, and two hydrogen tanks are located in Sector 4. The damaged area is located above the S-Band high gain antenna. Nearest the camera is the Service Propulsion System (SPS) engine and nozzle. The damage to the SM caused the Apollo 13 crew members to use the LM as a "lifeboat". The LM was jettisoned just prior to Earth re-entry by the CM. Photo credit: NASA
Barratt during 33P Progress unpacking
2009-05-13
ISS019-E-016480 (13 May 2009) --- Astronaut Michael Barratt, Expedition 19/20 flight engineer, is pictured near a tomato floating freely in the Zvezda Service Module of the International Space Station.
2006-10-01
ISS014-E-05962 (October 2006) --- European Space Agency (ESA) astronaut Thomas Reiter, Expedition 14 flight engineer, wears a communication system headset while using a computer in the Zvezda Service Module of the International Space Station.
Tyurin in Zvezda with communication system
2007-02-24
ISS014-E-14765 (24 Feb. 2007) --- Cosmonaut Mikhail Tyurin, Expedition 14 flight engineer representing Russia's Federal Space Agency, uses a communication system in the Zvezda Service Module of the International Space Station.
Skripochka and Kaleri watch monitor
2011-03-04
ISS026-E-031766 (4 March 2011) --- Russian cosmonauts Oleg Skripochka (foreground) and Alexander Kaleri, both Expedition 26 flight engineers, watch a computer monitor in the Zvezda Service Module of the International Space Station.
2013-06-24
View of Russian cosmonaut Alexander Misurkin (bottom center), Expedition 36 flight engineer, participating in Russian extravehicular activity (EVA) 33. Also visible are the Progress spacecraft docked to the Pirs Docking Compartment (DC1) with the Service Module (SM) .
2009-08-28
ISS020-E-035022 (27 Aug. 2009) --- Russian cosmonaut Roman Romanenko, Expedition 20 flight engineer, uses the Russian BAR/EXPERT science payload to take various environmental measurements in the Zvezda Service Module of the International Space Station.
Kuipers near food containers in the SM
2012-03-28
ISS030-E-178069 (28 March 2012) --- European Space Agency astronaut Andre Kuipers, Expedition 30 flight engineer, is pictured near food storage containers in the Zvezda Service Module of the International Space Station.
Shkaplerov makes a selection from food container
2012-02-03
ISS030-E-117514 (3 Feb. 2012) --- Russian cosmonaut Anton Shkaplerov, Expedition 30 flight engineer, makes a selection from a food storage container in the Zvezda Service Module of the International Space Station.
Barrett during TVIS maintenance
2009-04-21
ISS019-E-008750 (21 April 2009) --- Astronaut Michael Barratt, Expedition 19/20 flight engineer, performs in-flight maintenance on the Treadmill Vibration Isolation System (TVIS) in the Zvezda Service Module of the International Space Station.
Barrett during TVIS maintenance
2009-04-21
ISS019-E-008752 (21 April 2009) --- Astronaut Michael Barratt, Expedition 19/20 flight engineer, performs in-flight maintenance on the Treadmill Vibration Isolation System (TVIS) in the Zvezda Service Module of the International Space Station.
Barrett during TVIS maintenance
2009-04-21
ISS019-E-008767 (21 April 2009) --- Astronaut Michael Barratt, Expedition 19/20 flight engineer, performs in-flight maintenance on the Treadmill Vibration Isolation System (TVIS) in the Zvezda Service Module of the International Space Station.
Barrett during TVIS maintenance
2009-04-21
ISS019-E-008764 (21 April 2009) --- Astronaut Michael Barratt, Expedition 19/20 flight engineer, performs in-flight maintenance on the Treadmill Vibration Isolation System (TVIS) in the Zvezda Service Module of the International Space Station.
Nespoli services the FCF in the US Lab
2011-04-21
ISS027-E-014888 (21 April 2011) --- European Space Agency astronaut Paolo Nespoli, Expedition 27 flight engineer, works with the Light Microscopy Module (LMM) in the Destiny laboratory of the International Space Station.
Nespoli services the FCF in the US Lab
2011-04-21
ISS027-E-014895 (21 April 2011) --- European Space Agency astronaut Paolo Nespoli, Expedition 27 flight engineer, works with the Light Microscopy Module (LMM) in the Destiny laboratory of the International Space Station.
Nespoli services the FCF in the US Lab
2011-04-21
ISS027-E-014894 (21 April 2011) --- European Space Agency astronaut Paolo Nespoli, Expedition 27 flight engineer, works with the Light Microscopy Module (LMM) in the Destiny laboratory of the International Space Station.
Whitson cuts Treschev's hair in the SM during Expedition Five on the ISS
2002-07-20
ISS005-E-08151 (July 2002) --- Astronaut Peggy A. Whitson, Expedition Five flight engineer, cuts cosmonaut Sergei Y. Treschevs hair in the Zvezda Service Module on the International Space Station (ISS). Treschev, flight engineer representing Rosaviakosmos, holds a vacuum device the crew has fashioned to garner freshly cut hair, which is floating freely.
Dezhurov removes the docking probe in Zvezda during Expedition Three
2001-09-17
ISS003-E-5621 (17 September 2001) --- Cosmonaut Vladimir Dezhurov, Expedition Three flight engineer, prepares to remove the docking probe in the Zvezda Service Module's pressurized adapter. The docking probe successfully guided the arrival of the Russian-built Pirs docking compartment to the International Space Station (ISS). Mikhail Tyurin, flight engineer, is visible in the background. Tyurin and Dezhurov represent Rosaviakosmos.
Reiter working in SM during Expedition 13
2006-08-19
ISS013-E-67495 (19 Aug. 2006) --- European Space Agency (ESA) astronaut Thomas Reiter, Expedition 13 flight engineer, wears a communication system while using a computer in the Zvezda Service Module of the International Space Station.
Ivanishin wearing a communication system headset in the SM
2012-01-05
ISS030-E-021036 (5 Jan. 2012) --- Russian cosmonaut Anatoly Ivanishin, Expedition 30 flight engineer, wears a communication system headset while using a computer in the Zvezda Service Module of the International Space Station.
Malenchenko uses communication equipment in the SM
2008-01-09
ISS016-E-022130 (9 Jan. 2008) --- Cosmonaut Yuri I. Malenchenko, Expedition 16 flight engineer representing Russia's Federal Space Agency, uses a communication system while working in the Zvezda Service Module of the International Space Station.
Malenchenko uses communication equipment in the SM
2008-01-09
ISS016-E-022134 (9 Jan. 2008) --- Cosmonaut Yuri I. Malenchenko, Expedition 16 flight engineer representing Russia's Federal Space Agency, uses a communication system while working in the Zvezda Service Module of the International Space Station.
Wakata during 33P Progress unpacking
2009-05-13
ISS019-E-016481 (13 May 2009) --- Japan Aerospace Exploration Agency (JAXA) astronaut Koichi Wakata, Expedition 19/20 flight engineer, is pictured with fresh tomatoes and apples in the Zvezda Service Module of the International Space Station.
Chamitoff works on TVIS in the SM during Expedition 17
2008-08-01
ISS017-E-012105 (1 Aug. 2008) --- NASA astronaut Greg Chamitoff, Expedition 17 flight engineer, works with the Treadmill Vibration Isolation System (TVIS) in the Zvezda Service Module of the International Space Station.
Expedition 32 Crew Members work in the SM
2012-07-22
ISS032-E-010076 (22 July 2012) --- Russian cosmonaut Sergei Revin (left) and NASA astronaut Joe Acaba, both Expedition 32 flight engineers, use a computer in the Zvezda Service Module of the International Space Station.
Malenchenko wearing Penguin-3 suit in the SM
2008-01-13
ISS016-E-022540 (13 Jan. 2008) --- Cosmonaut Yuri I. Malenchenko, Expedition 16 flight engineer representing Russia's Federal Space Agency, watches a computer monitor in the Zvezda Service Module of the International Space Station.
MATRYOSHKA-R. Receiving and preparing of PADLE detectors for return
2014-09-09
ISS040-E-130020 (9 Sept. 2014) --- European Space Agency astronaut Alexander Gerst, Expedition 40 flight engineer, opens a package of dosimeters in the Zvezda Service Module of the International Space Station.
Kotov works at a Computer Workstation during Expedition 15
2007-07-01
ISS015-E-15616 (1 July 2007) --- Cosmonaut Oleg V. Kotov, Expedition 15 flight engineer representing Russia's Federal Space Agency, uses a computer in the Zvezda Service Module of the International Space Station.
ERIC Educational Resources Information Center
Minnesota State Dept. of Education, St. Paul. Div. of Vocational and Technical Education.
THIS MODULE OF A 30-MODULE COURSE IS DESIGNED TO DEVELOP AN UNDERSTANDING OF THE FUNCTIONS OF DIESEL ENGINE LUBRICATION SYSTEMS AND COMPONENTS AND THE PRINCIPLES OF OPERATION OF BRAKE SYSTEMS USED ON DIESEL POWERED VEHICLES. TOPICS ARE (1) THE NEED FOR OIL, (2) SERVICE CLASSIFICATION OF OILS, (3) CATERPILLAR LUBRICATION SYSTEM COMPONENTS (4)…
2013-07-02
ISS036-E-013924 (2 July 2013) --- NASA astronaut Chris Cassidy, Expedition 36 flight engineer, works in the European Space Agency's Automated Transfer Vehicle-4 (ATV-4) "Albert Einstein" currently docked to the Zvezda Service Module of the International Space Station.
2014-08-18
ISS040E099874 (08/18/2014) --- Cosmonauts Alexander Skvortsov (red stripe - foreground) and Oleg Artemyev (blue stripe - background), Expedition 40 flight engineers, move to the Russian Service Module for repairs during International Space Station Russian EVA 39 on Aug. 18, 2014.
2001-05-15
ISS002-E-6675 (15 May 2001) --- James S. Voss, Expedition Two flight engineer, wearing a safety harness, exercises on the Treadmill Vibration Isolation System (TVIS) equipment in the Zvezda Service Module. This image was taken with a digital still camera.
Williams exercises on TVIS in Zvezda
2007-12-28
ISS014-E-10591 (28 Dec. 2006) --- Astronaut Sunita L. Williams, Expedition 14 flight engineer, equipped with a bungee harness, exercises on the Treadmill Vibration Isolation System (TVIS) in the Zvezda Service Module of the International Space Station.
Wakata during TVIS maintenance
2009-04-21
ISS019-E-008758 (21 April 2009) --- Japan Aerospace Exploration Agency (JAXA) astronaut Koichi Wakata, Expedition 19/20 flight engineer, performs in-flight maintenance on the Treadmill Vibration Isolation System (TVIS) in the Zvezda Service Module of the International Space Station.
Chamitoff performs maintenance on the TVIS during Expedition 17
2008-08-12
ISS017-E-012864 (12 Aug. 2008) --- NASA astronaut Greg Chamitoff, Expedition 17 flight engineer, performs in-flight maintenance on the Treadmill Vibration Isolation System (TVIS) in the Zvezda Service Module of the International Space Station.
Novitskiy performs in-flight maintenance on the TVIS
2013-01-23
ISS034-E-033549 (23 Jan. 2013) --- Russian cosmonaut Oleg Novitskiy, Expedition 34 flight engineer, performs routine in-flight maintenance on the Treadmill Vibration Isolation System (TVIS) in the Zvezda Service Module of the International Space Station.
2007-02-28
ISS014-E-15475 (28 Feb. 2007) --- Cosmonaut Mikhail Tyurin, Expedition 14 flight engineer representing Russia's Federal Space Agency, checks the progress of plants growing in the Russian Lada greenhouse in the Zvezda Service Module of the International Space Station.
2007-02-28
ISS014-E-15479 (28 Feb. 2007) --- Cosmonaut Mikhail Tyurin, Expedition 14 flight engineer representing Russia's Federal Space Agency, checks the progress of plants growing in the Russian Lada greenhouse in the Zvezda Service Module of the International Space Station.
Kotov works with Plasma Crystal-3+ Experiment in the SM during Expedition 22
2010-01-25
ISS022-E-035436 (25 Jan. 2010) --- Russian cosmonaut Oleg Kotov, Expedition 22 flight engineer, works with the Plasma Crystal-3 experiment in the Zvezda Service Module of the International Space Station.
Kotov works with Plasma Crystal-3+ Experiment in the SM during Expedition 22
2010-01-25
ISS022-E-035434 (25 Jan. 2010) --- Russian cosmonaut Oleg Kotov, Expedition 22 flight engineer, works with the Plasma Crystal-3 experiment in the Zvezda Service Module of the International Space Station.
P6 Truss aft radiator seen during EVA
2007-02-04
ISS014-E-13293 (4 Feb. 2007) --- The partially retracted aft radiator of the P6 truss of the International Space Station is featured in this image photographed during the second of three sessions of extravehicular activity (EVA) in nine days by astronauts Michael E. Lopez-Alegria (out of frame), Expedition 14 commander and NASA space station science officer; and Sunita L. Williams (out of frame), flight engineer. The Zvezda Service Module and the Zarya module are visible at left. During the spacewalk, Williams and Lopez-Alegria reconfigured the second of two cooling loops for the Destiny laboratory module, secured the aft radiator of the P6 truss after retraction and prepared the obsolete Early Ammonia Servicer (EAS) for removal this summer.
P6 Truss aft radiator seen during EVA
2007-02-04
ISS014-E-13296 (4 Feb. 2007) --- The partially retracted aft radiator of the P6 truss of the International Space Station is featured in this image photographed during the second of three sessions of extravehicular activity (EVA) in nine days by astronauts Michael E. Lopez-Alegria (out of frame), Expedition 14 commander and NASA space station science officer; and Sunita L. Williams (out of frame), flight engineer. The Zvezda Service Module and the Zarya module are visible at left. During the spacewalk, Williams and Lopez-Alegria reconfigured the second of two cooling loops for the Destiny laboratory module, secured the aft radiator of the P6 truss after retraction and prepared the obsolete Early Ammonia Servicer (EAS) for removal this summer.
The Multi-purpose Crew Vehicle European Service Module: a European Contribution to Human Exploration
NASA Technical Reports Server (NTRS)
Schubert, Kathleen; Berthe, Philippe; Grantier, Julie; Pietsch, Klaus; Angelillo, Philippe; Price, Laurence
2013-01-01
This paper provides an overview of the system and subsystem configuration of the MPCV European Service Module (ESM) at Preliminary Design Review (PDR) stage as well as its perspectives of utilisation within the global space exploration endeavour. The MPCV ESM is a cylindrical module with a diameter of 4500 mm and a total length - main engine excluded - of 2700 mm. It is fitted with four solar array wings with a span of 18.8 m. Its dry mass is 3.5 metric tons and it can carry 8.6 tons of propellant. The main functions of the European Service Module are to bring the structural continuity between the launcher and the crew module, to provide propulsion to the MPCV, to ensure its thermal control as well as electrical power and to store water, oxygen and nitrogen for the mission. The current agreement foresees the development and production by Europe of one flight model, with an option for a second one. This module will be assembled in Europe and delivered to NASA in 2016. It will be used for a flight of the MPCV Orion in December 2017.
The Multi-purpose Crew Vehicle European Service Module: a European Contribution to Human Exploration
NASA Technical Reports Server (NTRS)
Berthe, Philippe; Schubert, Kathleen; Grantier, Julie; Pietsch, Klaus; Angelillo, Philippe; Price, Laurence
2013-01-01
This paper provides an overview of the system and subsystem configuration of the MPCV European Service Module (ESM) at Preliminary Design Review (PDR) stage as well as its perspectives of utilisation within the global space exploration endeavour. The MPCV ESM is a cylindrical module with a diameter of 4500 mm and a total length – main engine excluded – of 2700 mm. It is fitted with four solar array wings with a span of 18.8 m. Its dry mass is 3.5 metric tons and it can carry 8.6 tons of propellant. The main functions of the European Service Module are to bring the structural continuity between the launcher and the crew module, to provide propulsion to the MPCV, to ensure its thermal control as well as electrical power and to store water, oxygen and nitrogen for the mission. The current agreement foresees the development and production by Europe of one flight model, with an option for a second one. This module will be assembled in Europe and delivered to NASA in 2016. It will be used for a flight of the MPCV Orion in December 2017.
Orion Service Module Umbilical (OSMU) Testing Complete
2016-10-19
Testing of the Orion Service Module Umbilical (OSMU) was completed at the Launch Equipment Test Facility at NASA’s Kennedy Space Center in Florida. The OSMU was attached to Vehicle Motion Simulator 1 for a series of simulated launch tests to validate it for installation on the mobile launcher. The mobile launcher tower will be equipped with a number of lines, called umbilicals that will connect to the Space Launch System rocket and Orion spacecraft for Exploration Mission-1 (EM-1). The OSMU will be located high on the mobile launcher tower and, prior to launch, will transfer liquid coolant for the electronics and air for the Environmental Control System to the Orion service module that houses these critical systems to support the spacecraft. Kennedy's Engineering Directorate is providing support to the Ground Systems Development and Operations Program for testing of the OSMU. EM-1 is scheduled to launch in 2018.
2013-06-18
ISS036-E-009246 (18 June 2013) --- NASA astronaut Chris Cassidy, Expedition 36 flight engineer, takes inventory of cargo in the European Space Agency's Automated Transfer Vehicle-4 (ATV-4) "Albert Einstein" currently docked to the Zvezda Service Module of the International Space Station.
Expedition 16 FE Malenchenko works on the P-KINASE Experiment in the SM
2007-10-13
ISS015-E-34291 (13 Oct. 2007) --- Cosmonaut Yuri I. Malenchenko, Expedition 16 flight engineer representing Russia's Federal Space Agency, works with an incubator in the Zvezda Service Module of the International Space Station.
Expedition 16 FE Malenchenko works on the P-KINASE Experiment in the SM
2007-10-13
ISS015-E-34289 (13 Oct. 2007) --- Cosmonaut Yuri I. Malenchenko, Expedition 16 flight engineer representing Russia's Federal Space Agency, works with an incubator in the Zvezda Service Module of the International Space Station.
2007-01-15
ISS014-E-11798 (14 Jan. 2007) --- Cosmonaut Mikhail Tyurin, Expedition 14 flight engineer representing Russia's Federal Space Agency, watches a water bubble float between him and the camera, showing his image refracted, in the Zvezda Service Module of the International Space Station.
2009-10-08
ISS020-E-049859 (8 Oct. 2009) --- Russian cosmonaut Maxim Suraev, Expedition 21/22 flight engineer, uses science hardware RUSALKA at a window in the Zvezda Service Module of the International Space Station to take methane and carbon dioxide measurements in Earth's atmosphere at sunset.
2009-08-19
ISS020-E-031542 (19 Aug. 2009) --- Cosmonaut Roman Romanenko, Expedition 20 flight engineer, uses science hardware RUSALKA at a window in the Zvezda Service Module of the International Space Station to take methane and carbon dioxide measurements in Earth’s atmosphere at sunset.
2009-08-19
ISS020-E-031541 (19 Aug. 2009) --- Cosmonaut Roman Romanenko, Expedition 20 flight engineer, uses science hardware RUSALKA at a window in the Zvezda Service Module of the International Space Station to take methane and carbon dioxide measurements in Earth’s atmosphere at sunset.
SVS (Self-Propagating High-Temperature Synthesis)
2009-08-21
ISS020-E-032798 (21 Aug. 2009) --- Cosmonaut Roman Romanenko, Expedition 20 flight engineer, works with video equipment and a Russian payload TkhN-7 Self-Propagating High-Temperature Synthesis in the Zvezda Service Module of the International Space Station.
Kotov holds Retractable Equipment Tethers in the SM during Expedition 22
2010-01-06
ISS022-E-019986 (6 Jan. 2010) --- Russian cosmonaut Oleg Kotov, Expedition 22 flight engineer, holds a stowage box containing extravehicular activity (EVA) retractable equipment tethers in the Zvezda Service Module of the International Space Station.
Eyharts performs TVIS maintenance
2008-03-03
ISS016-E-030559 (4 March 2008) --- European Space Agency (ESA) astronaut Leopold Eyharts, Expedition 16 flight engineer, works with the Treadmill Vibration Isolation System (TVIS) removed from the Zvezda Service Module floor during in-flight maintenance (IFM) on the International Space Station.
Bursch poses next to the Elektron oxygen generator in the SM during Expedition Four
2002-04-26
ISS004-E-11791 (26 April 2002) --- Astronaut Daniel W. Bursch, Expedition Four flight engineer, works on the Elektron Oxygen Generator in the Zvezda Service Module on the International Space Station (ISS).
Walz poses next to the Elektron oxygen generator in the SM during Expedition Four
2002-04-26
ISS004-E-11792 (26 April 2002) --- Astronaut Carl E. Walz, Expedition Four flight engineer, works on the Elektron Oxygen Generator in the Zvezda Service Module on the International Space Station (ISS).
View of Kotov working at a Computer in the SM during Expedition 15
2007-07-04
ISS015-E-17632 (4 July 2007) --- Cosmonaut Oleg V. Kotov, Expedition 15 flight engineer representing Russia's Federal Space Agency, uses a computer in the Zvezda Service Module of the International Space Station.
2013-06-15
ISS036-E-008182 (15 June 2013) --- Expedition 36 Flight Engineer Fyodor Yurchikhin with Russia's Federal Space Agency (Roscosmos) takes pictures of a highly anticipated event from a window in the Pirs module on the International Space Station. The European Space Agency's Automated Transfer Vehicle-4 (ATV-4) “Albert Einstein” was about to dock to the orbital outpost at 2:07 GMT, June 15, 2013, following a ten-day period of free-flight.
2014-06-06
CAPE CANAVERAL, Fla. -- Inside the Operations and Checkout Building high bay at NASA's Kennedy Space Center in Florida, NASA and Lockheed Martin engineers and technicians monitor the progress as a crane lowers the Orion service module into the Final Assembly and System Testing, or FAST, cell. The Orion crew module will be stacked on the service module in the FAST cell and then both modules will be put through their final system tests for Exploration Flight Test-1, or EFT-1, before rolling out of the facility for integration with the United Launch Alliance Delta IV Heavy rocket. Orion is the exploration spacecraft designed to carry astronauts to destinations not yet explored by humans, including an asteroid and Mars. It will have emergency abort capability, sustain the crew during space travel and provide safe re-entry from deep space return velocities. The first unpiloted test flight of Orion, EFT-1, is scheduled to launch later this year atop a Delta IV rocket from Cape Canaveral Air Force Station in Florida to an altitude of 3,600 miles above the Earth's surface. The two-orbit, four-hour flight test will help engineers evaluate the systems critical to crew safety including the heat shield, parachute system and launch abort system. For more information, visit http://www.nasa.gov/orion. Photo credit: NASA/Glenn Benson
2014-06-06
CAPE CANAVERAL, Fla. -- Inside the Operations and Checkout Building high bay at NASA's Kennedy Space Center in Florida, NASA and Lockheed Martin technicians and engineers prepare to move the Orion service module to the Final Assembly and System Testing, or FAST, cell further down the aisle. The Orion crew module will be stacked on the service module in the FAST cell and then both modules will be put through their final system tests for Exploration Flight Test-1, or EFT-1, prior to rolling out of the facility for integration with the United Launch Alliance Delta IV Heavy rocket. Orion is the exploration spacecraft designed to carry astronauts to destinations not yet explored by humans, including an asteroid and Mars. It will have emergency abort capability, sustain the crew during space travel and provide safe re-entry from deep space return velocities. The first unpiloted test flight of Orion, EFT-1, is scheduled to launch later this year atop a Delta IV rocket from Cape Canaveral Air Force Station in Florida to an altitude of 3,600 miles above the Earth's surface. The two-orbit, four-hour flight test will help engineers evaluate the systems critical to crew safety including the heat shield, parachute system and launch abort system. For more information, visit http://www.nasa.gov/orion. Photo credit: NASA/Glenn Benson
2014-06-06
CAPE CANAVERAL, Fla. -- Inside the Operations and Checkout Building high bay at NASA's Kennedy Space Center in Florida, NASA and Lockheed Martin engineers and technicians help guide the Orion service module into the Final Assembly and System Testing, or FAST, cell. The Orion crew module will be stacked on the service module in the FAST cell and then both modules will be put through their final system tests for Exploration Flight Test-1, or EFT-1, before rolling out of the facility for integration with the United Launch Alliance Delta IV Heavy rocket. Orion is the exploration spacecraft designed to carry astronauts to destinations not yet explored by humans, including an asteroid and Mars. It will have emergency abort capability, sustain the crew during space travel and provide safe re-entry from deep space return velocities. The first unpiloted test flight of Orion, EFT-1, is scheduled to launch later this year atop a Delta IV rocket from Cape Canaveral Air Force Station in Florida to an altitude of 3,600 miles above the Earth's surface. The two-orbit, four-hour flight test will help engineers evaluate the systems critical to crew safety including the heat shield, parachute system and launch abort system. For more information, visit http://www.nasa.gov/orion. Photo credit: NASA/Glenn Benson
2014-06-06
CAPE CANAVERAL, Fla. -- Inside the Operations and Checkout Building high bay at NASA's Kennedy Space Center in Florida, NASA and Lockheed Martin engineers and technicians monitor the progress as a crane lowers the Orion service module into the Final Assembly and System Testing, or FAST, cell. The Orion crew module will be stacked on the service module in the FAST cell and then both modules will be put through their final system tests for Exploration Flight Test-1, or EFT-1, before rolling out of the facility for integration with the United Launch Alliance Delta IV Heavy rocket. Orion is the exploration spacecraft designed to carry astronauts to destinations not yet explored by humans, including an asteroid and Mars. It will have emergency abort capability, sustain the crew during space travel and provide safe re-entry from deep space return velocities. The first unpiloted test flight of Orion, EFT-1, is scheduled to launch later this year atop a Delta IV rocket from Cape Canaveral Air Force Station in Florida to an altitude of 3,600 miles above the Earth's surface. The two-orbit, four-hour flight test will help engineers evaluate the systems critical to crew safety including the heat shield, parachute system and launch abort system. For more information, visit http://www.nasa.gov/orion. Photo credit: NASA/Glenn Benson
Lonchakov checks the Rasteniya-2 plant growth experiment in the SM during Expedition Five
2002-11-08
ISS005-E-20309 (8 November 2002) --- Soyuz 5 Flight Engineer Yuri V. Lonchakov looks at a plant growth experiment in the Zvezda Service Module on the International Space Station (ISS). Lonchakov represents Rosaviakosmos.
2013-06-18
ISS036-E-009256 (18 June 2013) --- NASA astronauts Chris Cassidy and Karen Nyberg, both Expedition 36 flight engineers, perform cargo operations in the European Space Agency's Automated Transfer Vehicle-4 (ATV-4) "Albert Einstein" currently docked to the Zvezda Service Module of the International Space Station.
FE Thirsk exercises on the TVIS in the SM
2009-11-11
ISS021-E-024162 (11 Nov. 2009) --- Canadian Space Agency astronaut Robert Thirsk, Expedition 21 flight engineer, equipped with a bungee harness, exercises on the Treadmill Vibration Isolation System (TVIS) in the Zvezda Service Module of the International Space Station.
2011-07-01
ISS028-E-013758 (1 July 2011) --- Russian cosmonauts Sergei Volkov, Expedition 28 flight engineer; and Andrey Borisenko (mostly out of frame at left), commander, perform in-flight maintenance on the Treadmill Vibration Isolation System (TVIS) in the Zvezda Service Module of the International Space Station.
2007-01-13
ISS014-E-11786 (13 Jan. 2007) --- Surrounded by hardware, astronaut Sunita L. Williams, Expedition 14 flight engineer, equipped with a bungee harness, exercises on the Treadmill Vibration Isolation System (TVIS) (out of frame) in the Zvezda Service Module of the International Space Station.
2007-01-13
ISS014-E-11784 (13 Jan. 2007) --- Surrounded by hardware, astronaut Sunita L. Williams, Expedition 14 flight engineer, equipped with a bungee harness, exercises on the Treadmill Vibration Isolation System (TVIS) (out of frame) in the Zvezda Service Module of the International Space Station.
Tokarev assembles the RadioSkaf antenna during Expedition 12
2006-01-24
ISS012-E-17050 (24 Jan. 2006) --- Cosmonaut Valery I. Tokarev, Expedition 12 flight engineer representing Russia's Federal Space Agency, assembles the antenna kit for the Radioskaf (SuitSat) payload in the Zvezda Service Module on the International Space Station.
Reiter works with Heart Rate and Blood Pressure measuring devices in the SM during Expedition 13
2006-07-01
ISS013-E-54170 (July 2006) --- European Space Agency (ESA) astronaut Thomas Reiter, Expedition 13 flight engineer, looks over a procedures checklist in the Zvezda Service Module of the International Space Station.
Expedition 16 FE Malenchenko working on the Conjugation Experiment Hardware in the SM
2007-10-13
ISS015-E-34287 (13 Oct. 2007) --- Cosmonaut Yuri I. Malenchenko, Expedition 16 flight engineer representing Russia's Federal Space Agency, places hybridizers in orange Rekomb-kit in the Zvezda Service Module of the International Space Station.
MATRYOSHKA-R. Receiving and preparing of PADLE detectors for return
2014-09-09
ISS040-E-130021 (9 Sept. 2014) --- European Space Agency astronaut Alexander Gerst (left), writes a note while Russian cosmonaut Alexander Skvortsov, both Expedition 40 flight engineers, looks on in the Zvezda Service Module of the International Space Station.
Ivanishin prepares his first session with the Russian Behavioral Assessment TIPOLOGIA
2011-12-07
ISS030-E-009567 (7 Dec. 2011) --- Russian cosmonaut Anatoly Ivanishin, Expedition 30 flight engineer, prepares for a session with the Russian behavioral assessment TIPOLOGIA (MBI-20) in the Zvezda Service Module of the International Space Station.
Ivanishin prepares his first session with the Russian Behavioral Assessment TIPOLOGIA
2011-12-07
ISS030-E-009568 (7 Dec. 2011) --- Russian cosmonaut Anatoly Ivanishin, Expedition 30 flight engineer, prepares for a session with the Russian behavioral assessment TIPOLOGIA (MBI-20) in the Zvezda Service Module of the International Space Station.
Ivanishin prepares his first session with the Russian Behavioral Assessment TIPOLOGIA
2011-12-07
ISS030-E-009565 (7 Dec. 2011) --- Russian cosmonaut Anatoly Ivanishin, Expedition 30 flight engineer, prepares for a session with the Russian behavioral assessment TIPOLOGIA (MBI-20) in the Zvezda Service Module of the International Space Station.
2011-09-15
ISS028-E-050058 (15 Sept. 2011) --- NASA astronaut Mike Fossum, Expedition 28 flight engineer, inspects a new growth experiment on the BIO-5 Rasteniya-2 (Plants-2) payload with its LADA-01 greenhouse in the Zvezda Service Module of the International Space Station.
Malenchenko checks Lada Greenhouse in SM
2008-03-06
ISS016-E-031242 (6 March 2008) --- Cosmonaut Yuri I. Malenchenko, Expedition 16 flight engineer representing Russia's Federal Space Agency, checks the progress of pea plants growing in the Russian Lada greenhouse in the Zvezda Service Module of the International Space Station.
Shkaplerov works with EVA Hardware in the SM
2012-02-03
ISS030-E-061158 (3 Feb. 2012) --- Russian cosmonaut Oleg Kononenko, Expedition 30 flight engineer, works with extravehicular activity (EVA) hardware in the Zvezda Service Module of the International Space Station in preparation for an EVA scheduled for Feb. 16, 2012.
Shkaplerov works with EVA Hardware in the SM
2012-02-03
ISS030-E-061157 (3 Feb. 2012) --- Russian cosmonaut Anton Shkaplerov, Expedition 30 flight engineer, works with extravehicular activity (EVA) hardware in the Zvezda Service Module of the International Space Station in preparation for an EVA scheduled for Feb. 16, 2012.
Kotov works with Plasma Crystal-3+ Experiment in the SM during Expedition 22
2010-01-28
ISS022-E-040614 (28 Jan. 2010) --- Russian cosmonaut Oleg Kotov, Expedition 22 flight engineer, is pictured while working with the Plasma Crystal-3 experiment in the Zvezda Service Module of the International Space Station.
Kotov works with Plasma Crystal-3 Experiment in the SM during Expedition 22
2010-01-25
ISS022-E-035439 (25 Jan. 2010) --- Russian cosmonaut Oleg Kotov, Expedition 22 flight engineer, is pictured while working with the Plasma Crystal-3 experiment in the Zvezda Service Module of the International Space Station.
Kotov works with Plasma Crystal-3+ Experiment in the SM during Expedition 22
2010-01-28
ISS022-E-040617 (28 Jan. 2010) --- Russian cosmonaut Oleg Kotov, Expedition 22 flight engineer, is pictured while working with the Plasma Crystal-3 experiment in the Zvezda Service Module of the International Space Station.
NASA Technical Reports Server (NTRS)
Bowyer, J. M.
1984-01-01
The potential of a suitably designed and economically manufactured Stirling engine as the energy conversion subsystem of a paraboloidal dish-Stirling solar thermal power module was estimated. Results obtained by elementary cycle analyses were shown to match quite well the performance characteristics of an advanced kinematic Stirling engine, the United Stirling P-40, as established by current prototypes of the engine and by a more sophisticated analytic model of its advanced derivative. In addition to performance, brief consideration was given to other Stirling engine criteria such as durability, reliability, and serviceability. Production costs were not considered here.
Kononenko reviews crew procedures
2012-03-24
ISS030-E-171108 (24 March 2012) --- Russian cosmonaut Oleg Kononenko, Expedition 30 flight engineer, wearing a communication headset, is pictured in the Zvezda Service Module of the International Space Station as crew members prepare for their move to the appropriate Soyuz vehicles, due to the possibility that space debris could pass close to the station. Burbank, Shkaplerov and Ivanishin sheltered in the Soyuz TMA-22 spacecraft attached to the Poisk Mini-Research Module 2 (MRM2) while Kononenko, Kuipers and Pettit took to the Soyuz TMA-03M docked to the Rassvet Mini-Research Module 1 (MRM-1).
2012-08-20
ISS032-E-021060 (20 Aug. 2012) --- Russian cosmonauts Gennady Padalka (top), Expedition 32 commander; and Yuri Malenchenko, flight engineer, participate in a session of extravehicular activity (EVA) to continue outfitting the International Space Station. During the five-hour, 51-minute spacewalk, Padalka and Malenchenko moved the Strela-2 cargo boom from the Pirs docking compartment to the Zarya module to prepare Pirs for its eventual replacement with a new Russian multipurpose laboratory module. The two spacewalking cosmonauts also installed micrometeoroid debris shields on the exterior of the Zvezda service module and deployed a small science satellite.
2012-08-20
ISS032-E-021061 (20 Aug. 2012) --- Russian cosmonauts Gennady Padalka (top), Expedition 32 commander; and Yuri Malenchenko, flight engineer, participate in a session of extravehicular activity (EVA) to continue outfitting the International Space Station. During the five-hour, 51-minute spacewalk, Padalka and Malenchenko moved the Strela-2 cargo boom from the Pirs docking compartment to the Zarya module to prepare Pirs for its eventual replacement with a new Russian multipurpose laboratory module. The two spacewalking cosmonauts also installed micrometeoroid debris shields on the exterior of the Zvezda service module and deployed a small science satellite.
2012-08-20
ISS032-E-021284 (20 Aug. 2012) --- Russian cosmonaut Gennady Padalka, Expedition 32 commander, participates in a session of extravehicular activity (EVA) to continue outfitting the International Space Station. During the five-hour, 51-minute spacewalk, Padalka and Russian cosmonaut Yuri Malenchenko (out of frame), flight engineer, moved the Strela-2 cargo boom from the Pirs docking compartment to the Zarya module to prepare Pirs for its eventual replacement with a new Russian multipurpose laboratory module. The two spacewalking cosmonauts also installed micrometeoroid debris shields on the exterior of the Zvezda service module and deployed a small science satellite.
2012-08-20
ISS032-E-021044 (20 Aug. 2012) --- Russian cosmonauts Gennady Padalka (top), Expedition 32 commander; and Yuri Malenchenko, flight engineer, participate in a session of extravehicular activity (EVA) to continue outfitting the International Space Station. During the five-hour, 51-minute spacewalk, Padalka and Malenchenko moved the Strela-2 cargo boom from the Pirs docking compartment to the Zarya module to prepare Pirs for its eventual replacement with a new Russian multipurpose laboratory module. The two spacewalking cosmonauts also installed micrometeoroid debris shields on the exterior of the Zvezda service module and deployed a small science satellite.
2012-08-20
ISS032-E-021296 (20 Aug. 2012) --- Russian cosmonaut Gennady Padalka, Expedition 32 commander, participates in a session of extravehicular activity (EVA) to continue outfitting the International Space Station. During the five-hour, 51-minute spacewalk, Padalka and Russian cosmonaut Yuri Malenchenko (out of frame), flight engineer, moved the Strela-2 cargo boom from the Pirs docking compartment to the Zarya module to prepare Pirs for its eventual replacement with a new Russian multipurpose laboratory module. The two spacewalking cosmonauts also installed micrometeoroid debris shields on the exterior of the Zvezda service module and deployed a small science satellite.
2012-08-20
ISS032-E-021028 (20 Aug. 2012) --- Russian cosmonaut Gennady Padalka, Expedition 32 commander, participates in a session of extravehicular activity (EVA) to continue outfitting the International Space Station. During the five-hour, 51-minute spacewalk, Padalka and Russian cosmonaut Yuri Malenchenko (out of frame), flight engineer, moved the Strela-2 cargo boom from the Pirs docking compartment to the Zarya module to prepare Pirs for its eventual replacement with a new Russian multipurpose laboratory module. The two spacewalking cosmonauts also installed micrometeoroid debris shields on the exterior of the Zvezda service module and deployed a small science satellite.
2012-08-20
ISS032-E-020884 (20 Aug. 2012) --- Russian cosmonaut Yuri Malenchenko, Expedition 32 flight engineer, participates in a session of extravehicular activity (EVA) to continue outfitting the International Space Station. During the five-hour, 51-minute spacewalk, Malenchenko and Russian cosmonaut Gennady Padalka (out of frame), commander, moved the Strela-2 cargo boom from the Pirs docking compartment to the Zarya module to prepare Pirs for its eventual replacement with a new Russian multipurpose laboratory module. The two spacewalking cosmonauts also installed micrometeoroid debris shields on the exterior of the Zvezda service module and deployed a small science satellite.
2012-08-20
ISS032-E-021046 (20 Aug. 2012) --- Russian cosmonauts Gennady Padalka (top), Expedition 32 commander; and Yuri Malenchenko, flight engineer, participate in a session of extravehicular activity (EVA) to continue outfitting the International Space Station. During the five-hour, 51-minute spacewalk, Padalka and Malenchenko moved the Strela-2 cargo boom from the Pirs docking compartment to the Zarya module to prepare Pirs for its eventual replacement with a new Russian multipurpose laboratory module. The two spacewalking cosmonauts also installed micrometeoroid debris shields on the exterior of the Zvezda service module and deployed a small science satellite.
2012-08-20
ISS032-E-020610 (20 Aug. 2012) --- Russian cosmonaut Gennady Padalka, Expedition 32 commander, participates in a session of extravehicular activity (EVA) to continue outfitting the International Space Station. During the five-hour, 51-minute spacewalk, Padalka and Russian cosmonaut Yuri Malenchenko (out of frame), flight engineer, moved the Strela-2 cargo boom from the Pirs docking compartment to the Zarya module to prepare Pirs for its eventual replacement with a new Russian multipurpose laboratory module. The two spacewalking cosmonauts also installed micrometeoroid debris shields on the exterior of the Zvezda service module and deployed a small science satellite.
2012-08-20
ISS032-E-021024 (20 Aug. 2012) --- Russian cosmonaut Gennady Padalka, Expedition 32 commander, participates in a session of extravehicular activity (EVA) to continue outfitting the International Space Station. During the five-hour, 51-minute spacewalk, Padalka and Russian cosmonaut Yuri Malenchenko (out of frame), flight engineer, moved the Strela-2 cargo boom from the Pirs docking compartment to the Zarya module to prepare Pirs for its eventual replacement with a new Russian multipurpose laboratory module. The two spacewalking cosmonauts also installed micrometeoroid debris shields on the exterior of the Zvezda service module and deployed a small science satellite.
2012-08-20
ISS032-E-021058 (20 Aug. 2012) --- Russian cosmonaut Yuri Malenchenko, Expedition 32 flight engineer, participates in a session of extravehicular activity (EVA) to continue outfitting the International Space Station. During the five-hour, 51-minute spacewalk, Malenchenko and Russian cosmonaut Gennady Padalka (out of frame), commander, moved the Strela-2 cargo boom from the Pirs docking compartment to the Zarya module to prepare Pirs for its eventual replacement with a new Russian multipurpose laboratory module. The two spacewalking cosmonauts also installed micrometeoroid debris shields on the exterior of the Zvezda service module and deployed a small science satellite.
2012-08-20
ISS032-E-021085 (20 Aug. 2012) --- Russian cosmonaut Gennady Padalka, Expedition 32 commander, participates in a session of extravehicular activity (EVA) to continue outfitting the International Space Station. During the five-hour, 51-minute spacewalk, Padalka and Russian cosmonaut Yuri Malenchenko (out of frame), flight engineer, moved the Strela-2 cargo boom from the Pirs docking compartment to the Zarya module to prepare Pirs for its eventual replacement with a new Russian multipurpose laboratory module. The two spacewalking cosmonauts also installed micrometeoroid debris shields on the exterior of the Zvezda service module and deployed a small science satellite.
2012-08-20
ISS032-E-020576 (20 Aug. 2012) --- Russian cosmonaut Gennady Padalka, Expedition 32 commander, participates in a session of extravehicular activity (EVA) to continue outfitting the International Space Station. During the five-hour, 51-minute spacewalk, Padalka and Russian cosmonaut Yuri Malenchenko (out of frame), flight engineer, moved the Strela-2 cargo boom from the Pirs docking compartment to the Zarya module to prepare Pirs for its eventual replacement with a new Russian multipurpose laboratory module. The two spacewalking cosmonauts also installed micrometeoroid debris shields on the exterior of the Zvezda service module and deployed a small science satellite.
2012-08-20
ISS032-E-020594 (20 Aug. 2012) --- Russian cosmonaut Gennady Padalka, Expedition 32 commander, participates in a session of extravehicular activity (EVA) to continue outfitting the International Space Station. During the five-hour, 51-minute spacewalk, Padalka and Russian cosmonaut Yuri Malenchenko (out of frame), flight engineer, moved the Strela-2 cargo boom from the Pirs docking compartment to the Zarya module to prepare Pirs for its eventual replacement with a new Russian multipurpose laboratory module. The two spacewalking cosmonauts also installed micrometeoroid debris shields on the exterior of the Zvezda service module and deployed a small science satellite.
2012-08-20
ISS032-E-021081 (20 Aug. 2012) --- Russian cosmonaut Gennady Padalka, Expedition 32 commander, participates in a session of extravehicular activity (EVA) to continue outfitting the International Space Station. During the five-hour, 51-minute spacewalk, Padalka and Russian cosmonaut Yuri Malenchenko (out of frame), flight engineer, moved the Strela-2 cargo boom from the Pirs docking compartment to the Zarya module to prepare Pirs for its eventual replacement with a new Russian multipurpose laboratory module. The two spacewalking cosmonauts also installed micrometeoroid debris shields on the exterior of the Zvezda service module and deployed a small science satellite.
2012-08-20
ISS032-E-020856 (20 Aug. 2012) --- Russian cosmonaut Yuri Malenchenko, Expedition 32 flight engineer, participates in a session of extravehicular activity (EVA) to continue outfitting the International Space Station. During the five-hour, 51-minute spacewalk, Malenchenko and Russian cosmonaut Gennady Padalka (out of frame), commander, moved the Strela-2 cargo boom from the Pirs docking compartment to the Zarya module to prepare Pirs for its eventual replacement with a new Russian multipurpose laboratory module. The two spacewalking cosmonauts also installed micrometeoroid debris shields on the exterior of the Zvezda service module and deployed a small science satellite.
2012-08-20
ISS032-E-020683 (20 Aug. 2012) --- Russian cosmonaut Gennady Padalka, Expedition 32 commander, participates in a session of extravehicular activity (EVA) to continue outfitting the International Space Station. During the five-hour, 51-minute spacewalk, Padalka and Russian cosmonaut Yuri Malenchenko (out of frame), flight engineer, moved the Strela-2 cargo boom from the Pirs docking compartment to the Zarya module to prepare Pirs for its eventual replacement with a new Russian multipurpose laboratory module. The two spacewalking cosmonauts also installed micrometeoroid debris shields on the exterior of the Zvezda service module and deployed a small science satellite.
2012-08-20
ISS032-E-021037 (20 Aug. 2012) --- Russian cosmonaut Gennady Padalka, Expedition 32 commander, participates in a session of extravehicular activity (EVA) to continue outfitting the International Space Station. During the five-hour, 51-minute spacewalk, Padalka and Russian cosmonaut Yuri Malenchenko (out of frame), flight engineer, moved the Strela-2 cargo boom from the Pirs docking compartment to the Zarya module to prepare Pirs for its eventual replacement with a new Russian multipurpose laboratory module. The two spacewalking cosmonauts also installed micrometeoroid debris shields on the exterior of the Zvezda service module and deployed a small science satellite.
2012-08-20
ISS032-E-020581 (20 Aug. 2012) --- Russian cosmonaut Gennady Padalka, Expedition 32 commander, participates in a session of extravehicular activity (EVA) to continue outfitting the International Space Station. During the five-hour, 51-minute spacewalk, Padalka and Russian cosmonaut Yuri Malenchenko (out of frame), flight engineer, moved the Strela-2 cargo boom from the Pirs docking compartment to the Zarya module to prepare Pirs for its eventual replacement with a new Russian multipurpose laboratory module. The two spacewalking cosmonauts also installed micrometeoroid debris shields on the exterior of the Zvezda service module and deployed a small science satellite.
2012-08-20
ISS032-E-021293 (20 Aug. 2012) --- Russian cosmonaut Yuri Malenchenko, Expedition 32 flight engineer, participates in a session of extravehicular activity (EVA) to continue outfitting the International Space Station. During the five-hour, 51-minute spacewalk, Malenchenko and Russian cosmonaut Gennady Padalka (out of frame), commander, moved the Strela-2 cargo boom from the Pirs docking compartment to the Zarya module to prepare Pirs for its eventual replacement with a new Russian multipurpose laboratory module. The two spacewalking cosmonauts also installed micrometeoroid debris shields on the exterior of the Zvezda service module and deployed a small science satellite.
2012-08-20
ISS032-E-021286 (20 Aug. 2012) --- Russian cosmonauts Gennady Padalka (top), Expedition 32 commander; and Yuri Malenchenko, flight engineer, participate in a session of extravehicular activity (EVA) to continue outfitting the International Space Station. During the five-hour, 51-minute spacewalk, Padalka and Malenchenko moved the Strela-2 cargo boom from the Pirs docking compartment to the Zarya module to prepare Pirs for its eventual replacement with a new Russian multipurpose laboratory module. The two spacewalking cosmonauts also installed micrometeoroid debris shields on the exterior of the Zvezda service module and deployed a small science satellite.
2012-08-20
ISS032-E-020892 (20 Aug. 2012) --- Russian cosmonaut Yuri Malenchenko, Expedition 32 flight engineer, participates in a session of extravehicular activity (EVA) to continue outfitting the International Space Station. During the five-hour, 51-minute spacewalk, Malenchenko and Russian cosmonaut Gennady Padalka (out of frame), commander, moved the Strela-2 cargo boom from the Pirs docking compartment to the Zarya module to prepare Pirs for its eventual replacement with a new Russian multipurpose laboratory module. The two spacewalking cosmonauts also installed micrometeoroid debris shields on the exterior of the Zvezda service module and deployed a small science satellite.
2012-08-20
ISS032-E-021054 (20 Aug. 2012) --- Russian cosmonaut Yuri Malenchenko, Expedition 32 flight engineer, participates in a session of extravehicular activity (EVA) to continue outfitting the International Space Station. During the five-hour, 51-minute spacewalk, Malenchenko and Russian cosmonaut Gennady Padalka (out of frame), commander, moved the Strela-2 cargo boom from the Pirs docking compartment to the Zarya module to prepare Pirs for its eventual replacement with a new Russian multipurpose laboratory module. The two spacewalking cosmonauts also installed micrometeoroid debris shields on the exterior of the Zvezda service module and deployed a small science satellite.
2012-08-20
ISS032-E-021080 (20 Aug. 2012) --- Russian cosmonaut Gennady Padalka, Expedition 32 commander, participates in a session of extravehicular activity (EVA) to continue outfitting the International Space Station. During the five-hour, 51-minute spacewalk, Padalka and Russian cosmonaut Yuri Malenchenko (out of frame), flight engineer, moved the Strela-2 cargo boom from the Pirs docking compartment to the Zarya module to prepare Pirs for its eventual replacement with a new Russian multipurpose laboratory module. The two spacewalking cosmonauts also installed micrometeoroid debris shields on the exterior of the Zvezda service module and deployed a small science satellite.
Design development of the Apollo command and service module thrust vector attitude control systems
NASA Technical Reports Server (NTRS)
Peters, W. H.
1978-01-01
Development of the Apollo thrust vector control digital autopilot (TVC DAP) was summarized. This is the control system that provided pitch and yaw attitude control during velocity change maneuvers using the main rocket engine on the Apollo service module. A list of ten primary functional requirements for this control system are presented, each being subordinate to a more general requirement appearing earlier on the list. Development process functions were then identified and the essential information flow paths were explored. This provided some visibility into the particular NASA/contractor interface, as well as relationships between the many individual activities.
Shkaplerov makes a selection from food container
2012-02-03
ISS030-E-117515 (3 Feb. 2012) --- Russian cosmonaut Anton Shkaplerov, Expedition 30 flight engineer, makes a selection from a food storage container in the Zvezda Service Module of the International Space Station. NASA astronaut Dan Burbank, commander, is visible in the background.
Williams holds package of food in the SM during Expedition 13
2006-06-01
ISS013-E-29344 (1 June 2006) --- Astronaut Jeffrey N. Williams, Expedition 13 NASA space station science officer and flight engineer, holds a package of food near the galley in the Zvezda Service Module of the International Space Station.
Kotov Exercising on the TVIS during Expedition 15
2007-05-06
ISS015-E-07005 (6 May 2007) --- Cosmonaut Oleg V. Kotov, Expedition 15 flight engineer representing Russia's Federal Space Agency, equipped with a bungee harness, exercises on the Treadmill Vibration Isolation System (TVIS) in the Zvezda Service Module of the International Space Station.
Flight Engineer Donald R. Pettit exercises on the TVIS in the SM during Expedition Six
2003-03-20
ISS006-E-45265 (20 March 2003) --- Astronaut Donald R. Pettit, Expedition 6 NASA ISS science officer, exercises on the Treadmill Vibration Isolation System (TVIS) in the Zvezda Service Module on the International Space Station (ISS).
Kotov Exercising on the TVIS during Expedition 15
2007-05-06
ISS015-E-07003 (6 May 2007) --- Cosmonaut Oleg V. Kotov, Expedition 15 flight engineer representing Russia's Federal Space Agency, equipped with a bungee harness, exercises on the Treadmill Vibration Isolation System (TVIS) in the Zvezda Service Module of the International Space Station.
Sample Collection for the Russian Biodegradatsiya Experiment
2007-10-01
ISS015-E-32031 (October 2007) --- Cosmonaut Oleg V. Kotov, Expedition 15 flight engineer representing Russia's Federal Space Agency, uses a Bioproby Kit to collect surface samples for analysis for the Russian Biodegradation experiment in the Zvezda Service Module of the International Space Station.
Wakata and Barratt with cameras at SM window
2009-04-19
ISS019-E-008935 (19 April 2009) --- Japan Aerospace Exploration Agency (JAXA) astronaut Koichi Wakata (left) and NASA astronaut Michael Barratt, both Expedition 19/20 flight engineers, use still cameras at a window in the Zvezda Service Module of the International Space Station.
MATRYOSHKA-R. Receiving and preparing of PADLE detectors for return
2014-09-09
ISS040-E-130025 (9 Sept. 2014) --- European Space Agency astronaut Alexander Gerst (right) and Russian cosmonaut Alexander Skvortsov, both Expedition 40 flight engineers, work with a package of dosimeters in the Zvezda Service Module of the International Space Station.
Replacing E-K pre-treat container and hose in АСУ system
2006-11-29
ISS014-E-08798 (29 Nov. 2006) --- Cosmonaut Mikhail Tyurin, Expedition 14 flight engineer, replaces the E-K pre-treat container and hose in the waste management system in the Zvezda Service Module of the International Space Station.
2011-08-31
ISS028-E-034854 (31 Aug. 2011) --- Russian cosmonaut Sergei Volkov, Expedition 28 flight engineer, checks the progress of a new growth experiment on the BIO-5 Rasteniya-2 (Plants-2) payload with its LADA-01 greenhouse in the Zvezda Service Module of the International Space Station.
2001-12-12
ISS003-E-8406 (12 December 2001) --- Astronauts Frank L. Culbertson, Jr. (left), Expedition Three mission commander, and Daniel W. Bursch, Expedition Four flight engineer, work in the Zvezda Service Module on the International Space Station (ISS). The image was taken with a digital still camera.
DOE Office of Scientific and Technical Information (OSTI.GOV)
Silverman, Timothy J.; Deceglie, Michael G.; Sun, Xingshu
2015-09-02
Photovoltaic cells can be damaged by reverse bias stress, which arises during service when a monolithically integrated thin-film module is partially shaded. We introduce a model for describing a module's internal thermal and electrical state, which cannot normally be measured. Using this model and experimental measurements, we present several results with relevance for reliability testing and module engineering: Modules with a small breakdown voltage experience less stress than those with a large breakdown voltage, with some exceptions for modules having light-enhanced reverse breakdown. Masks leaving a small part of the masked cells illuminated can lead to very high temperature andmore » current density compared to masks covering entire cells.« less
Thermal and Electrical Effects of Partial Shade in Monolithic Thin-Film Photovoltaic Modules
DOE Office of Scientific and Technical Information (OSTI.GOV)
Silverman, Timothy J.; Deceglie, Michael G.; Sun, Xingshu
2015-06-14
Photovoltaic cells can be damaged by reverse bias stress, which arises during service when a monolithically integrated thin-film module is partially shaded. We introduce a model for describing a module's internal thermal and electrical state, which cannot normally be measured. Using this model and experimental measurements, we present several results with relevance for reliability testing and module engineering: Modules with a small breakdown voltage experience less stress than those with a large breakdown voltage, with some exceptions for modules having light-enhanced reverse breakdown. Masks leaving a small part of the masked cells illuminated can lead to very high temperature andmore » current density compared to masks covering entire cells.« less
Expedition 14 crew in the Zvezda Service module
2006-12-25
ISS014-E-10242 (25 Dec. 2006) --- Cosmonaut Mikhail Tyurin (left), Expedition 14 flight engineer representing Russia's Federal Space Agency; astronaut Michael E. Lopez-Alegria, commander and NASA space station science officer; and astronaut Sunita L. Williams, flight engineer, conduct a teleconference with the Moscow Support Group for the Russian New Year celebration, via Ku- and S-band, with audio and video relayed to the Mission Control Center at Johnson Space Center.
Clinical image processing engine
NASA Astrophysics Data System (ADS)
Han, Wei; Yao, Jianhua; Chen, Jeremy; Summers, Ronald
2009-02-01
Our group provides clinical image processing services to various institutes at NIH. We develop or adapt image processing programs for a variety of applications. However, each program requires a human operator to select a specific set of images and execute the program, as well as store the results appropriately for later use. To improve efficiency, we design a parallelized clinical image processing engine (CIPE) to streamline and parallelize our service. The engine takes DICOM images from a PACS server, sorts and distributes the images to different applications, multithreads the execution of applications, and collects results from the applications. The engine consists of four modules: a listener, a router, a job manager and a data manager. A template filter in XML format is defined to specify the image specification for each application. A MySQL database is created to store and manage the incoming DICOM images and application results. The engine achieves two important goals: reduce the amount of time and manpower required to process medical images, and reduce the turnaround time for responding. We tested our engine on three different applications with 12 datasets and demonstrated that the engine improved the efficiency dramatically.
Fincke smiles at the camera as he holds a partially eaten apple during Expedition 9
2004-10-14
ISS009-E-28931 (16 October 2004) --- Astronaut Edward M. (Mike) Fincke, Expedition 9 NASA ISS science officer and flight engineer, enjoys eating a fresh apple in the Zvezda Service Module of the International Space Station (ISS).
Fincke watches apples and a tennis ball float in the Service Module during Expedition 9
2004-08-15
ISS009-E-18563 (15 August 2004) --- Astronaut Edward M. (Mike) Fincke, Expedition 9 NASA ISS science officer and flight engineer, is pictured near fresh fruit floating freely in the Unity node of the International Space Station (ISS).
2010-05-26
ISS023-E-052104 (26 May 2010) --- Japan Aerospace Exploration Agency (JAXA) astronaut Soichi Noguchi, Expedition 23 flight engineer, uses the IM mass measurement device to perform the PZEh-MO-8/Body Mass Measurement Russian biomedical routine assessments in the Zvezda Service Module of the International Space Station.
Novitskiy prepares for the Typologia Experiment
2013-02-12
ISS034-E-042297 (12 Feb. 2013) --- Russian cosmonaut Oleg Novitskiy, Expedition 34 flight engineer, prepares for the Typologia experiment in the Zvezda Service Module of the International Space Station. This experiment studies the crew member's psychophysical state and ability to perform and communicate under stress.
Novitskiy prepares for the Typologia Experiment
2013-02-12
ISS034-E-042298 (12 Feb. 2013) --- Russian cosmonaut Oleg Novitskiy, Expedition 34 flight engineer, prepares for the Typologia experiment in the Zvezda Service Module of the International Space Station. This experiment studies the crew member's psychophysical state and ability to perform and communicate under stress.
Williams makes adjustment to strap in the SM during Expedition 13
2006-04-18
ISS013-E-08023 (18 April 2006) --- Astronaut Jeffrey N. Williams, Expedition 13 NASA space station science officer and flight engineer, prepares to exercise on the Treadmill Vibration Isolation System (TVIS) in the Zvezda Service Module of the International Space Station.
Whitson and Treschev work on TVIS treadmill
2002-08-07
ISS005-E-08808 (7 August 2002) --- Cosmonaut Sergei Y. Treschev (left) and astronaut Peggy A. Whitson, both Expedition Five flight engineers, perform maintenance on the Treadmill Vibration Isolation System (TVIS) in the Zvezda Service Module on the International Space Station (ISS). Treschev represents Rosaviakosmos.
Whitson and Treschev work on TVIS treadmill
2002-08-07
ISS005-E-08819 (7 August 2002) --- Cosmonaut Sergei Y. Treschev (left) and astronaut Peggy A. Whitson, both Expedition Five flight engineers, perform maintenance on the Treadmill Vibration Isolation System (TVIS) in the Zvezda Service Module on the International Space Station (ISS). Treschev represents Rosaviakosmos.
Whitson and Treschev work on TVIS treadmill
2002-08-07
ISS005-E-08821 (7 August 2002) --- Cosmonaut Sergei Y. Treschev (left) and astronaut Peggy A. Whitson, both Expedition Five flight engineers, are photographed near the Treadmill Vibration Isolation System (TVIS) in the Zvezda Service Module on the International Space Station (ISS). Treschev represents Rosaviakosmos.
Whitson and Treschev perform maintenance on the TVIS
2002-10-13
ISS005-E-17387 (13 October 2002) --- Cosmonaut Sergei Y. Treschev (left) and astronaut Peggy A. Whitson, Expedition Five flight engineers, perform maintenance on the Treadmill Vibration Isolation System (TVIS) in the Zvezda Service Module on the International Space Station (ISS). Treschev represents Rosaviakosmos.
Phillips with TVIS hardware in Zvezda
2005-09-07
ISS011-E-12608 (7 September 2005) --- Astronaut John L. Phillips, Expedition 11 NASA Space Station science officer and flight engineer, works with a portion of the Treadmill Vibration Isolation System (TVIS) during In-Flight Maintenance (IFM) in the Zvezda Service Module of the International Space Station.
Whitson and Treschev perform maintenance on the TVIS
2002-10-13
ISS005-E-17388 (13 October 2002) --- Cosmonaut Sergei Y. Treschev (left) and astronaut Peggy A. Whitson, Expedition Five flight engineers, perform maintenance on the Treadmill Vibration Isolation System (TVIS) in the Zvezda Service Module on the International Space Station (ISS). Treschev represents Rosaviakosmos.
FE Yurchikhin poses for a photo with SonoCard
2010-06-25
ISS024-E-006664 (25 June 2010) --- With most of his body tucked away in a sleeping bag, Russian cosmonaut Fyodor Yurchikhin, Expedition 24 flight engineer, is pictured in his crew quarters compartment in the Zvezda Service Module of the International Space Station.
2014-08-12
ISS040-E-091634 (12 Aug. 2014) --- In the Zvezda Service Module, European Space Agency astronaut Alexander Gerst (left) and Russian cosmonaut Alexander Skvortsov, both Expedition 40 flight engineers, monitor the approach and docking of ESA's "Georges Lemaitre" Automated Transfer Vehicle-5 (ATV-5) to the International Space Station.
2014-08-12
ISS040-E-091638 (12 Aug. 2014) --- In the Zvezda Service Module, European Space Agency astronaut Alexander Gerst (left) and Russian cosmonaut Alexander Skvortsov, both Expedition 40 flight engineers, monitor the approach and docking of ESA's "Georges Lemaitre" Automated Transfer Vehicle-5 (ATV-5) to the International Space Station.
2014-08-12
ISS040-E-091635 (12 Aug. 2014) --- In the Zvezda Service Module, European Space Agency astronaut Alexander Gerst (left) and Russian cosmonaut Alexander Skvortsov, both Expedition 40 flight engineers, monitor the approach and docking of ESA's "Georges Lemaitre" Automated Transfer Vehicle-5 (ATV-5) to the International Space Station.
2014-08-12
ISS040-E-091655 (12 Aug. 2014) --- In the Zvezda Service Module, European Space Agency astronaut Alexander Gerst (right) and Russian cosmonaut Alexander Skvortsov, both Expedition 40 flight engineers, monitor the approach and docking of ESA's "Georges Lemaitre" Automated Transfer Vehicle-5 (ATV-5) to the International Space Station.
2014-08-12
ISS040-E-091688 (12 Aug. 2014) --- In the Zvezda Service Module, European Space Agency astronaut Alexander Gerst (left) and Russian cosmonaut Alexander Skvortsov, both Expedition 40 flight engineers, monitor the approach and docking of ESA?s "Georges Lemaitre" Automated Transfer Vehicle-5 (ATV-5) to the International Space Station.
Crew Exploration Vehicle Ascent Abort Trajectory Analysis and Optimization
NASA Technical Reports Server (NTRS)
Falck, Robert D.; Gefert, Leon P.
2007-01-01
The Orion Crew Exploration Vehicle is the first crewed capsule design to be developed by NASA since Project Apollo. Unlike Apollo, however, the CEV is being designed for service in both Lunar and International Space Station missions. Ascent aborts pose some issues that were not present for Apollo, due to its launch azimuth, nor Space Shuttle, due to its cross range capability. The requirement that a North Atlantic splashdown following an abort be avoidable, in conjunction with the requirement for overlapping abort modes to maximize crew survivability, drives the thrust level of the service module main engine. This paper summarizes 3DOF analysis conducted by NASA to aid in the determination of the appropriate propulsion system for the service module, and the appropriate propellant loading for ISS missions such that crew survivability is maximized.
Maroney, Susan A; McCool, Mary Jane; Geter, Kenneth D; James, Angela M
2007-01-01
The internet is used increasingly as an effective means of disseminating information. For the past five years, the United States Department of Agriculture (USDA) Veterinary Services (VS) has published animal health information in internet-based map server applications, each oriented to a specific surveillance or outbreak response need. Using internet-based technology allows users to create dynamic, customised maps and perform basic spatial analysis without the need to buy or learn desktop geographic information systems (GIS) software. At the same time, access can be restricted to authorised users. The VS internet mapping applications to date are as follows: Equine Infectious Anemia Testing 1972-2005, National Tick Survey tick distribution maps, the Emergency Management Response System-Mapping Module for disease investigations and emergency outbreaks, and the Scrapie mapping module to assist with the control and eradication of this disease. These services were created using Environmental Systems Research Institute (ESRI)'s internet map server technology (ArcIMS). Other leading technologies for spatial data dissemination are ArcGIS Server, ArcEngine, and ArcWeb Services. VS is prototyping applications using these technologies, including the VS Atlas of Animal Health Information using ArcGIS Server technology and the Map Kiosk using ArcEngine for automating standard map production in the case of an emergency.
Orion Service Module Umbilical (OSMU) Testing Complete
2016-10-19
Testing of the Orion Service Module Umbilical (OSMU) was completed at the Launch Equipment Test Facility at NASA’s Kennedy Space Center in Florida. The OSMU was attached to Vehicle Motion Simulator 1 for a series of simulated launch tests to validate it for installation on the mobile launcher. The test team gathered for an event to mark the end of testing. The mobile launcher tower will be equipped with a number of lines, called umbilicals that will connect to the Space Launch System rocket and Orion spacecraft for Exploration Mission-1 (EM-1). The OSMU will be located high on the mobile launcher tower and, prior to launch, will transfer liquid coolant for the electronics and air for the Environmental Control System to the Orion service module that houses these critical systems to support the spacecraft. Kennedy's Engineering Directorate is providing support to the Ground Systems Development and Operations Program for testing of the OSMU. EM-1 is scheduled to launch in 2018.
Orion Service Module Umbilical (OSMU) Testing Complete
2016-10-19
Testing of the Orion Service Module Umbilical (OSMU) was completed at the Launch Equipment Test Facility at NASA’s Kennedy Space Center in Florida. The OSMU was attached to Vehicle Motion Simulator 1 for a series of simulated launch tests to validate it for installation on the mobile launcher. The test team gathered with a special banner during an event to mark the end of testing. The mobile launcher tower will be equipped with a number of lines, called umbilicals that will connect to the Space Launch System rocket and Orion spacecraft for Exploration Mission-1 (EM-1). The OSMU will be located high on the mobile launcher tower and, prior to launch, will transfer liquid coolant for the electronics and air for the Environmental Control System to the Orion service module that houses these critical systems to support the spacecraft. Kennedy's Engineering Directorate is providing support to the Ground Systems Development and Operations Program for testing of the OSMU. EM-1 is scheduled to launch in 2018.
Orion Service Module Umbilical (OSMU) Testing Complete
2016-10-19
Testing of the Orion Service Module Umbilical (OSMU) was completed at the Launch Equipment Test Facility at NASA’s Kennedy Space Center in Florida. The OSMU was attached to Vehicle Motion Simulator 1 for a series of simulated launch tests to validate it for installation on the mobile launcher. One of the test team members signs a banner during an event to mark the end of testing. The mobile launcher tower will be equipped with a number of lines, called umbilicals that will connect to the Space Launch System rocket and Orion spacecraft for Exploration Mission-1 (EM-1). The OSMU will be located high on the mobile launcher tower and, prior to launch, will transfer liquid coolant for the electronics and air for the Environmental Control System to the Orion service module that houses these critical systems to support the spacecraft. Kennedy's Engineering Directorate is providing support to the Ground Systems Development and Operations Program for testing of the OSMU. EM-1 is scheduled to launch in 2018.
Orion Service Module Umbilical (OSMU) Testing Complete
2016-10-19
Testing of the Orion Service Module Umbilical (OSMU) was completed at the Launch Equipment Test Facility at NASA’s Kennedy Space Center in Florida. The OSMU was attached to Vehicle Motion Simulator 1 for a series of simulated launch tests to validate it for installation on the mobile launcher. The test team signed a special banner during an event to mark the end of testing. The mobile launcher tower will be equipped with a number of lines, called umbilicals that will connect to the Space Launch System rocket and Orion spacecraft for Exploration Mission-1 (EM-1). The OSMU will be located high on the mobile launcher tower and, prior to launch, will transfer liquid coolant for the electronics and air for the Environmental Control System to the Orion service module that houses these critical systems to support the spacecraft. Kennedy's Engineering Directorate is providing support to the Ground Systems Development and Operations Program for testing of the OSMU. EM-1 is scheduled to launch in 2018.
2014-06-06
CAPE CANAVERAL, Fla. -- Inside the Operations and Checkout Building high bay at NASA's Kennedy Space Center in Florida, NASA and Lockheed Martin engineers and technicians monitor the progress as a crane is used to move the Orion service module to the Final Assembly and System Testing, or FAST, cell further down the aisle. The Orion crew module will be stacked on the service module in the FAST cell and then both modules will be put through their final system tests for Exploration Flight Test-1, or EFT-1, before rolling out of the facility for integration with the United Launch Alliance Delta IV Heavy rocket. Orion is the exploration spacecraft designed to carry astronauts to destinations not yet explored by humans, including an asteroid and Mars. It will have emergency abort capability, sustain the crew during space travel and provide safe re-entry from deep space return velocities. The first unpiloted test flight of Orion, EFT-1, is scheduled to launch later this year atop a Delta IV rocket from Cape Canaveral Air Force Station in Florida to an altitude of 3,600 miles above the Earth's surface. The two-orbit, four-hour flight test will help engineers evaluate the systems critical to crew safety including the heat shield, parachute system and launch abort system. For more information, visit http://www.nasa.gov/orion. Photo credit: NASA/Glenn Benson
2014-06-06
CAPE CANAVERAL, Fla. -- Inside the Operations and Checkout Building high bay at NASA's Kennedy Space Center in Florida, NASA and Lockheed Martin engineers and technicians monitor the progress as a crane is used to move the Orion service module to the Final Assembly and System Testing, or FAST, cell further down the aisle. The Orion crew module will be stacked on the service module in the FAST cell and then both modules will be put through their final system tests for Exploration Flight Test-1, or EFT-1, before rolling out of the facility for integration with the United Launch Alliance Delta IV Heavy rocket. Orion is the exploration spacecraft designed to carry astronauts to destinations not yet explored by humans, including an asteroid and Mars. It will have emergency abort capability, sustain the crew during space travel and provide safe re-entry from deep space return velocities. The first unpiloted test flight of Orion, EFT-1, is scheduled to launch later this year atop a Delta IV rocket from Cape Canaveral Air Force Station in Florida to an altitude of 3,600 miles above the Earth's surface. The two-orbit, four-hour flight test will help engineers evaluate the systems critical to crew safety including the heat shield, parachute system and launch abort system. For more information, visit http://www.nasa.gov/orion. Photo credit: NASA/Glenn Benson
2014-06-06
CAPE CANAVERAL, Fla. -- Inside the Operations and Checkout Building high bay at NASA's Kennedy Space Center in Florida, NASA and Lockheed Martin technicians and engineers monitor the progress as a crane is used to lift the Orion service module from a test stand and move it to the Final Assembly and System Testing, or FAST, cell further down the aisle. The Orion crew module will be stacked on the service module in the FAST cell and then both modules will be put through their final system tests for Exploration Flight Test-1, or EFT-1, before rolling out of the facility for integration with the United Launch Alliance Delta IV Heavy rocket. Orion is the exploration spacecraft designed to carry astronauts to destinations not yet explored by humans, including an asteroid and Mars. It will have emergency abort capability, sustain the crew during space travel and provide safe re-entry from deep space return velocities. The first unpiloted test flight of Orion, EFT-1, is scheduled to launch later this year atop a Delta IV rocket from Cape Canaveral Air Force Station in Florida to an altitude of 3,600 miles above the Earth's surface. The two-orbit, four-hour flight test will help engineers evaluate the systems critical to crew safety including the heat shield, parachute system and launch abort system. For more information, visit http://www.nasa.gov/orion. Photo credit: NASA/Glenn Benson
Spacecraft servicing demonstration plan
NASA Technical Reports Server (NTRS)
Bergonz, F. H.; Bulboaca, M. A.; Derocher, W. L., Jr.
1984-01-01
A preliminary spacecraft servicing demonstration plan is prepared which leads to a fully verified operational on-orbit servicing system based on the module exchange, refueling, and resupply technologies. The resulting system can be applied at the space station, in low Earth orbit with an orbital maneuvering vehicle (OMV), or be carried with an OMV to geosynchronous orbit by an orbital transfer vehicle. The three phase plan includes ground demonstrations, cargo bay demonstrations, and free flight verifications. The plan emphasizes the exchange of multimission modular spacecraft (MMS) modules which involves space repairable satellites. Three servicer mechanism configurations are the engineering test unit, a protoflight quality unit, and two fully operational units that have been qualified and documented for use in free flight verification activity. The plan balances costs and risks by overlapping study phases, utilizing existing equipment for ground demonstrations, maximizing use of existing MMS equipment, and rental of a spacecraft bus.
Burbank and Kuipers review crew procedures
2012-03-24
ISS030-E-171113 (24 March 2012) --- NASA astronaut Dan Burbank (wearing a communication headset), Expedition 30 commander; and European Space Agency astronaut Andre Kuipers, flight engineer, review crew procedures in the Zvezda Service Module of the International Space Station in preparation of moving to the appropriate Soyuz vehicles, due to the possibility that space debris could pass close to the station. Burbank, Shkaplerov and Ivanishin sheltered in the Soyuz TMA-22 spacecraft attached to the Poisk Mini-Research Module 2 (MRM2) while Kononenko, Kuipers and Pettit took to the Soyuz TMA-03M docked to the Rassvet Mini-Research Module 1 (MRM-1).
Burbank and Shkaplerov review crew procedures
2012-03-24
ISS030-E-171107 (24 March 2012) --- NASA astronaut Dan Burbank (left), Expedition 30 commander; and Russian cosmonaut Anton Shkaplerov, flight engineer, wearing communication headsets, review crew procedures in the Zvezda Service Module of the International Space Station in preparation of moving to the appropriate Soyuz vehicles, due to the possibility that space debris could pass close to the station. Burbank, Shkaplerov and Ivanishin sheltered in the Soyuz TMA-22 spacecraft attached to the Poisk Mini-Research Module 2 (MRM2) while Kononenko, Kuipers and Pettit took to the Soyuz TMA-03M docked to the Rassvet Mini-Research Module 1 (MRM-1).
2012-08-20
ISS032-E-020596 (20 Aug. 2012) --- Russian cosmonaut Gennady Padalka, Expedition 32 commander, deploys a small ball-shaped science satellite during a session of extravehicular activity (EVA) to continue outfitting the International Space Station. During the five-hour, 51-minute spacewalk, Padalka and Russian cosmonaut Yuri Malenchenko (out of frame), flight engineer, also moved the Strela-2 cargo boom from the Pirs docking compartment to the Zarya module to prepare Pirs for its eventual replacement with a new Russian multipurpose laboratory module. The two spacewalking cosmonauts also installed micrometeoroid debris shields on the exterior of the Zvezda service module.
2012-08-20
ISS032-E-021078 (20 Aug. 2012) --- Russian cosmonaut Gennady Padalka, Expedition 32 commander, uses a still camera during a session of extravehicular activity (EVA) to continue outfitting the International Space Station. During the five-hour, 51-minute spacewalk, Padalka and Russian cosmonaut Yuri Malenchenko (out of frame), flight engineer, moved the Strela-2 cargo boom from the Pirs docking compartment to the Zarya module to prepare Pirs for its eventual replacement with a new Russian multipurpose laboratory module. The two spacewalking cosmonauts also installed micrometeoroid debris shields on the exterior of the Zvezda service module and deployed a small science satellite.
2012-08-20
ISS032-E-020619 (20 Aug. 2012) --- Russian cosmonaut Gennady Padalka, Expedition 32 commander, uses a still camera during a session of extravehicular activity (EVA) to continue outfitting the International Space Station. During the five-hour, 51-minute spacewalk, Padalka and Russian cosmonaut Yuri Malenchenko (out of frame), flight engineer, moved the Strela-2 cargo boom from the Pirs docking compartment to the Zarya module to prepare Pirs for its eventual replacement with a new Russian multipurpose laboratory module. The two spacewalking cosmonauts also installed micrometeoroid debris shields on the exterior of the Zvezda service module and deployed a small science satellite.
2012-08-20
ISS032-E-020601 (20 Aug. 2012) --- Russian cosmonaut Gennady Padalka, Expedition 32 commander, deploys a small ball-shaped science satellite during a session of extravehicular activity (EVA) to continue outfitting the International Space Station. During the five-hour, 51-minute spacewalk, Padalka and Russian cosmonaut Yuri Malenchenko (out of frame), flight engineer, also moved the Strela-2 cargo boom from the Pirs docking compartment to the Zarya module to prepare Pirs for its eventual replacement with a new Russian multipurpose laboratory module. The two spacewalking cosmonauts also installed micrometeoroid debris shields on the exterior of the Zvezda service module.
2012-08-20
ISS032-E-021072 (20 Aug. 2012) --- Russian cosmonaut Gennady Padalka, Expedition 32 commander, uses a still camera during a session of extravehicular activity (EVA) to continue outfitting the International Space Station. During the five-hour, 51-minute spacewalk, Padalka and Russian cosmonaut Yuri Malenchenko (out of frame), flight engineer, moved the Strela-2 cargo boom from the Pirs docking compartment to the Zarya module to prepare Pirs for its eventual replacement with a new Russian multipurpose laboratory module. The two spacewalking cosmonauts also installed micrometeoroid debris shields on the exterior of the Zvezda service module and deployed a small science satellite.
2012-08-20
ISS032-E-021067 (20 Aug. 2012) --- Russian cosmonaut Gennady Padalka, Expedition 32 commander, uses a still camera during a session of extravehicular activity (EVA) to continue outfitting the International Space Station. During the five-hour, 51-minute spacewalk, Padalka and Russian cosmonaut Yuri Malenchenko (out of frame), flight engineer, moved the Strela-2 cargo boom from the Pirs docking compartment to the Zarya module to prepare Pirs for its eventual replacement with a new Russian multipurpose laboratory module. The two spacewalking cosmonauts also installed micrometeoroid debris shields on the exterior of the Zvezda service module and deployed a small science satellite.
Signing ISS RS Handover Protocol
2014-09-09
ISS040-E-123948 (9 Sept. 2014) --- In the Zvezda Service Module, Russian cosmonaut Maxim Suraev (right), Expedition 41 commander, signs a ceremonial document as the new commander of the International Space Station following the traditional Change of Command Ceremony. Russian cosmonaut Alexander Skvortsov, Expedition 40 flight engineer, looks on.
FE-1 Suraev prepares a new version of the BIO-5 Rasteniya-2 Experiment
2009-10-29
ISS021-E-016211 (29 Oct. 2009) --- Russian cosmonaut Maxim Suraev, Expedition 21 flight engineer, works with a new growth experiment on the BIO-5 Rasteniya-2 (Plants-2) payload in the Zvezda Service Module of the International Space Station.
FE-1 Suraev prepares a new version of the BIO-5 Rasteniya-2 Experiment
2009-10-29
ISS021-E-016204 (29 Oct. 2009) --- Russian cosmonaut Maxim Suraev, Expedition 21 flight engineer, works with a new growth experiment on the BIO-5 Rasteniya-2 (Plants-2) payload in the Zvezda Service Module of the International Space Station.
View of FE Stott using the BMMD in the SM
2009-10-12
ISS021-E-014503 (12 Oct. 2009) --- NASA astronaut Nicole Stott, Expedition 21 flight engineer, uses the IM mass measurement device to perform the PZEh-MO-8/Body Mass Measurement Russian biomedical routine assessments in the Zvezda Service Module of the International Space Station.
PZEh-MO-8/Body Mass Measurement
2009-06-30
ISS020-E-015853 (30 June 2009) --- Japan Aerospace Exploration Agency (JAXA) astronaut Koichi Wakata, Expedition 20 flight engineer, uses the IM mass measurement device to perform the PZEh-MO-8/Body Mass Measurement Russian biomedical routine assessments in the Zvezda Service Module of the International Space Station.
Tarelkin prepares for the Typologia Experiment in the SM
2013-01-24
ISS034-E-033718 (24 Jan. 2013) --- Russian cosmonaut Evgeny Tarelkin, Expedition 34 flight engineer, prepares for the Typologia experiment in the Zvezda Service Module of the International Space Station. This experiment studies the crew member's psychophysical state and ability to perform and communicate under stress.
Sharipov holds the probe-and-cone docking mechanism in the SM during Expedition 10
2005-03-03
ISS010-E-19105 (3 March 2005) --- Cosmonaut Salizhan S. Sharipov, Expedition 10 flight engineer representing Russia's Federal Space Agency, holds the Progress supply vehicle probe-and-cone docking mechanism in the Zvezda Service Module of the International Space Station (ISS).
Fincke holds the active docking assembly inside the SM during Expedition 9
2004-08-14
ISS009-E-18539 (14 August 2004) --- Astronaut Edward M. (Mike) Fincke, Expedition 9 NASA ISS science officer and flight engineer, holds the Progress 15 supply vehicle probe-and-cone docking mechanism in the Zvezda Service Module of the International Space Station (ISS).
Malenchenko uses a computer in the SM during Joint Operations
2008-03-21
S123-E-008370 (21 March 2008) --- Cosmonaut Yuri I. Malenchenko, Expedition 16 flight engineer representing Russia's Federal Space Agency, uses a computer in the Zvezda Service Module of the International Space Station while Space Shuttle Endeavour (STS-123) is docked with the station.
BIO-5 Rasteniya-2 (Plants-2) Experiment in the LADA-16 Greenhouse
2009-10-26
ISS021-E-012522 (26 Oct. 2009) --- Russian cosmonaut Roman Romanenko, Expedition 21 flight engineer, poses for a photo with the current growth experiment on the BIO-5 Rasteniya-2 (Plants-2) payload in the Zvezda Service Module of the International Space Station.
Expedition 39 Crewmembers Inflight Portrait
2014-04-11
ISS039-E-011175 (11 April 2014) --- Inside the Zvezda service module on the Earth-orbiting International Space Station, the six Expedition 39 crew members face the camera during a call with Russian President Vladimir Putin. From left to right are NASA astronauts Rick Mastracchio and Steve Swanson, both flight engineers; Commander Koichi Wakata of the Japan Aerospace Exploration Agency (JAXA), and cosmonauts Alexander Skvortsov, Mikhail Tyurin and Oleg Artemyev, all flight engineers with Russia's Federal Space Agency (Roscosmos).
Expedition 39 Crewmembers Inflight Portrait
2014-04-11
ISS039-E-011174 (11 April 2014) --- Inside the Zvezda service module on the Earth-orbiting International Space Station, the six Expedition 39 crew members face the camera during a call with Russian President Vladimir Putin. From left to right are NASA astronauts Rick Mastracchio and Steve Swanson, both flight engineers; Commander Koichi Wakata of the Japan Aerospace Exploration Agency (JAXA), and cosmonauts Alexander Skvortsov, Mikhail Tyurin and Oleg Artemyev, all flight engineers with Russia's Federal Space Agency (Roscosmos).
2011-02-16
ISS026-E-027391 (16 Feb. 2011) --- Russian cosmonaut Dmitry Kondratyev, Expedition 26 flight engineer, wearing a Russian Orlan-MK spacesuit, participates in a session of extravehicular activity (EVA) focused on the installation of two scientific experiments outside the Zvezda Service Module of the International Space Station. During the four-hour, 51-minute spacewalk, Kondratyev and Russian cosmonaut Oleg Skripochka (out of frame), flight engineer, installed a pair of earthquake and lightning sensing experiments and retrieved a pair of spacecraft material evaluation panels.
Boeing CST-100 Starliner Processing
2018-04-26
Boeing’s CST-100 Pad Abort Test Vehicle is almost ready to head to White Sands, New Mexico, to test the launch abort engines. During that test, the four abort engines will prove that the vehicle can safely perform an abort maneuver in the event of an emergency on the launchpad or during flight. The vehicle is mated to the service module for a fit check, and then the two will be taken apart for final preparations before heading to the desert.
2011-02-16
ISS026-E-027361 (16 Feb. 2011) --- Russian cosmonaut Dmitry Kondratyev, Expedition 26 flight engineer, wearing a Russian Orlan-MK spacesuit, participates in a session of extravehicular activity (EVA) focused on the installation of two scientific experiments outside the Zvezda Service Module of the International Space Station. During the four-hour, 51-minute spacewalk, Kondratyev and Russian cosmonaut Oleg Skripochka (out of frame), flight engineer, installed a pair of earthquake and lightning sensing experiments and retrieved a pair of spacecraft material evaluation panels.
2011-02-16
ISS026-E-027368 (16 Feb. 2011) --- Russian cosmonaut Dmitry Kondratyev, Expedition 26 flight engineer, wearing a Russian Orlan-MK spacesuit, participates in a session of extravehicular activity (EVA) focused on the installation of two scientific experiments outside the Zvezda Service Module of the International Space Station. During the four-hour, 51-minute spacewalk, Kondratyev and Russian cosmonaut Oleg Skripochka (out of frame), flight engineer, installed a pair of earthquake and lightning sensing experiments and retrieved a pair of spacecraft material evaluation panels.
NASA Technical Reports Server (NTRS)
Thomas, R. E.; Gaines, G. B.
1978-01-01
Recommended design procedures to reduce the complete factorial design by retaining information on anticipated important interaction effects, and by generally giving up information on unconditional main effects are discussed. A hypothetical photovoltaic module used in the test design is presented. Judgments were made of the relative importance of various environmental stresses such as UV radiation, abrasion, chemical attack, temperature, mechanical stress, relative humidity and voltage. Consideration is given to a complete factorial design and its graphical representation, elimination of selected test conditions, examination and improvement of an engineering design, and parametric study. The resulting design consists of a mix of conditional main effects and conditional interactions and represents a compromise between engineering and statistical requirements.
2017-02-15
Charles Spern, at right, project manager on the Engineering Services Contract (ESC), and Glenn Washington, ESC quality assurance specialist, perform final inspections of the Veggie Series 1 plant experiment inside a laboratory in the Space Station Processing Facility at NASA's Kennedy Space Center in Florida. The Series 1 experiment is being readied for flight aboard Orbital ATK's Cygnus module on its seventh (OA-7) Commercial Resupply Services mission to the International Space Station. The Veggie system is on the space station.
DeWinne posing at the Rasteniya-2 plant growth experiment in the SM during Expedition Five
2002-11-08
ISS005-E-20310 (8 November 2002) --- Belgian Soyuz 5 Flight Engineer Frank DeWinne is pictured near a plant growth experiment in the Zvezda Service Module on the International Space Station (ISS). DeWinne represents the European Space Agency (ESA).
2013-08-22
ISS036-E-035256 (22 Aug. 2013) --- Russian cosmonauts Alexander Misurkin (top) and Fyodor Yurchikhin, both Expedition 36 flight engineers, are pictured in the Zvezda Service Module of the International Space Station following a session of extravehicular activity (EVA). Misurkin and Yurchikhin are wearing blue thermal undergarments that complement the Russian Orlan spacesuit.
FE Fyodor Yurchikhin works on the Uragan Experiment in the SM
2010-07-08
ISS024-E-007525 (8 July 2010) --- In the International Space Station’s Zvezda Service Module, Russian cosmonaut Fyodor Yurchikhin, Expedition 24 flight engineer, conducts a session for Russia's Environmental Safety Agency (EKON), making observations and taking KPT-3 aerial photography of environmental conditions on Earth.
FE Fyodor Yurchikhin works on the Uragan Experiment in the SM
2010-07-08
ISS024-E-007526 (8 July 2010) --- In the International Space Station’s Zvezda Service Module, Russian cosmonaut Fyodor Yurchikhin, Expedition 24 flight engineer, conducts a session for Russia's Environmental Safety Agency (EKON), making observations and taking KPT-3 aerial photography of environmental conditions on Earth.
FE Fyodor Yurchikhin works on the Uragan Experiment in the SM
2010-07-08
ISS024-E-007527 (8 July 2010) --- In the International Space Station’s Zvezda Service Module, Russian cosmonaut Fyodor Yurchikhin, Expedition 24 flight engineer, conducts a session for Russia's Environmental Safety Agency (EKON), making observations and taking KPT-3 aerial photography of environmental conditions on Earth.
FE Fyodor Yurchikhin works on the Uragan Experiment in the SM
2010-07-08
ISS024-E-007521 (8 July 2010) --- In the International Space Station’s Zvezda Service Module, Russian cosmonaut Fyodor Yurchikhin, Expedition 24 flight engineer, prepares to conduct a session for Russia's Environmental Safety Agency (EKON), making observations and taking KPT-3 aerial photography of environmental conditions on Earth.
Kaleri works on the SKV-2 AC in the SM during Expedition 8
2003-12-16
ISS008-E-08615 (16 December 2003) --- Cosmonaut Alexander Y. Kaleri, Expedition 8 flight engineer, works to remove and replace a Heat Exchanger on the SKV-2 Air Conditioner in the Zvezda Service Module on the International Space Station (ISS). Kaleri represents Rosaviakosmos.
49 CFR Appendix A to Part 395 - Electronic On-Board Recorder Performance Specifications
Code of Federal Regulations, 2011 CFR
2011-10-01
... (to home office or wireless service provider). External Sensor Issue NO_ECM no ECM data No sensory information received from vehicle's Engine Control Module (ECM). External Sensor Issue ECM_ID ECM ID number mismatch ECM identification/serial number mismatch (with preprogrammed information). 2. Communications...
Chiao performs in-flight maintenance on the TVIS in the SM during Expedition 10
2005-02-15
ISS010-E-17815 (15 February 2005) --- Cosmonaut Salizhan S. Sharipov, Expedition 10 flight engineer representing Russia's Federal Space Agency, performs in-flight maintenance on the Treadmill Vibration Isolation System (TVIS) in the Zvezda Service Module of the International Space Station (ISS).
Kaleri prepares for a data collection / exercise session on the TVIS in the SM during Expedition 8
2003-11-23
ISS008-E-05964 (23 November 2003) --- Cosmonaut Alexander Y. Kaleri, Expedition 8 flight engineer, performs in-flight maintenance (IFM) on the Treadmill Vibration Isolation System (TVIS) in the Zvezda Service Module on the International Space Station (ISS). Kaleri represents Rosaviakosmos.
Walz configures the Amateur Radio (HAM) WA3 Antenna Assembly, Expedition Four
2002-01-12
ISS004-E-5930 (January 2002) --- Astronaut Carl E. Walz, Expedition Four flight engineer, works with the Amateur Radio (HAM) WA3 Antenna Assembly in the Zvezda Service Module on the International Space Station (ISS). The image was taken with a digital still camera.
Expedition 16 FE Malenchenko working on the Conjugation Experiment Hardware in the SM
2007-10-13
ISS015-E-34286 (13 Oct. 2007) --- Cosmonaut Yuri I. Malenchenko, Expedition 16 flight engineer representing Russia's Federal Space Agency, works with a hybridizer from the Rekomb-K kit used in the Konyugatsia (Conjugation) experiment in the Zvezda Service Module of the International Space Station.
Expedition Five crew perform maintenance on the TVIS
2002-10-13
ISS005-E-17412 (13 October 2002) --- Cosmonaut Valery G. Korzun (left), Expedition Five mission commander, and astronaut Peggy A. Whitson, Expedition Five flight engineer, perform maintenance on the Treadmill Vibration Isolation System (TVIS) in the Zvezda Service Module on the International Space Station (ISS). Korzun represents Rosaviakosmos.
Sharipov holds a package of Russian food near the galley in the SM during Expedition 9/10 joint OPS
2004-10-16
ISS009-E-29027 (17 October 2004) --- Cosmonaut Salizhan S. Sharipov, Expedition 10 flight engineer representing Russia's Federal Space Agency, holds a package of food near the galley in the Zvezda Service Module of the International Space Station (ISS).
Kuipers and Kononenko during ATV Approach and Docking
2012-03-28
ISS030-E-177327 (28 March 2012) --- European Space Agency astronaut Andre Kuipers and Russian cosmonaut Oleg Kononenko (foreground), both Expedition 30 flight engineers, monitor the approach and docking of ESA’s “Edoardo Amaldi” Automated Transfer Vehicle-3 (ATV-3) in the Zvezda Service Module of the International Space Station.
Kuipers and Kononenko during ATV Approach and Docking
2012-03-28
ISS030-E-177363 (28 March 2012) --- European Space Agency astronaut Andre Kuipers and Russian cosmonaut Oleg Kononenko (foreground), both Expedition 30 flight engineers, monitor the approach and docking of ESA’s “Edoardo Amaldi” Automated Transfer Vehicle-3 (ATV-3) in the Zvezda Service Module of the International Space Station.
Kuipers and Kononenko during ATV Approach and Docking
2012-03-28
ISS030-E-177317 (28 March 2012) --- European Space Agency astronaut Andre Kuipers and Russian cosmonaut Oleg Kononenko (foreground), both Expedition 30 flight engineers, monitor the approach and docking of ESA’s “Edoardo Amaldi” Automated Transfer Vehicle-3 (ATV-3) in the Zvezda Service Module of the International Space Station.
Space Station Cosmonauts Walk in Space to Upgrade Communications Hardware
2018-02-02
Aboard the International Space Station, Expedition 54 Flight Engineers Alexander Misurkin and Anton Shkaplerov of the Russian Federal Space Agency (Roscosmos) conducted a spacewalk outside the Pirs docking compartment Feb. 2 to install a new high-gain communications antenna on the aft end of the Zvezda Service Module and retrieve science experiment packages from the hull of the module. It was the 208th spacewalk in support of space station assembly and maintenance, the fourth in Misurkin’s career and the second for Shkaplerov.
2009-02-16
CAPE CANAVERAL, Fla. – In high bay 4 of the Vehicle Assembly Building at NASA's Kennedy Space Center, workers lift the Ares I-X crew module mock-up during a fit check with a mock-up of the service module. When fully developed, the 16-foot diameter crew module will furnish living space and reentry protection for future astronauts, and the service module’s main engine will be used to break out of lunar orbit for the return trip to Earth. Ares I-X is the test flight for the Ares I, which is part of the Constellation Program to return men to the moon and beyond. The I-X flight will provide NASA an early opportunity to test and prove hardware, facilities and ground operations associated with Ares I launches. Targeted for the summer of 2009, the launch of the full-scale Ares I-X will be the first in a series of unpiloted rocket launches from Kennedy. Photo credit: NASA/Jack Pfaller
Boeing's CST-100 Launch Abort Engine Test
2016-10-10
Boeing and Aerojet Rocketdyne have begun a series of developmental hot-fire tests with two launch abort engines similar to the ones that will be part of Boeing’s CST-100 Starliner service module, in the Mojave Desert in California. The engines, designed to maximize thrust build-up, while minimizing overshoot during start up, will be fired between half a second and 3 seconds each during the test campaign. If the Starliner’s four launch abort engines were used during an abort scenario, they would fire between 3 and 5.5. seconds, with enough thrust to get the spacecraft and its crew away from the rocket, before splashing down in the ocean under parachutes.
NASA Technical Reports Server (NTRS)
Prisbell, Andrew; Marichalar, J.; Lumpkin, F.; LeBeau, G.
2010-01-01
Plume impingement effects on the Orion Crew Service Module (CSM) were analyzed for various dual Reaction Control System (RCS) engine firings and various configurations of the solar arrays. The study was performed using a decoupled computational fluid dynamics (CFD) and Direct Simulation Monte Carlo (DSMC) approach. This approach included a single jet plume solution for the R1E RCS engine computed with the General Aerodynamic Simulation Program (GASP) CFD code. The CFD solution was used to create an inflow surface for the DSMC solution based on the Bird continuum breakdown parameter. The DSMC solution was then used to model the dual RCS plume impingement effects on the entire CSM geometry with deployed solar arrays. However, because the continuum breakdown parameter of 0.5 could not be achieved due to geometrical constraints and because high resolution in the plume shock interaction region is desired, a focused DSMC simulation modeling only the plumes and the shock interaction region was performed. This high resolution intermediate solution was then used as the inflow to the larger DSMC solution to obtain plume impingement heating, forces, and moments on the CSM and the solar arrays for a total of 21 cases that were analyzed. The results of these simulations were used to populate the Orion CSM Aerothermal Database.
OA-7 Veggie Series 1 Processing
2017-02-15
Charles Spern, project manager on the Engineering Services Contract (ESC), and Glenn Washington, ESC quality assurance specialist, perform final inspections of the Veggie Series 1 plant experiment inside a laboratory in the Space Station Processing Facility at NASA's Kennedy Space Center in Florida. The Series 1 experiment is being readied for flight aboard Orbital ATK's Cygnus module on its seventh (OA-7) Commercial Resupply Services mission to the International Space Station. The Veggie system is on the space station.
Burbank, Shkaplerov, and Kuipers review crew procedures
2012-03-24
ISS030-E-171111 (24 March 2012) --- NASA astronaut Dan Burbank (left), Expedition 30 commander; along with Russian cosmonaut Anton Shkaplerov (center) and European Space Agency astronaut Andre Kuipers, both flight engineers, review crew procedures in the Zvezda Service Module of the International Space Station in preparation of moving to the appropriate Soyuz vehicles, due to the possibility that space debris could pass close to the station. Burbank, Shkaplerov and Ivanishin sheltered in the Soyuz TMA-22 spacecraft attached to the Poisk Mini-Research Module 2 (MRM2) while Kononenko, Kuipers and Pettit took to the Soyuz TMA-03M docked to the Rassvet Mini-Research Module 1 (MRM-1).
Lonchakov on Service Module (SM) during Russian Extravehicular Activity (EVA) 21A
2009-03-10
ISS018-E-039196 (10 March 2009) --- Cosmonaut Yury Lonchakov, Expedition 18 flight engineer, participates in a session of extravehicular activity (EVA) to perform maintenance on the International Space Station. During the 4-hour, 49-minute spacewalk, Lonchakov and astronaut Michael Fincke (out of frame), commander, reinstalled the Exposing Specimens of Organic and Biological Materials to Open Space (Expose-R) experiment on the universal science platform mounted to the exterior of the Zvezda Service Module. The spacewalkers also removed straps, or tape, from the area of the docking target on the Pirs airlock and docking compartment. The tape was removed to ensure it does not get in the way during the arrival of visiting Soyuz or Progress spacecraft.
Lonchakov on Service Module (SM) near 2AP-BKA during Russian Extravehicular Activity (EVA) 21A
2009-03-10
ISS018-E-039147 (10 March 2009) --- Cosmonaut Yury Lonchakov, Expedition 18 flight engineer, participates in a session of extravehicular activity (EVA) to perform maintenance on the International Space Station. During the 4-hour, 49-minute spacewalk, Lonchakov and astronaut Michael Fincke (out of frame), commander, reinstalled the Exposing Specimens of Organic and Biological Materials to Open Space (Expose-R) experiment on the universal science platform mounted to the exterior of the Zvezda Service Module. The spacewalkers also removed straps, or tape, from the area of the docking target on the Pirs airlock and docking compartment. The tape was removed to ensure it does not get in the way during the arrival of visiting Soyuz or Progress spacecraft.
Lonchakov on Service Module (SM) near 2AP-BKA during Russian Extravehicular Activity (EVA) 21A
2009-03-10
ISS018-E-039156 (10 March 2009) --- Cosmonaut Yury Lonchakov, Expedition 18 flight engineer, participates in a session of extravehicular activity (EVA) to perform maintenance on the International Space Station. During the 4-hour, 49-minute spacewalk, Lonchakov and astronaut Michael Fincke (out of frame), commander, reinstalled the Exposing Specimens of Organic and Biological Materials to Open Space (Expose-R) experiment on the universal science platform mounted to the exterior of the Zvezda Service Module. The spacewalkers also removed straps, or tape, from the area of the docking target on the Pirs airlock and docking compartment. The tape was removed to ensure it does not get in the way during the arrival of visiting Soyuz or Progress spacecraft.
Duque and Kaleri in Zvezda Service module with video camera
2003-10-23
ISS007-E-17842 (23 October 2003) --- European Space Agency (ESA) astronaut Pedro Duque (left) of Spain and cosmonaut Alexander Y. Kaleri, Expedition 8 flight engineer representing Rosaviakosmos, work with a scientific experiment in the Zvezda Service Module on the International Space Station (ISS). Duque and Kaleri performed the European educational VIDEO-2 (VID-01) experiment, which uses the Russian DSR PD-150P digital video camcorder for recording demos of several basic physical phenomena, viz., Isaac Newton's three motion laws, with narration. [The demo made use of a sealed bag containing coffee and a syringe to fill one of two hollow balls with the brown liquid (to provide "mass", as opposed to the other, "mass-less" ball).
Automated Heat-Flux-Calibration Facility
NASA Technical Reports Server (NTRS)
Liebert, Curt H.; Weikle, Donald H.
1989-01-01
Computer control speeds operation of equipment and processing of measurements. New heat-flux-calibration facility developed at Lewis Research Center. Used for fast-transient heat-transfer testing, durability testing, and calibration of heat-flux gauges. Calibrations performed at constant or transient heat fluxes ranging from 1 to 6 MW/m2 and at temperatures ranging from 80 K to melting temperatures of most materials. Facility developed because there is need to build and calibrate very-small heat-flux gauges for Space Shuttle main engine (SSME).Includes lamp head attached to side of service module, an argon-gas-recirculation module, reflector, heat exchanger, and high-speed positioning system. This type of automated heat-flux calibration facility installed in industrial plants for onsite calibration of heat-flux gauges measuring fluxes of heat in advanced gas-turbine and rocket engines.
Williams receives a haircut from Yurchikhin in the SM during Expedition 15
2007-06-03
ISS015-E-10596 (3 June 2007) --- Cosmonaut Fyodor N. Yurchikhin, Expedition 15 commander representing Russia's Federal Space Agency, cuts astronaut Sunita L. Williams' hair in the Zvezda Service Module of the International Space Station. Williams, flight engineer, holds a vacuum device fashioned to garner freshly cut hair.
Whitson receives haircut from Korzun in Zvezda
2002-10-01
ISS005-E-18072 (October 2002) --- Cosmonaut Valery G. Korzun, Expedition Five mission commander, cuts astronaut Peggy A. Whitsons hair in the Zvezda Service Module on the International Space Station (ISS). Whitson, flight engineer, holds a vacuum device the crew has fashioned to garner freshly cut hair, which is floating freely.
Whitson receives haircut from Korzun in Zvezda
2002-10-01
ISS005-E-18071 (October 2002) --- Cosmonaut Valery G. Korzun, Expedition Five mission commander, cuts astronaut Peggy A. Whitsons hair in the Zvezda Service Module on the International Space Station (ISS). Whitson, flight engineer, holds a vacuum device the crew has fashioned to garner freshly cut hair, which is floating freely.
Williams receives a haircut from Yurchikhin in the SM during Expedition 15
2007-06-03
ISS015-E-10595 (3 June 2007) --- Cosmonaut Fyodor N. Yurchikhin, Expedition 15 commander representing Russia's Federal Space Agency, cuts astronaut Sunita L. Williams' hair in the Zvezda Service Module of the International Space Station. Williams, flight engineer, holds a vacuum device fashioned to garner freshly cut hair.
Wakata uses Treadmill Vibration Isolation and Stabilization (TVIS)
2009-03-22
ISS018-E-042662 (22 March 2009) --- Japan Aerospace Exploration Agency (JAXA) astronaut Koichi Wakata, Expedition 18 flight engineer, equipped with a bungee harness, exercises on the Treadmill Vibration Isolation System (TVIS) in the Zvezda Service Module of the International Space Station while Space Shuttle Discovery (STS-119) remains docked with the station.
Expedition Five crew perform maintenance on the TVIS
2002-10-13
ISS005-E-17402 (13 October 2002) --- Cosmonauts Valery G. Korzun (left), Expedition Five mission commander, Sergei Y. Treschev and astronaut Peggy A. Whitson, Expedition Five flight engineers, perform maintenance on the Treadmill Vibration Isolation System (TVIS) in the Zvezda Service Module on the International Space Station (ISS). Korzun and Treschev represent Rosaviakosmos.
Expedition Five crew perform maintenance on the TVIS
2002-10-13
ISS005-E-17390 (13 October 2002) --- Cosmonauts Valery G. Korzun (left), Expedition Five mission commander, Sergei Y. Treschev and astronaut Peggy A. Whitson, Expedition Five flight engineers, perform maintenance on the Treadmill Vibration Isolation System (TVIS) in the Zvezda Service Module on the International Space Station (ISS). Korzun and Treschev represent Rosaviakosmos.
Expedition Five crew perform maintenance on the TVIS
2002-10-13
ISS005-E-17392 (13 October 2002) --- Cosmonauts Valery G. Korzun (left), Expedition Five mission commander, Sergei Y. Treschev and astronaut Peggy A. Whitson, Expedition Five flight engineers, perform maintenance on the Treadmill Vibration Isolation System (TVIS) in the Zvezda Service Module on the International Space Station (ISS). Korzun and Treschev represent Rosaviakosmos.
Onufrienko and Bursch perform IFM on SM Potok air purification unit during Expedition Four
2002-01-01
ISS004-E-5387 (January 2002) --- Cosmonaut Yuri I. Onufrienko (right), Expedition Four mission commander, and astronaut Daniel W. Bursch, flight engineer, perform maintenance on equipment in the Zvezda Service Module on the International Space Station (ISS). Onufrienko represents Rosaviakosmos. The image was taken with a digital still camera.
NASA Technical Reports Server (NTRS)
1979-01-01
Contractor information requirements necessary to support the power extension package project of the space shuttle program are specified for the following categories of data: project management; configuration management; systems engineering and test; manufacturing; reliability, quality assurance and safety; logistics; training; and operations.
2014-08-12
ISS040-E-091673 (12 Aug. 2014) --- In the Zvezda Service Module, European Space Agency astronaut Alexander Gerst (right) and Russian cosmonaut Alexander Skvortsov, both Expedition 40 flight engineers, take a brief moment for a photo during the approach and docking operations of ESA's "Georges Lemaitre" Automated Transfer Vehicle-5 (ATV-5) to the International Space Station.
The Waukesha Turbocharger Control Module: A tool for improved engine efficiency and response
DOE Office of Scientific and Technical Information (OSTI.GOV)
Zurlo, J.R.; Reinbold, E.O.; Mueller, J.
1996-12-31
The Waukesha Turbocharger Control Module allows optimum control of turbochargers on lean burn gaseous fueled engines. The Turbocharger Control Module is user programmed to provide either maximum engine efficiency or best engine response to load changes. In addition, the Turbocharger Control Module prevents undesirable turbocharger surge. The Turbocharger Control Module consists of an electronic control box, engine speed, intake manifold pressure, ambient temperature sensors, and electric actuators driving compressor bypass and wastegate valves. The Turbocharger Control Module expands the steady state operational environment of the Waukesha AT27GL natural gas engine from sea level to 1,525 m altitude with one turbochargermore » match and improves the engine speed turn down by 80 RPM. Finally, the Turbocharger Control Module improves engine response to load changes.« less
GAIA payload module mechanical development
NASA Astrophysics Data System (ADS)
Touzeau, S.; Sein, E.; Lebranchu, C.
2017-11-01
Gaia is the European Space Agency's cornerstone mission for global space astrometry. Its goal is to make the largest, most precise three-dimensional map of our Galaxy by surveying an unprecedented number of stars. This paper gives an overview of the mechanical system engineering and verification of the payload module. This development includes several technical challenges. First of all, the very high stability performance as required for the mission is a key driver for the design, which incurs a high degree of stability. This is achieved through the extensive use of Silicon Carbide (Boostec® SiC) for both structures and mirrors, a high mechanical and thermal decoupling between payload and service modules, and the use of high-performance engineering tools. Compliance of payload mass and volume with launcher capability is another key challenge, as well as the development and manufacturing of the 3.2-meter diameter toroidal primary structure. The spacecraft mechanical verification follows an innovative approach, with direct testing on the flight model, without any dedicated structural model.
2017-02-15
Charles Spern, at right, project manager on the Engineering Services Contract (ESC), and Glenn Washington, ESC quality assurance specialist, perform final inspections of the Veggie Series 1 plant experiment inside a laboratory in the Space Station Processing Facility at NASA's Kennedy Space Center in Florida. At far left is Dena Richmond, ESC configuration management. The Series 1 experiment is being readied for flight aboard Orbital ATK's Cygnus module on its seventh (OA-7) Commercial Resupply Services mission to the International Space Station. The Veggie system is on the space station.
2013-06-15
ISS036-E-008165 (15 June 2013) --- Expedition 36 Flight Engineer Fyodor Yurchikhin with Russia's Federal Space Agency (Roscosmos) takes pictures of a highly anticipated event from a window in the Pirs module on the International Space Station. His electronic still camera is equipped with a 400mm lens to capture distant images of the European Space Agency's Automated Transfer Vehicle-4 (ATV-4) “Albert Einstein.” The spacecraft eventually moved in much closer and successfully docked to the orbital outpost at 2:07 GMT, June 15, 2013, following a ten-day period of free-flight.
Orbital ATK CRS-7 "What's on Board" Science Briefing
2017-04-17
Paul Escalera, Orbital ATK staff systems engineer, speaks to NASA Social participants about the Cygnus pressurized cargo module during a "What's on Board" science briefing at the agency's Kennedy Space Center in Florida. The briefing was for Orbital ATK's seventh commercial ressuply services mission, CRS-7, to the International Space Station. Orbital ATK's Cygnus module is set to launch on the United Launch Alliance Atlas V rocket from Space Launch Complex 41 at Cape Canaveral Air Force Station on April 18. Liftoff is scheduled for 11:11 a.m. EDT.
The Apollo 17 far ultraviolet spectrometer experiment
NASA Technical Reports Server (NTRS)
Fastie, W. G.
1972-01-01
The Apollo 17 command service module in lunar orbit will carry a far ultraviolet scanning spectrometer whose prime mission will be to measure the composition of the lunar atmosphere. Additional observations will include the spectral lunar albedo, the temporary atmosphere injected by the engines of the lunar exploration module, the solar system atmosphere, the galactic atmosphere and the spectra of astronomical sources, including the earth. A detailed description of the experimental equipment which observes the spectral range 1180 to 1680 A, the observing program and broad speculation about the possible results of the experiment, are presented.
The Soyuz Taxi crew pose for a group photo in Zvezda during Expedition Three
2001-10-23
ISS003-E-7033 (23-31 October 2001) --- The Soyuz Taxi crewmembers assemble for a group photo in the Zvezda Service Module on the International Space Station (ISS). From the left are Flight Engineer Konstantin Kozeev, Commander Victor Afanasyev, and French Flight Engineer Claudie Haignere. Afanasyev and Kozeev represent Rosaviakosmos, and Haignere represents ESA, carrying out a flight program for CNES, the French Space Agency, under a commercial contract with the Russian Aviation and Space Agency. This image was taken with a digital still camera.
2013-12-04
ISS038-E-011708 (4 Dec. 2013) --- In the International Space Station?s Zvezda Service Module, Russian cosmonaut Sergey Ryazanskiy, Expedition 38 flight engineer, reads a procedures checklist during an emergency simulation drill with participation from flight controllers on the ground. During the exercise, the crew practiced emergency communication and procedures in response to a predetermined scenario such as pressure leak.
Fincke inside the Progress Vehicle with open SM/Progress transfer hatch during Expedition 9
2004-08-14
ISS009-E-18533 (14 August 2004) --- Astronaut Edward M. (Mike) Fincke, Expedition 9 NASA ISS science officer and flight engineer, appears behind the probe-and-cone mechanism on the hatch of the Progress 15 supply vehicle docked to the aft port on the Zvezda Service Module of the International Space Station (ISS).
Romanenko works with the Electronic Nose (Enose) Hardware in the SM
2013-02-21
ISS034-E-051551 (21 Feb. 2013) --- Cosmonaut Roman Romanenko, Expedition 34 flight engineer, works with the Electronic Nose hardware in the Zvezda service module aboard the International Space Station in Earth orbit. This hardware is used to measure contamination in the environment should there be hard to detect chemical leaks or spills.
Heavy Duty Mechanics Apprenticeship Training, Module One. Volume II.
ERIC Educational Resources Information Center
Batchelor, Leslie A.; Abercrombie, Richard, Ed.
This training manual, the second of two volumes, comprises the final three blocks in a nine-block in-service training course for apprentices working in heavy duty mechanics. Addressed in the individual blocks included in this volume are engines, basic electricity, and winches. Each block contains a section on parts theory that gives the purpose,…
ERIC Educational Resources Information Center
Lyon, Liz
2016-01-01
This article presents a case study where students aspiring to professional library roles who need to understand diverse disciplinary research data practices are placed in a laboratory with domain researchers during an immersive module within graduate MLIS programs at the School of Information Sciences (iSchool), University of Pittsburgh. A…
Bursch, Ross and Smith talk in Zvezda during STS-110's visit to the ISS
2002-04-09
STS110-E-5122 (10 April 2002) --- Astronauts Daniel W. Bursch (left), Expedition Four flight engineer, Jerry L. Ross and Steven L. Smith, both STS-110 mission specialists, converse in the Zvezda Service Module on the International Space Station (ISS). The image was taken with a digital still camera.
Expedition 30 crewmembers look at crew procedures in the SM
2012-03-24
ISS030-E-173973 (24 March 2012) --- NASA astronaut Dan Burbank (second left), Expedition 30 commander; along with Russian cosmonauts Oleg Kononenko (left) and Anton Shkaplerov and NASA astronaut Don Pettit, all flight engineers, are pictured in the Zvezda Service Module of the International Space Station as they prepare to move to the appropriate Soyuz vehicles, due to the possibility that space debris could pass close to the station. Burbank, Shkaplerov and Ivanishin sheltered in the Soyuz TMA-22 spacecraft attached to the Poisk Mini-Research Module 2 (MRM2) while Kononenko, Kuipers and Pettit took to the Soyuz TMA-03M docked to the Rassvet Mini-Research Module 1 (MRM-1).
78 FR 42758 - 36(b)(1) Arms Sales Notification
Federal Register 2010, 2011, 2012, 2013, 2014
2013-07-17
... aircraft, to include: Inlet/Fan Modules, Core Engine Modules, Rear Compressor Drive Turbines, Fan Drive...-PW-229 engines for the Hellenic Air Force F-16 aircraft, to include: Inlet/Fan Modules, Core Engine Modules, Rear Compressor Drive Turbines, Fan Drive Turbine Modules, Augmentor Duct and Nozzle Modules, and...
NASA Technical Reports Server (NTRS)
Bielozer, M.; VanLear, Benjamin S.; Kindred, N.; Monien, G.; Schulte, U.
2014-01-01
A concept of operations for the Assembly, Integration and Testing (AIT) and the Ground Systems Development Operations (GSDO) of the European Service Module (ESM) propulsion system has been developed. The AIT concept of operations covers all fabrication, integration and testing activities in both Europe and in the United States. The GSDO Program develops the facilities, equipment, and procedures for the loading of hypergolic propellants, the filling of high-pressure gases, and contingency de-servicing operations for the ESM. NASA and ESA along with the Lockheed Martin and Airbus Space and Defense are currently working together for the EM-1 and EM-2 missions in which the ESM will be flown as part of the Orion Multi-Purpose Crew Vehicle (MPCV). The NASA/ESA SM propulsion team is collaborating with the AIT personnel from ESA/Airbus and NASA/Lockheed Martin to ensure successful integration of the European designed Service Module propulsion system, the Lockheed Martin designed Crew Module Adapter and the heritage Space Shuttle Orbital Maneuvering System Engines (OMS-E) being provided as Government Furnished Equipment (GFE). This paper will provide an overview of the current AIT and GSDO concept of operations for the ESM propulsion system.
NASA Technical Reports Server (NTRS)
Bielozer, Matthew C.
2014-01-01
A concept of operations for the Assembly, Integration and Testing (AIT) and the Ground Systems Development Operations (GSDO) of the European Service Module (ESM) propulsion system has been developed. The AIT concept of operations covers all fabrication, integration and testing activities in both Europe and in the United States. The GSDO Program develops the facilities, equipment, and procedures for the loading of hypergolic propellants, the filling of high-pressure gases, and contingency de-servicing operations for the ESM. NASA and ESA along with the Lockheed Martin and Airbus Space and Defense are currently working together for the EM-1 and EM-2 missions in which the ESM will be flown as part of the Orion Multi-Purpose Crew Vehicle (MPCV). The NASA/ESA SM propulsion team is collaborating with the AIT personnel from ESA/Airbus and NASA/Lockheed Martin to ensure successful integration of the European designed Service Module propulsion system, the Lockheed Martin designed Crew Module Adapter and the heritage Space Shuttle Orbital Maneuvering System Engines (OMS-E) being provided as Government Furnished Equipment (GFE). This paper will provide an overview of the current AIT and GSDO concept of operations for the ESM propulsion system.
2009-02-16
CAPE CANAVERAL, Fla. – In high bay 4 of the Vehicle Assembly Building at NASA's Kennedy Space Center, workers lift the Ares I-X crew module mock-up from a work stand for a fit check with a mock-up of the service module. When fully developed, the 16-foot diameter crew module will furnish living space and reentry protection for future astronauts, and the service module’s main engine will be used to break out of lunar orbit for the return trip to Earth. Ares I-X is the test flight for the Ares I, which is part of the Constellation Program to return men to the moon and beyond. The I-X flight will provide NASA an early opportunity to test and prove hardware, facilities and ground operations associated with Ares I launches. Targeted for the summer of 2009, the launch of the full-scale Ares I-X will be the first in a series of unpiloted rocket launches from Kennedy. Photo credit: NASA/Jack Pfaller
2009-02-16
CAPE CANAVERAL, Fla. – In high bay 4 of the Vehicle Assembly Building at NASA's Kennedy Space Center, workers position the Ares I-X crew module mock-up onto a mock-up of the service module during a fit check of the hardware. When fully developed, the 16-foot diameter crew module will furnish living space and reentry protection for future astronauts, and the service module’s main engine will be used to break out of lunar orbit for the return trip to Earth. Ares I-X is the test flight for the Ares I, which is part of the Constellation Program to return men to the moon and beyond. The I-X flight will provide NASA an early opportunity to test and prove hardware, facilities and ground operations associated with Ares I launches. Targeted for the summer of 2009, the launch of the full-scale Ares I-X will be the first in a series of unpiloted rocket launches from Kennedy. Photo credit: NASA/Jack Pfaller
2009-02-16
CAPE CANAVERAL, Fla. – In high bay 4 of the Vehicle Assembly Building at NASA's Kennedy Space Center, workers lower the Ares I-X crew module mock-up onto a mock-up of the service module during a fit check of the hardware. When fully developed, the 16-foot diameter crew module will furnish living space and reentry protection for future astronauts, and the service module’s main engine will be used to break out of lunar orbit for the return trip to Earth. Ares I-X is the test flight for the Ares I, which is part of the Constellation Program to return men to the moon and beyond. The I-X flight will provide NASA an early opportunity to test and prove hardware, facilities and ground operations associated with Ares I launches. Targeted for the summer of 2009, the launch of the full-scale Ares I-X will be the first in a series of unpiloted rocket launches from Kennedy. Photo credit: NASA/Jack Pfaller
2009-02-16
CAPE CANAVERAL, Fla. – In high bay 4 of the Vehicle Assembly Building at NASA's Kennedy Space Center, the Ares I-X crew module mock-up hangs suspended from a crane as it is moved for a fit check with a mock-up of the service module. When fully developed, the 16-foot diameter crew module will furnish living space and reentry protection for future astronauts, and the service module’s main engine will be used to break out of lunar orbit for the return trip to Earth. Ares I-X is the test flight for the Ares I, which is part of the Constellation Program to return men to the moon and beyond. The I-X flight will provide NASA an early opportunity to test and prove hardware, facilities and ground operations associated with Ares I launches. Targeted for the summer of 2009, the launch of the full-scale Ares I-X will be the first in a series of unpiloted rocket launches from Kennedy. Photo credit: NASA/Jack Pfaller
2009-02-16
CAPE CANAVERAL, Fla. – In high bay 4 of the Vehicle Assembly Building at NASA's Kennedy Space Center, the Ares I-X crew module mock-up is positioned onto a mock-up of the service module to determine that the pieces of hardware are a perfect fit. When fully developed, the 16-foot diameter crew module will furnish living space and reentry protection for future astronauts, and the service module’s main engine will be used to break out of lunar orbit for the return trip to Earth. Ares I-X is the test flight for the Ares I, which is part of the Constellation Program to return men to the moon and beyond. The I-X flight will provide NASA an early opportunity to test and prove hardware, facilities and ground operations associated with Ares I launches. Targeted for the summer of 2009, the launch of the full-scale Ares I-X will be the first in a series of unpiloted rocket launches from Kennedy. Photo credit: NASA/Jack Pfaller
Padalka spins a box of chocolates as Kaleri looks on in the SM during EXP 9 / EXP 8
2004-04-22
ISS008-E-22002 (22 April 2004) --- Cosmonaut Gennady I. Padalka, Expedition 9 commander, spins a box of chocolates as cosmonaut Alexander Y. Kaleri, Expedition 8 flight engineer, looks on in the Zvezda Service Module on the International Space Station (ISS). Padalka and Kaleri represent Russias Federal Space Agency.
Expedition Three crew pose for a group photo in Zvezda during Expedition Three
2001-10-01
ISS003-E-7044 (October 2001) --- Astronaut Frank L. Culbertson, Jr. (center), Expedition Three mission commander, flanked by cosmonauts Mikhail Tyurin and Vladimir N. Dezhurov, both flight engineers, assemble for a group photo in the Zvezda Service Module on the International Space Station (ISS). Tyurin and Dezhurov represent Rosaviakosmos. This image was taken with a digital still camera.
2015-04-08
ISS043E091650 (04/08/2015) --- A view of the food table located in the Russian Zvezda service module on the International Space Station taken by Expedition 43 Flight Engineer Scott Kelly. Assorted food, drink and condiment packets are visible. Kelly tweeted this image along with the comment: ""Looks messy, but it's functional. Our #food table on the @space station. What's for breakfast? #YearInSpace".
Expedition Six Flight Engineer Pettit uses a chemical/microbial analysis bag to collect water sample
2002-12-18
ISS006-E-08628 (18 December 2002) --- Astronaut Donald R. Pettit, Expedition Six NASA ISS science officer, is pictured in the Zvezda Service Module on the International Space Station (ISS) during the scheduled Week 3 potable water sampling and on-orbit chemical/microbial analysis of the SM environment control and life support system.
Expedition Six Flight Engineer Pettit uses a chemical/microbial analysis bag to collect water sample
2002-12-18
ISS006-E-08616 (18 December 2002) --- Astronaut Donald R. Pettit, Expedition Six NASA ISS science officer, is pictured in the Zvezda Service Module on the International Space Station (ISS) during the scheduled Week 3 potable water sampling and on-orbit chemical/microbial analysis of the SM environment control and life support system.
Modulation of high frequency noise by engine tones of small boats.
Pollara, Alexander; Sutin, Alexander; Salloum, Hady
2017-07-01
The effect of modulation of high frequency ship noise by propeller rotation frequencies is well known. This modulation is observed with the Detection of Envelope Modulation on Noise (DEMON) algorithm. Analysis of the DEMON spectrum allows the revolutions per minute and number of blades of the propeller to be determined. This work shows that the high frequency noise of a small boat can also be modulated by engine frequencies. Prior studies have not reported high frequency noise amplitude modulated at engine frequencies. This modulation is likely produced by bubbles from the engine exhaust system.
1999-02-25
KENNEDY SPACE CENTER, FLA. -- Cutting a red ribbon for the unveiling of a newly renovated altitude chamber are (left to right) Tommy Mack, project manager, NASA; Steve Francois, director, Space Station and Shuttle Payloads; Sterling Walker, director, Engineering Development; Roy Bridges, director, Kennedy Space Center; Jay Greene, International Space Station manager for Technical; Michael Terry, project manager, Boeing; and Terry Smith, director of Engineering, Boeing Space Coast Operations. The chamber was reactivated, after a 24-year hiatus, to perform leak tests on International Space Station pressurized modules at the launch site. Originally, two chambers were built to test the Apollo command and lunar service modules. They were last used in 1975 during the Apollo-Soyuz Test Project. After installation of new vacuum pumping equipment and controls, a new control room, and a new rotation handling fixture, the chamber again became operational in February 1999. The chamber, which is 33 feet in diameter and 50 feet tall, is constructed of stainless steel. The first module that will be tested for leaks is the U.S. Laboratory. No date has been determined for the test
The ribbon-cutting ceremony unveils the reactivated altitude chamber inside the O&C high bay
NASA Technical Reports Server (NTRS)
1999-01-01
Cutting a red ribbon for the unveiling of a newly renovated altitude chamber are (left to right) Tommy Mack, project manager, NASA; Steve Francois, director, Space Station and Shuttle Payloads; Sterling Walker, director, Engineering Development; Roy Bridges, director, Kennedy Space Center; Jay Greene, International Space Station manager for Technical; Michael Terry, project manager, Boeing; and Terry Smith, director of Engineering, Boeing Space Coast Operations. The chamber was reactivated, after a 24-year hiatus, to perform leak tests on International Space Station pressurized modules at the launch site. Originally, two chambers were built to test the Apollo command and lunar service modules. They were last used in 1975 during the Apollo-Soyuz Test Project. After installation of new vacuum pumping equipment and controls, a new control room, and a new rotation handling fixture, the chamber again became operational in February 1999. The chamber, which is 33 feet in diameter and 50 feet tall, is constructed of stainless steel. The first module that will be tested for leaks is the U.S. Laboratory. No date has been determined for the test.
Line drawing of Apollo 14 Command/Service Modules
1971-01-12
S71-16823 (January 1971) --- A line drawing illustrating a cutaway view of the Apollo 14 Command and Service Modules, showing the engineering changes in the CSM which were recommended by the Apollo 13 Review Board. (The Apollo 13 abort was caused by a short circuit and wiring overheating in one of the SM cryogenic oxygen tanks.) The major changes to the Apollo 14 CSM include adding a third cryogenic oxygen tank installed in a heretofore empty bay (in sector one) of the SM, addition of an auxiliary battery in the SM as a backup in case of fuel cell failure, and removal of destratification fans in the cryogenic oxygen tanks and removal of thermostat switches from the oxygen tank heater circuits. Provision for stowage of an emergency five-gallon supply of drinking water has been added to the CM.
Taxi and Expedition Three crews pose for a group photo in Zvezda during Expedition Three
2001-10-23
ISS003-E-7036 (23-31 October 2001) --- Astronaut Frank L. Culbertson, Jr. (foreground), Expedition Three mission commander, and the Soyuz Taxi crewmembers assemble for a group photo in the Zvezda Service Module on the International Space Station (ISS). From the left are Flight Engineer Konstantin Kozeev, Commander Victor Afanasyev, and French Flight Engineer Claudie Haignere. Afanasyev and Kozeev represent Rosaviakosmos, and Haignere represents ESA, carrying out a flight program for CNES, the French Space Agency, under a commercial contract with the Russian Aviation and Space Agency. This image was taken with a digital still camera.
Taxi and Expedition Three crews pose for a group photo in Zvezda during Expedition Three
2001-10-23
ISS003-E-7037 (23-31 October 2001) --- Astronaut Frank L. Culbertson, Jr. (foreground), Expedition Three mission commander, and the Soyuz Taxi crewmembers assemble for a group photo in the Zvezda Service Module on the International Space Station (ISS). From the left are Flight Engineer Konstantin Kozeev, Commander Victor Afanasyev, and French Flight Engineer Claudie Haignere. Afanasyev and Kozeev represent Rosaviakosmos, and Haignere represents ESA, carrying out a flight program for CNES, the French Space Agency, under a commercial contract with the Russian Aviation and Space Agency. This image was taken with a digital still camera.
2014-06-08
CAPE CANAVERAL, Fla. -- Inside the Operations and Checkout Building high bay at NASA's Kennedy Space Center in Florida, the Orion service module has been secured in the Final Assembly and System Testing, or FAST, cell. The Orion crew module will be stacked on the service module in the FAST cell and then both modules will be put through their final system tests for Exploration Flight Test-1, or EFT-1, before rolling out of the facility for integration with the United Launch Alliance Delta IV Heavy rocket. Orion is the exploration spacecraft designed to carry astronauts to destinations not yet explored by humans, including an asteroid and Mars. It will have emergency abort capability, sustain the crew during space travel and provide safe re-entry from deep space return velocities. The first unpiloted test flight of Orion, EFT-1, is scheduled to launch later this year atop a Delta IV rocket from Cape Canaveral Air Force Station in Florida to an altitude of 3,600 miles above the Earth's surface. The two-orbit, four-hour flight test will help engineers evaluate the systems critical to crew safety including the heat shield, parachute system and launch abort system. For more information, visit http://www.nasa.gov/orion. Photo credit: NASA/Glenn Benson
2014-06-08
CAPE CANAVERAL, Fla. -- Inside the Operations and Checkout Building high bay at NASA's Kennedy Space Center in Florida, the Orion service module has been secured in the Final Assembly and System Testing, or FAST, cell. The Orion crew module will be stacked on the service module in the FAST cell and then both modules will be put through their final system tests for Exploration Flight Test-1, or EFT-1, before rolling out of the facility for integration with the United Launch Alliance Delta IV Heavy rocket. Orion is the exploration spacecraft designed to carry astronauts to destinations not yet explored by humans, including an asteroid and Mars. It will have emergency abort capability, sustain the crew during space travel and provide safe re-entry from deep space return velocities. The first unpiloted test flight of Orion, EFT-1, is scheduled to launch later this year atop a Delta IV rocket from Cape Canaveral Air Force Station in Florida to an altitude of 3,600 miles above the Earth's surface. The two-orbit, four-hour flight test will help engineers evaluate the systems critical to crew safety including the heat shield, parachute system and launch abort system. For more information, visit http://www.nasa.gov/orion. Photo credit: NASA/Glenn Benson
NASA Ames Research Center R and D Services Directorate Biomedical Systems Development
NASA Technical Reports Server (NTRS)
Pollitt, J.; Flynn, K.
1999-01-01
The Ames Research Center R&D Services Directorate teams with NASA, other government agencies and/or industry investigators for the development, design, fabrication, manufacturing and qualification testing of space-flight and ground-based experiment hardware for biomedical and general aerospace applications. In recent years, biomedical research hardware and software has been developed to support space-flight and ground-based experiment needs including the E 132 Biotelemetry system for the Research Animal Holding Facility (RAHF), E 100 Neurolab neuro-vestibular investigation systems, the Autogenic Feedback Systems, and the Standard Interface Glove Box (SIGB) experiment workstation module. Centrifuges, motion simulators, habitat design, environmental control systems, and other unique experiment modules and fixtures have also been developed. A discussion of engineered systems and capabilities will be provided to promote understanding of possibilities for future system designs in biomedical applications. In addition, an overview of existing engineered products will be shown. Examples of hardware and literature that demonstrate the organization's capabilities will be displayed. The Ames Research Center R&D Services Directorate is available to support the development of new hardware and software systems or adaptation of existing systems to meet the needs of academic, commercial/industrial, and government research requirements. The Ames R&D Services Directorate can provide specialized support for: System concept definition and feasibility Mathematical modeling and simulation of system performance Prototype hardware development Hardware and software design Data acquisition systems Graphical user interface development Motion control design Hardware fabrication and high-fidelity machining Composite materials development and application design Electronic/electrical system design and fabrication System performance verification testing and qualification.
Assessment of SEPS solar array technology for orbital service module application
NASA Technical Reports Server (NTRS)
1978-01-01
Work performed in the following assessment areas on the SEPS solar array is reported: (1) requirements definition, (2) electrical design evaluation, (3) mechanical design evaluation, and (4) design modification analysis. General overall assessment conclusions are summarized. There are no known serious design limitations involved in the implementation of the recommended design modifications. A section of orbiter and array engineering drawings is included.
Kuipers sets up the EHS/TEPC Spectrometer and Detector Assembly in the SM
2012-03-12
ISS030-E-177101 (12 March 2012) --- European Space Agency astronaut Andre Kuipers, Expedition 30 flight engineer, sets up the Environmental Health System / Tissue Equivalent Proportional Counter (EHS/TEPC) spectrometer and detector assembly on panel 327 in the Zvezda Service Module of the International Space Station. The TEPC detector assembly is the primary radiation measurement tool on the space station.
Dezhurov works with electronic equipment in Zvezda during Expedition Three
2001-08-01
ISS003-E-5486 (August 2001) --- Cosmonaut Vladimir Dezhurov of Rosaviakosmos, Expedition Three flight engineer, works on electronic equipment behind a panel in the Zvezda Service Module. Please note: The date identifiers on some frames are not accurate due to a technical problem with one of the Expedition Three cameras. When a specific date is given in the text or description portion, it is correct.
Dezhurov works with electronic equipment in Zvezda during Expedition Three
2001-08-01
ISS003-E-5489 (August 2001) --- Cosmonaut Vladimir Dezhurov of Rosaviakosmos, Expedition Three flight engineer, works on electronic equipment behind a panel in the Zvezda Service Module. Please note: The date identifiers on some frames are not accurate due to a technical problem with one of the Expedition Three cameras. When a specific date is given in the text or description portion, it is correct.
NASA Astrophysics Data System (ADS)
Li, Chao; Hu, Chunbo; Zhu, Xiaofei; Hu, Jiaming; Li, Yue; Hu, Xu
2018-06-01
Powdered Mg and CO2 bipropellant engine providing a practical demonstration of in situ resource utilization (ISRU) for Mars Sample Return (MSR) mission seems to be feasible by current investigations. However, essential functions of the engine to satisfy the complicated ballistics requirements such as thrust modulation and multiple pulse have not been established yet. The aim of this experimental study is to evaluate the engine's thrust modulation feasibility and to investigate its thrust modulation characteristics. A powdered Mg and CO2 bipropellant engine construction aiming to achieve thrust modulation ability was proposed. A mass flow rate calibration experiment to evaluate the gas-solid mass flow rate regulating performance was conducted before fire tests. Fire test result shows that the engine achieved successful ignition as well as self-sustaining combustion; Thrust modulation of the engine is feasible, detail thrust estimating result of the test shows that maximum thrust is 135.91 N and the minimum is 5.65 N with a 22.11 thrust modulation ratio, moreover, the transportation period is quick and the thrust modulation ratio is adjustable. At the same time, the powder feed system reaches a two-step flow rate regulating with a modulation ratio of 4.5-5. What' more, caused by the uneven engine working conditions, there is an obvious difference in combustion efficiency value, maximum combustion efficiency of the powdered Mg and CO2 bipropellant engine is 80.20%.
A WorkFlow Engine Oriented Modeling System for Hydrologic Sciences
NASA Astrophysics Data System (ADS)
Lu, B.; Piasecki, M.
2009-12-01
In recent years the use of workflow engines for carrying out modeling and data analyses tasks has gained increased attention in the science and engineering communities. Tasks like processing raw data coming from sensors and passing these raw data streams to filters for QA/QC procedures possibly require multiple and complicated steps that need to be repeated over and over again. A workflow sequence that carries out a number of steps of various complexity is an ideal approach to deal with these tasks because the sequence can be stored, called up and repeated over again and again. This has several advantages: for one it ensures repeatability of processing steps and with that provenance, an issue that is increasingly important in the science and engineering communities. It also permits the hand off of lengthy and time consuming tasks that can be error prone to a chain of processing actions that are carried out automatically thus reducing the chance for error on the one side and freeing up time to carry out other tasks on the other hand. This paper aims to present the development of a workflow engine embedded modeling system which allows to build up working sequences for carrying out numerical modeling tasks regarding to hydrologic science. Trident, which facilitates creating, running and sharing scientific data analysis workflows, is taken as the central working engine of the modeling system. Current existing functionalities of the modeling system involve digital watershed processing, online data retrieval, hydrologic simulation and post-event analysis. They are stored as sequences or modules respectively. The sequences can be invoked to implement their preset tasks in orders, for example, triangulating a watershed from raw DEM. Whereas the modules encapsulated certain functions can be selected and connected through a GUI workboard to form sequences. This modeling system is demonstrated by setting up a new sequence for simulating rainfall-runoff processes which involves embedded Penn State Integrated Hydrologic Model(PIHM) module for hydrologic simulation as a kernel, DEM processing sub-sequence which prepares geospatial data for PIHM, data retrieval module which access time series data from online data repository via web services or from local database, post- data management module which stores , visualizes and analyzes model outputs.
AUTOMOTIVE DIESEL MAINTENANCE 1. UNIT VII, ENGINE TUNE-UP--DETROIT DIESEL ENGINE.
ERIC Educational Resources Information Center
Human Engineering Inst., Cleveland, OH.
THIS MODULE OF A 30-MODULE COURSE IS DESIGNED TO DEVELOP AN UNDERSTANDING OF TUNE-UP PROCEDURES FOR DIESEL ENGINES. TOPICS ARE SCHEDULING TUNE-UPS, AND TUNE-UP PROCEDURES. THE MODULE CONSISTS OF A SELF-INSTRUCTIONAL BRANCH PROGRAMED TRAINING FILM "ENGINE TUNE-UP--DETROIT DIESEL ENGINE" AND OTHER MATERIALS. SEE VT 005 655 FOR FURTHER INFORMATION.…
Test results of a Stirling engine utilizing heat exchanger modules with an integral heat pipe
NASA Astrophysics Data System (ADS)
Skupinski, Robert C.; Tower, Leonard K.; Madi, Frank J.; Brusk, Kevin D.
1993-04-01
The Heat Pipe Stirling Engine (HP-1000), a free-piston Stirling engine incorporating three heat exchanger modules, each having a sodium filled heat pipe, has been tested at the NASA-Lewis Research Center as part of the Civil Space Technology Initiative (CSTI). The heat exchanger modules were designed to reduce the number of potential flow leak paths in the heat exchanger assembly and incorporate a heat pipe as the link between the heat source and the engine. An existing RE-1000 free-piston Stirling engine was modified to operate using the heat exchanger modules. This paper describes heat exchanger module and engine performance during baseline testing. Condenser temperature profiles, brake power, and efficiency are presented and discussed.
Test results of a Stirling engine utilizing heat exchanger modules with an integral heat pipe
NASA Technical Reports Server (NTRS)
Skupinski, Robert C.; Tower, Leonard K.; Madi, Frank J.; Brusk, Kevin D.
1993-01-01
The Heat Pipe Stirling Engine (HP-1000), a free-piston Stirling engine incorporating three heat exchanger modules, each having a sodium filled heat pipe, has been tested at the NASA-Lewis Research Center as part of the Civil Space Technology Initiative (CSTI). The heat exchanger modules were designed to reduce the number of potential flow leak paths in the heat exchanger assembly and incorporate a heat pipe as the link between the heat source and the engine. An existing RE-1000 free-piston Stirling engine was modified to operate using the heat exchanger modules. This paper describes heat exchanger module and engine performance during baseline testing. Condenser temperature profiles, brake power, and efficiency are presented and discussed.
The design and fabrication of a Stirling engine heat exchanger module with an integral heat pipe
NASA Technical Reports Server (NTRS)
Schreiber, Jeffrey G.
1988-01-01
The conceptual design of a free-piston Stirling Space Engine (SSE) intended for space power applications has been generated. The engine was designed to produce 25 kW of electric power with heat supplied by a nuclear reactor. A novel heat exchanger module was designed to reduce the number of critical joints in the heat exchanger assembly while also incorporating a heat pipe as the link between the engine and the heat source. Two inexpensive verification tests are proposed. The SSE heat exchanger module is described and the operating conditions for the module are outlined. The design process of the heat exchanger modules, including the sodium heat pipe, is briefly described. Similarities between the proposed SSE heat exchanger modules and the LeRC test modules for two test engines are presented. The benefits and weaknesses of using a sodium heat pipe to transport heat to a Stirling engine are discussed. Similarly, the problems encountered when using a true heat pipe, as opposed to a more simple reflux boiler, are described. The instruments incorporated into the modules and the test program are also outlined.
ERIC Educational Resources Information Center
Human Engineering Inst., Cleveland, OH.
THIS MODULE OF A 30-MODULE COURSE IS DESIGNED TO DEVELOP AN UNDERSTANDING OF THE OPERATION AND MAINTENANCE OF THE DIESEL ENGINE FUEL SYSTEM AND THE PROCEDURES FOR DIESEL ENGINE INSTALLATION. TOPICS ARE FUEL FLOW CHARACTERISTICS, PTG FUEL PUMP, PREPARATION FOR INSTALLATION, AND INSTALLING ENGINE. THE MODULE CONSISTS OF A SELF-INSTRUCTIONAL BRANCH…
Encapsulant selection and durability testing experience
NASA Technical Reports Server (NTRS)
Cuddihy, E. F.
1985-01-01
The Flat Plate Solar Array Project (FSA) has established technically challenging cost and service life goals for photovoltaic modules. These goals are a cost of $70 sq m and an expected 30 years of service life in an outdoor weathering environment. out of the cost goal, $14 sq m is allocated for encapsulation materials, which includes the cost of a structural panel. At FSA's inception in 1975, the cumulative cost of encapsulation materials in popular use, such as room temperature vulcanized (RTV) silicones, aluminum panels, etc., greatly exceeded $14/sq m. Accordingly, it became necessary to identify and/or develop new materials and new material technologies to achieve the goals. Many of these new materials are low cost polymers that satisfy module engineering and encapsulation processing requirements but unfortunately are not intrinsically weather stable. This necessitates identifying lifetime and/or weathering deficiencies inherent in these low cost materials and developing specific approaches to enhancing weather stability.
STS-97 and Expedition One crewmembers pose for a photo in the Service Module
2000-12-08
STS097-326-031 (8 December 2000)--- When the five STS-97 astronauts paid a visit to the three Expedition 1 crew members onboard the International Space Station (ISS), they all posed for a traditional in-flight portrait, albeit for the first time in the Zvezda Service Module. On the front row are (left to right) astronauts Brent W. Jett, Jr., STS-97 commander; William M. Shepherd, Expedition 1 mission commander; and Joseph R. Tanner, STS-97 mission specialist. On the second row are (from the left) cosmonaut Sergei K. Krikalev, Expedition 1 flight engineer; astronaut Carlos I. Noriega, STS-97 mission specialist; cosmonaut Yuri P. Gidzenko, Expedition 1 Soyuz commander; and astronaut Michael J. Bloomfield, STS-97 pilot. Behind them is astronaut Marc Garneau, STS-97 mission specialist representing the Canadian Space Agency (CSA). Krikalev and Gidzenko represent the Russian Aviation and Space Agency.
STS-97 and Expedition One crewmembers pose for a photo in the Service Module
2000-12-08
STS097-313-001 (8 December 2000)--- When the five STS-97 astronauts paid a visit to the three Expedition 1 crew members onboard the International Space Station (ISS), they all posed for a traditional in-flight portrait, albeit for the first time in the Zvezda Service Module. On the front row are (left to right) astronauts Brent W. Jett, Jr., STS-97 commander; William M. Shepherd, Expedition 1 mission commander; and Joseph R. Tanner, STS-97 mission specialist. On the second row are (from the left) cosmonaut Sergei K. Krikalev, Expedition 1 flight engineer; astronaut Carlos I. Noriega, STS-97 mission specialist; cosmonaut Yuri P. Gidzenko, Expedition 1 Soyuz commander; and astronaut Michael J. Bloomfield, STS-97 pilot. Behind them is astronaut Marc Garneau, STS-97 mission specialist representing the Canadian Space Agency (CSA). Krikalev and Gidzenko represent the Russian Aviation and Space Agency.
Meal for Expedition Two, Three and STS-105 crews in the ISS Service Module/Zvezda
2001-08-15
STS105-E-5201 (15 August 2001) --- Part of the "dessert" course for one of the first meals shared by the STS-105 and Expedition Two crews was the issuance of mission shirts for the departing station occupants. Holding new jerseys in the Zvezda Service Module on the right side of the frame are astronauts Susan J. Helms and James S. Voss, departing flight engineers, and cosmonaut Yury V. Usachev, Expedition Two commander. Clockwise from the lower left corner are astronaut Frederick W. (Rick) Sturckow, cosmonauts Vladimir Dezhurov and Mikhail Tyurin, Helms, astronaut Frank L. Culbertson, Jr., Usachev, Voss and astronaut Patrick G. Forrester. Astronauts Daniel T. Barry and Scott J. Horowitz are out of frame. Usachev, Dezhurov and Tyurin all represent Rosaviakosmos. PLEASE NOTE: This event occurred on August 14, according to Central Daylight Time (CDT) but it was already the following day in Greenwich Mean Time (GMT).
View of Kotov working with Debris Panels during EVA18
2007-05-30
ISS015-E-10043 (30 May 2007) --- Cosmonaut Oleg V. Kotov, Expedition 15 flight engineer representing Russia's Federal Space Agency, wearing a Russian Orlan spacesuit, participates in a session of extravehicular activity (EVA). Among other tasks, Kotov and cosmonaut Fyodor N. Yurchikhin (out of frame), commander representing Russia's Federal Space Agency, retrieved the "Christmas tree" bundle of three packages of 17 protective debris panels for installation around the forward cone of the Zvezda Service Module of the International Space Station and to install the first set of those panels. The aluminum debris protection panels are designed to shield the module from micro-meteoroids.
Electrical Pressurization Concept for the Orion MPCV European Service Module Propulsion System
NASA Technical Reports Server (NTRS)
Meiss, Jan-Hendrik; Weber, Jorg; Ierardo, Nicola; Quinn, Frank D.; Paisley, Jonathan
2015-01-01
The paper presents the design of the pressurization system of the European Service Module (ESM) of the Orion Multi-Purpose Crew Vehicle (MPCV). Being part of the propulsion subsystem, an electrical pressurization concept is implemented to condition propellants according to the engine needs via a bang-bang regulation system. Separate pressurization for the oxidizer and the fuel tank permits mixture ratio adjustments and prevents vapor mixing of the two hypergolic propellants during nominal operation. In case of loss of pressurization capability of a single side, the system can be converted into a common pressurization system. The regulation concept is based on evaluation of a set of tank pressure sensors and according activation of regulation valves, based on a single-failure tolerant weighting of three pressure signals. While regulation is performed on ESM level, commanding of regulation parameters as well as failure detection, isolation and recovery is performed from within the Crew Module, developed by Lockheed Martin Space System Company. The overall design and development maturity presented is post Preliminary Design Review (PDR) and reflects the current status of the MPCV ESM pressurization system.
Kaleri works with the Pilot experiment during Expedition 8
2003-10-31
ISS008-E-05179 (31 October 2003) --- Cosmonaut Alexander Y. Kaleri, Expedition 8 flight engineer, works with the Russian biomedical Pilot experiment (MBI-15) in the Zvezda Service Module on the International Space Station (ISS). The experiment, which looks at psychological and physiological changes in crew performance during long-duration spaceflight, requires a worktable, ankle restraint system and two control handles for testing piloting skill. Kaleri represents Rosaviakosmos.
Dezhurov and Tyurin pose in Zvezda during Expedition Three
2001-08-01
ISS003-E-5498 (August 2001) --- Cosmonauts Mikhail Tyurin (left) and Vladimir Dezhurov, Expedition Three flight engineers, pose for a photograph in the Zvezda Service Module. Tyurin and Dezhurov represent Rosaviakosmos. Please note: The date identifiers on some frames are not accurate due to a technical problem with one of the Expedition Three cameras. When a specific date is given in the text or description portion, it is correct.
2007-02-22
ISS014-E-14500 (22 Feb. 2007) --- Cosmonaut Mikhail Tyurin, Expedition 14 flight engineer representing Russia's Federal Space Agency, wearing a Russian Orlan spacesuit, participates in a session of extravehicular activity (EVA). Among other tasks, Tyurin and astronaut Michael E. Lopez-Alegria (out of frame), commander and NASA space station science officer, were able to retract a stuck Kurs antenna on the Progress vehicle docked to the International Space Station's Zvezda Service Module.
Russian Extravehicular Activity (EVA) 17A.
2007-02-22
ISS014-E-14467 (22 Feb. 2007) --- Cosmonaut Mikhail Tyurin, Expedition 14 flight engineer representing Russia's Federal Space Agency, wearing a Russian Orlan spacesuit, participates in a session of extravehicular activity (EVA). Among other tasks, Tyurin and astronaut Michael E. Lopez-Alegria (out of frame), commander and NASA space station science officer, were able to retract a stuck Kurs antenna on the Progress vehicle docked to the International Space Station's Zvezda Service Module.
2007-02-22
ISS014-E-14502 (22 Feb. 2007) --- Cosmonaut Mikhail Tyurin, Expedition 14 flight engineer representing Russia's Federal Space Agency, wearing a Russian Orlan spacesuit, participates in a session of extravehicular activity (EVA). Among other tasks, Tyurin and astronaut Michael E. Lopez-Alegria (out of frame), commander and NASA space station science officer, were able to retract a stuck Kurs antenna on the Progress vehicle docked to the International Space Station's Zvezda Service Module.
2007-02-22
ISS014-E-14561 (22 Feb. 2007) --- Astronaut Michael E. Lopez-Alegria, Expedition 14 commander and NASA space station science officer, wearing a Russian Orlan spacesuit, participates in a session of extravehicular activity (EVA). Among other tasks, Lopez-Alegria and cosmonaut Mikhail Tyurin (out of frame), flight engineer representing Russia's Federal Space Agency, were able to retract a stuck antenna on the Progress vehicle docked to the International Space Station's Zvezda Service Module.
Russian Extravehicular Activity (EVA) 17A.
2007-02-22
ISS014-E-14469 (22 Feb. 2007) --- Cosmonaut Mikhail Tyurin, Expedition 14 flight engineer representing Russia's Federal Space Agency, wearing a Russian Orlan spacesuit, participates in a session of extravehicular activity (EVA). Among other tasks, Tyurin and astronaut Michael E. Lopez-Alegria (out of frame), commander and NASA space station science officer, were able to retract a stuck antenna on the Progress vehicle docked to the International Space Station's Zvezda Service Module.
Alexander Samokutyaev conducts BTKh-14/Bioemulsiya (Bioemulsion) Experiment
2011-05-05
ISS027-E-022454 (5 May 2011) --- Russian cosmonaut Alexander Samokutyaev, Expedition 27 flight engineer, uses a glovebox to service the Russian Bioemulsion science payload in the Poisk Mini-Research Module 2 (MRM2) of the International Space Station. The Bioemulsion experiment is attempting to develop faster technologies for obtaining microorganism biomass and biologically active substance biomass for creating highly efficient environmentally pure bacteria, enzymes, and medicinal/pharmaceutical preparations.
Hadfield works robotic controls in the Cupola Module
2013-01-10
ISS034-E-027317 (10 Jan. 2013) --- In the Cupola aboard the Earth-orbiting International Space Station, Canadian Space Agency astronaut Chris Hadfield, Expedition 34 flight engineer, works the controls at the Robotic workstation to maneuver the Space Station Remote Manipulator System (SSRMS) or CanadArm2 from its parked position to grapple the Mobile Remote Servicer (MRS) Base System (MBS) Power and Data Grapple Fixture 4 (PDGF-4).
FM Quieting Curves and Related Topics
1977-08-01
Electronics Engineering Group (EEO) is organized as an independent group reorting, directly to -the Comwiander, Air ’Force Conmmunica-r tions Service (WOC...NUMBER N/A 7. AklTHO -() 6. CONTRACT OR GRANT NUMBER(#) /, .C...or.e M./ Kizer/ , ,/A 9. PERFORMING ORGANIZATION NAME AND ADDRESS 10. PROGRAM ELEMENT...in vestigial sideband modulation) and are separated from the carrier frequency by a frequency difference equal to the frequency of the baseband
Dezhurov holds a GTS electronics unit in Zvezda during Expedition Three
2001-08-01
ISS003-E-5477 (August 2001) --- Cosmonaut Vladimir Dezhurov of Rosaviakosmos, Expedition Three flight engineer, holds a Global Time System (GTS) electronics unit in the Zvezda Service Module. Please note: The date identifiers on some frames are not accurate due to a technical problem with one of the Expedition Three cameras. When a specific date is given in the text or description portion, it is correct.
Foale and Kaleri pose beside the LADA-4 greenhouse in the U.S. Lab during Expedition 8
2004-04-12
ISS008-E-21916 (12 April 2004)--- Astronaut C. Michael Foale (left), Expedition 8 commander and NASA ISS science officer; and Alexander Kaleri, Russia's Federal Space Agency flight engineer, pose beside the pea plants growing in the Lada-4 greenhouse as part of the BIO-5 Rasteniya-2 (Plants-2) experiment located in the Zvezda Service Module of the International Space Station.
AUTOMOTIVE DIESEL MAINTENANCE 1. UNIT XX, CUMMINS DIESEL ENGINE, MAINTENANCE SUMMARY.
ERIC Educational Resources Information Center
Minnesota State Dept. of Education, St. Paul. Div. of Vocational and Technical Education.
THIS MODULE OF A 30-MODULE COURSE IS DESIGNED TO PROVIDE A SUMMARY OF THE REASONS AND PROCEDURES FOR DIESEL ENGINE MAINTENANCE. TOPICS ARE WHAT ENGINE BREAK-IN MEANS, ENGINE BREAK-IN, TORQUING BEARINGS (TEMPLATE METHOD), AND THE NEED FOR MAINTENANCE. THE MODULE CONSISTS OF A SELF-INSTRUCTIONAL BRANCH PROGRAMED TRAINING FILM "CUMMINS DIESEL ENGINE…
1969-11-19
AS12-48-7034 (19 Nov. 1969) --- A close-up view of a portion of quadrant II of the descent stage of the Apollo 12 Lunar Module (LM), photographed during the Apollo 12 extravehicular activity (EVA). At lower left is the LM's Y footpad. The empty Radioisotope Thermoelectric Generator (RTG) fuel cask is at upper right. The fuel capsule has already been removed and placed in the RTG. The RTG furnishes power for the Apollo Lunar Surface Experiments Package (ALSEP) which the Apollo 12 astronauts deployed on the moon. The LM's descent engine skirt is in the center background. The rod-like object protruding out from under the footpad is a lunar surface sensing probe. Astronaut Richard F. Gordon Jr., command module pilot, remained with the Command and Service Modules (CSM) in lunar orbit while astronauts Charles Conrad Jr., commander; and Alan L. Bean, lunar module pilot, descended in the LM to explore the moon.
Simultaneously firing two cylinders of an even firing camless engine
Brennan, Daniel G
2014-03-11
A valve control system includes an engine speed control module that determines an engine speed and a desired engine stop position. A piston position module determines a desired stopping position of a first piston based on the desired engine stop position. A valve control module receives the desired stopping position, commands a set of valves to close at the desired stopping position if the engine speed is less than a predetermined shutdown threshold, and commands the set of valves to reduce the engine speed if the engine speed is greater than the predetermined shutdown threshold.
Develop railway engineering modules in UTK civil engineering undergraduate and graduate courses.
DOT National Transportation Integrated Search
2015-05-31
The importance of railway transport has long been recognized. However, no railway : engineering courses have been provided in the UTK civil engineering curricula. The : objective of this education project is to develop some railway engineering module...
ERIC Educational Resources Information Center
Minnesota State Dept. of Education, St. Paul. Div. of Vocational and Technical Education.
THIS MODULE OF A 30-MODULE COURSE IS DESIGNED TO PROVIDE A SUMMARY OF DIESEL ENGINE MAINTENANCE FACTORS AND A REVIEW OF DIESEL ENGINE ALTERNATOR OPERATION. THE SEVEN SECTIONS COVER DIESEL ENGINE TROUBLESHOOTING AND THE OPERATION, TESTING, AND ADJUSTING OF ALTERNATORS. THE MODULE CONSISTS OF A SELF-INSTRUCTIONAL BRANCH PROGRAMED TRAINING FILM…
1999-02-25
KENNEDY SPACE CENTER, FLA. -- At a ribbon-cutting ceremony inside the Operations and Checkout Building high bay, Sterling Walker, director of Engineering Development, introduces the project team members responsible for renovating an altitude chamber formerly used on the Apollo program. In addition, management, media and onlookers are present for the ceremony. Seated in the front row left are (left to right) Terry Smith, director of Engineering, Boeing Space Coast Operations; Steve Francois, director, Space Station and Shuttle Payloads; Jay Greene, International Space Station manager for Technical; and Roy Bridges, center director. The chamber was reactivated, after a 24-year hiatus, to perform leak tests on International Space Station pressurized modules at the launch site. Originally, two chambers were built to test the Apollo command and lunar service modules. They were last used in 1975 during the Apollo-Soyuz Test Project. After installation of new vacuum pumping equipment and controls, a new control room, and a new rotation handling fixture, the chamber again became operational in February 1999. The chamber, which is 33 feet in diameter and 50 feet tall, is constructed of stainless steel. The first module that will be tested for leaks is the U.S. Laboratory. No date has been determined for the test
Expanding Metabolic Engineering Algorithms Using Feasible Space and Shadow Price Constraint Modules
Tervo, Christopher J.; Reed, Jennifer L.
2014-01-01
While numerous computational methods have been developed that use genome-scale models to propose mutants for the purpose of metabolic engineering, they generally compare mutants based on a single criteria (e.g., production rate at a mutant’s maximum growth rate). As such, these approaches remain limited in their ability to include multiple complex engineering constraints. To address this shortcoming, we have developed feasible space and shadow price constraint (FaceCon and ShadowCon) modules that can be added to existing mixed integer linear adaptive evolution metabolic engineering algorithms, such as OptKnock and OptORF. These modules allow strain designs to be identified amongst a set of multiple metabolic engineering algorithm solutions that are capable of high chemical production while also satisfying additional design criteria. We describe the various module implementations and their potential applications to the field of metabolic engineering. We then incorporated these modules into the OptORF metabolic engineering algorithm. Using an Escherichia coli genome-scale model (iJO1366), we generated different strain designs for the anaerobic production of ethanol from glucose, thus demonstrating the tractability and potential utility of these modules in metabolic engineering algorithms. PMID:25478320
PRiME: integrating professional responsibility into the engineering curriculum.
Moore, Christy; Hart, Hillary; Randall, D'Arcy; Nichols, Steven P
2006-04-01
Engineering educators have long discussed the need to teach professional responsibility and the social context of engineering without adding to overcrowded curricula. One difficulty we face is the lack of appropriate teaching materials that can fit into existing courses. The PRiME (Professional Responsibility Modules for Engineering) Project (http://www.engr.utexas.edu/ethics/primeModules.cfm) described in this paper was initiated at the University of Texas, Austin to provide web-based modules that could be integrated into any undergraduate engineering class. Using HPL (How People Learn) theory, PRiME developed and piloted four modules during the academic year 2004-2005. This article introduces the modules and the pilot, outlines the assessment process, analyzes the results, and describes how the modules are being revised in light of the initial assessment. In its first year of development and testing, PRiME made significant progress towards meeting its objectives. The PRiME Project can strengthen engineering education by providing faculty with an effective system for engaging students in learning about professional responsibility.
2014-06-06
CAPE CANAVERAL, Fla. -- Inside the Operations and Checkout Building high bay at NASA's Kennedy Space Center in Florida, a Lockheed Martin technician monitors the progress as a crane lowers the Orion service module into the Final Assembly and System Testing, or FAST, cell further down the aisle. The Orion crew module will be stacked on the service module in the FAST cell and then both modules will be put through their final system tests for Exploration Flight Test-1, or EFT-1, before rolling out of the facility for integration with the United Launch Alliance Delta IV Heavy rocket. Orion is the exploration spacecraft designed to carry astronauts to destinations not yet explored by humans, including an asteroid and Mars. It will have emergency abort capability, sustain the crew during space travel and provide safe re-entry from deep space return velocities. The first unpiloted test flight of Orion, EFT-1, is scheduled to launch later this year atop a Delta IV rocket from Cape Canaveral Air Force Station in Florida to an altitude of 3,600 miles above the Earth's surface. The two-orbit, four-hour flight test will help engineers evaluate the systems critical to crew safety including the heat shield, parachute system and launch abort system. For more information, visit http://www.nasa.gov/orion. Photo credit: NASA/Glenn Benson
ERIC Educational Resources Information Center
Lucy, William H.; Mladenka, Kenneth R.
This package contains the student materials for five modules which comprise a portion of the National Training and Development Service Urban Management Curriculum Development Project. These modules focus on the distribution of services in urban areas. Module One presents chapters on service distribution and equity, effectiveness, decision making,…
2007-02-22
ISS014-E-14523 (22 Feb. 2007) --- Astronaut Michael E. Lopez-Alegria, Expedition 14 commander and NASA space station science officer, wearing a Russian Orlan spacesuit, participates in a session of extravehicular activity (EVA). Among other tasks, Lopez-Alegria and cosmonaut Mikhail Tyurin (out of frame), flight engineer representing Russia's Federal Space Agency, were able to retract a stuck Kurs antenna on the Progress vehicle docked to the International Space Station's Zvezda Service Module.
2007-02-22
ISS014-E-14531 (22 Feb. 2007) --- Astronaut Michael E. Lopez-Alegria, Expedition 14 commander and NASA space station science officer, wearing a Russian Orlan spacesuit, participates in a session of extravehicular activity (EVA). Among other tasks, Lopez-Alegria and cosmonaut Mikhail Tyurin (out of frame), flight engineer representing Russia's Federal Space Agency, were able to retract a stuck Kurs antenna on the Progress vehicle docked to the International Space Station's Zvezda Service Module.
Walz, Bloomfield, Walheim and Ross pose in Zvezda during STS-110's visit to the ISS
2002-04-09
STS110-E-5127 (10 April 2002) --- Astronauts Carl E. Walz (top left), Expedition Four flight engineer, Michael J. Bloomfield, STS-110 mission commander, and Rex J. Walheim (bottom left) and Jerry L. Ross, both STS-110 mission specialists, gather for an informal photo in the Zvezda Service Module on the International Space Station (ISS). The image was taken with a digital still camera.
2017-01-09
Still sealed in its environmentally controlled shipping container, the Orbital ATK OA-7 Cygnus spacecraft's pressurized cargo module (PCM) has arrived inside the Space Station Processing Facility at NASA's Kennedy Space Center in Florida. Once the Cygnus spacecraft is removed from its shipping container, engineers and technicians will begin preparing for launch scheduled for March 2017. Orbital ATK CRS-7 will lift off atop a United Launch Alliance Atlas V rocket from Space launch Complex 41 at Cape Canaveral Air Force Station. The commercial resupply services mission to the International Space Station will deliver thousands of pounds of supplies, equipment and scientific research materials that improve life on Earth and drive progress toward future space exploration.
Impact of Multimedia and Network Services on an Introductory Level Course
NASA Technical Reports Server (NTRS)
Russ, John C.
1996-01-01
We will demonstrate and describe the impact of our use of multimedia and network connectivity on a sophomore-level introductory course in materials science. This class services all engineering students, resulting in large (more than 150) class sections with no hands-on laboratory. In 1990 we began to develop computer graphics that might substitute for some laboratory or real-world experiences, and demonstrate relationships hard to show with static textbook images or chalkboard drawings. We created a comprehensive series of modules that cover the entire course content. Called VIMS (Visualizations in Materials Science), these are available in the form of a CD-ROM and also via the internet.
System and method for controlling hydraulic pressure in electro-hydraulic valve actuation systems
Brennan, Daniel G; Marriott, Craig D; Cowgill, Joel; Wiles, Matthew A; Patton, Kenneth James
2014-09-23
A control system for an engine includes a first lift control module and a second lift control module. The first lift control module increases lift of M valves of the engine to a predetermined valve lift during a period before disabling or re-enabling N valves of the engine. The second lift control module decreases the lift of the M valves to a desired valve lift during a period after enabling or re-enabling the N valves of the engine, wherein N and M are integers greater than or equal to one.
Scientific Cluster Deployment and Recovery - Using puppet to simplify cluster management
NASA Astrophysics Data System (ADS)
Hendrix, Val; Benjamin, Doug; Yao, Yushu
2012-12-01
Deployment, maintenance and recovery of a scientific cluster, which has complex, specialized services, can be a time consuming task requiring the assistance of Linux system administrators, network engineers as well as domain experts. Universities and small institutions that have a part-time FTE with limited time for and knowledge of the administration of such clusters can be strained by such maintenance tasks. This current work is the result of an effort to maintain a data analysis cluster (DAC) with minimal effort by a local system administrator. The realized benefit is the scientist, who is the local system administrator, is able to focus on the data analysis instead of the intricacies of managing a cluster. Our work provides a cluster deployment and recovery process (CDRP) based on the puppet configuration engine allowing a part-time FTE to easily deploy and recover entire clusters with minimal effort. Puppet is a configuration management system (CMS) used widely in computing centers for the automatic management of resources. Domain experts use Puppet's declarative language to define reusable modules for service configuration and deployment. Our CDRP has three actors: domain experts, a cluster designer and a cluster manager. The domain experts first write the puppet modules for the cluster services. A cluster designer would then define a cluster. This includes the creation of cluster roles, mapping the services to those roles and determining the relationships between the services. Finally, a cluster manager would acquire the resources (machines, networking), enter the cluster input parameters (hostnames, IP addresses) and automatically generate deployment scripts used by puppet to configure it to act as a designated role. In the event of a machine failure, the originally generated deployment scripts along with puppet can be used to easily reconfigure a new machine. The cluster definition produced in our CDRP is an integral part of automating cluster deployment in a cloud environment. Our future cloud efforts will further build on this work.
Unstart coupling mechanism analysis of multiple-modules hypersonic inlet.
Hu, Jichao; Chang, Juntao; Wang, Lei; Cao, Shibin; Bao, Wen
2013-01-01
The combination of multiplemodules in parallel manner is an important way to achieve the much higher thrust of scramjet engine. For the multiple-modules scramjet engine, when inlet unstarted oscillatory flow appears in a single-module engine due to high backpressure, how to interact with each module by massflow spillage, and whether inlet unstart occurs in other modules are important issues. The unstarted flowfield and coupling characteristic for a three-module hypersonic inlet caused by center module II and side module III were, conducted respectively. The results indicate that the other two hypersonic inlets are forced into unstarted flow when unstarted phenomenon appears on a single-module hypersonic inlet due to high backpressure, and the reversed flow in the isolator dominates the formation, expansion, shrinkage, and disappearance of the vortexes, and thus, it is the major factor of unstart coupling of multiple-modules hypersonic inlet. The coupling effect among multiple modules makes hypersonic inlet be more likely unstarted.
AUTOMOTIVE DIESEL MAINTENANCE 1. UNIT XXIX, REVIEWING THE CONSTRUCTION OF ENGINE COMPONENTS.
ERIC Educational Resources Information Center
Human Engineering Inst., Cleveland, OH.
THIS MODULE OF A 30-MODULE COURSE IS DESIGNED TO PROVIDE A REVIEW OF THE CONSTRUCTION AND OPERATION OF DIESEL ENGINE COMPONENTS. TOPICS ARE STATIONARY PARTS, ENGINE MOVING PARTS, PISTON RINGS, AND CONNECTING RODS AND PISTON PINS. THE MODULE CONSISTS OF AN INSTRUCTOR'S GUIDE, TRANSPARENCIES, A LIST OF SUGGESTED SUPPLEMENTARY MATERIALS, AND TRAINEE…
2001-06-21
KENNEDY SPACE CENTER, Fla. -- After a journey of more than 8 hours from the Vehicle Assembly Building, Space Shuttle Atlantis sits on Launch Pad 39B. At left is the Rotating Service Structure, which will roll on its axis to enclose the Shuttle until launch. Towering above the Fixed Service Structure next to it is the 80-foot tall lightning mast that provides protection from lightning strikes. On the right is the elevated water tank with a capacity of 300,000 gallons. Part of the Sound Suppression Water System, the water in the tank is released just before ignition of the orbiter’s three main engines and twin solid rocket boosters and flow through parallel 7-foot-diameter pipes to the pad area. The Shuttle is targeted for launch no earlier than July 12 on mission STS-104, the 10th flight to the International Space Station. The payload on the 11-day mission is the Joint Airlock Module, which will allow astronauts and cosmonauts in residence on the Station to perform future spacewalks without the presence of a Space Shuttle. The module, which comprises a crew lock and an equipment lock, will be connected to the starboard (right) side of Node 1 Unity. Atlantis will also carry oxygen and nitrogen storage tanks, vital to operation of the Joint Airlock, on a Spacelab Logistics Double Pallet in the payload bay. The tanks, to be installed on the perimeter of the Joint Module during the mission’s spacewalks, will support future spacewalk operations and experiments plus augment the resupply system for the Station’s Service Module
Tyurin readies the NASDA exposure experiment cases for their EVA
2001-10-14
ISS003-E-6623 (14 October 2001) --- Cosmonaut Mikhail Tyurin, Expedition Three flight engineer representing Rosaviakosmos, works with hardware for the Micro-Particles Capturer (MPAC) and Space Environment Exposure Device (SEED) experiment and fixture mechanism in the Zvezda Service Module on the International Space Station (ISS). MPAC and SEED were developed by Japans National Space Development Agency (NASDA), and Russia developed the Fixture Mechanism. This image was taken with a digital still camera.
2006-11-29
ISS014-E-08795 (29 Nov. 2006) --- European Space Agency (ESA) astronaut Thomas Reiter, Expedition 14 flight engineer, works with the Cognitive Cardiovascular (Cardiocog-2) experiment in the Zvezda Service Module of the International Space Station. Cardiocog-2 will determine the impact of weightlessness on the cardiovascular system and respiratory system and the cognitive reactions of crewmembers. The results of this study will be used to develop additional countermeasures that will continue to keep crewmembers healthy during long-duration space exploration.
Parametric Model of an Aerospike Rocket Engine
NASA Technical Reports Server (NTRS)
Korte, J. J.
2000-01-01
A suite of computer codes was assembled to simulate the performance of an aerospike engine and to generate the engine input for the Program to Optimize Simulated Trajectories. First an engine simulator module was developed that predicts the aerospike engine performance for a given mixture ratio, power level, thrust vectoring level, and altitude. This module was then used to rapidly generate the aerospike engine performance tables for axial thrust, normal thrust, pitching moment, and specific thrust. Parametric engine geometry was defined for use with the engine simulator module. The parametric model was also integrated into the iSIGHTI multidisciplinary framework so that alternate designs could be determined. The computer codes were used to support in-house conceptual studies of reusable launch vehicle designs.
Parametric Model of an Aerospike Rocket Engine
NASA Technical Reports Server (NTRS)
Korte, J. J.
2000-01-01
A suite of computer codes was assembled to simulate the performance of an aerospike engine and to generate the engine input for the Program to Optimize Simulated Trajectories. First an engine simulator module was developed that predicts the aerospike engine performance for a given mixture ratio, power level, thrust vectoring level, and altitude. This module was then used to rapidly generate the aerospike engine performance tables for axial thrust, normal thrust, pitching moment, and specific thrust. Parametric engine geometry was defined for use with the engine simulator module. The parametric model was also integrated into the iSIGHT multidisciplinary framework so that alternate designs could be determined. The computer codes were used to support in-house conceptual studies of reusable launch vehicle designs.
NASA Astrophysics Data System (ADS)
Klein Altstedde, Mirko; Sottong, Reinhard; Freitag, Oliver; Kober, Martin; Dreißigacker, Volker; Zabrocki, Knud; Szabo, Patric
2015-06-01
Despite the ongoing electrification of vehicle propulsion systems, vehicles with combustion engines will continue to bear the brunt of passenger services worldwide for the next few decades. As a result, the German Aerospace Center Institute of Vehicle Concepts, the Institute of Materials Research and the Institute of Technical Thermodynamics have focused on utilising the exhaust heat of internal combustion engines by means of thermoelectric generators (TEGs). Their primary goal is the development of cost-efficient TEGs with long-term stability and maximised energy yield. In addition to the overall TEG system design, the development of long-term stable, efficient thermoelectric modules (TEMs) for high-temperature applications is a great challenge. This paper presents the results of internal development work and reveals an expedient module design for use in TEGs suitable for vehicles. The TEM requirements identified, which were obtained by means of experiments on the test vehicle and test bench, are described first. Doped semiconductor materials were produced and characterised by production methods capable of being scaled up in order to represent series application. The results in terms of thermoelectric properties (Seebeck coefficient, electrical conductivity and thermal conductivity) were used for the simulative design of a thermoelectric module using a constant-property model and with the aid of FEM calculations. Thermomechanical calculations of material stability were carried out in addition to the TEM's thermodynamic and thermoelectric design. The film sequence within the module represented a special challenge. Multilayer films facilitated adaptation of the thermal and mechanical properties of plasma-sprayed films. A joint which dispenses with solder additives was also possible using multilayer films. The research resulted in a functionally-optimised module design, which was enhanced for use in motor vehicles using process flexibility and close-to-production manufacturing methods.
Fuel premixing module for gas turbine engine combustor
NASA Technical Reports Server (NTRS)
Chin, Jushan (Inventor); Rizk, Nader K. (Inventor); Razdan, Mohan K. (Inventor); Marshall, Andre W. (Inventor)
2005-01-01
A fuel-air premixing module is designed to reduce emissions from a gas turbine engine. In one form, the premixing module includes a central pilot premixer module with a main premixer module positioned thereround. Each of the portions of the fuel-air premixing module include an axial inflow swirler with a plurality of fixed swirler vanes. Fuel is injected into the main premixer module between the swirler vanes of the axial inflow swirler and at an acute angle relative to the centerline of the premixing module.
The Use of Human Modeling of EVA Tasks as a Systems Engineering Tool
NASA Technical Reports Server (NTRS)
Dischinger, H. Charles, Jr.; Schmidt, Henry J.; Kross, Dennis A. (Technical Monitor)
2001-01-01
Computer-generated human models have been used in aerospace design for a decade. They have come to be highly reliable for worksite analysis of certain types of EVA tasks. In many design environments, this analysis comes after the structural design is largely complete. However, the use of these models as a development tool is gaining acceptance within organizations that practice good systems engineering processes. The design of the United States Propulsion Module for the International Space Station provides an example of this application. The Propulsion Module will provide augmentation to the propulsion capability supplied by the Russian Service Module Zvezda. It is a late addition to the set of modules provided by the United States to the ISS Program, and as a result, faces design challenges that result from the level of immaturity of its integration into the Station. Among these are heat dissipation and physical envelopes. Since the rest of the Station was designed to maximize the use of the cooling system, little margin is available for the addition of another module. The Propulsion Module will attach at the forward end of the Station, and will be between the Orbiter and the rest of ISS. Since cargo must be removed from the Payload Bay and transferred to Station by the Canadarm, there is a potential for protrusions from the module, such as thruster booms, to interfere with robotic operations. These and similar engineering issues must be addressed as part of the development. In the implementation of good system design, all design solutions should be analyzed for compatibility with all affected subsystems. Human modeling has been used in this project to provide rapid input to system trades of design concepts. For example, the placement of radiators and avionics components for optimization of heat dissipation had to be examined for feasibility of EVA translation paths and worksite development. Likewise, the location of and mechanism for the retraction of thruster booms was partly driven by available Orbiter, robotic arm, and other module envelopes; worksite analysis was required for early assessment of task success. Since these trade studies included the EVA analysis as part of the decision criteria, the design had a high degree of assurance of EVA supportability from the outset. This approach contributes greatly to mission success.
Stationary Engineers Apprenticeship. Related Training Modules. 20.1-23.1 Miscellaneous.
ERIC Educational Resources Information Center
Lane Community Coll., Eugene, OR.
This learning module, one in a series of 20 related training modules for apprentice stationary engineers, deals with miscellaneous job skills needed by persons working in power plants. Addressed in the individual instructional packages included in the module are the following topics: transformers, circuit protection, construction of foundations…
Biomedical and Biochemical Engineering for K-12 Students
ERIC Educational Resources Information Center
Madihally, Sundararajan V.; Maase, Eric L.
2006-01-01
REACH (Reaching Engineering and Architectural Career Heights) is a weeklong summer academy outreach program for high school students interested in engineering, architecture, or technology. Through module-based instruction, students are introduced to various engineering fields. This report describes one of the modules focused on introducing…
The International Space Station Habitat
NASA Technical Reports Server (NTRS)
Watson, Patricia Mendoza; Engle, Mike
2003-01-01
The International Space Station (ISS) is an engineering project unlike any other. The vehicle is inhabited and operational as construction goes on. The habitability resources available to the crew are the crew sleep quarters, the galley, the waste and hygiene compartment, and exercise equipment. These items are mainly in the Russian Service Module and their placement is awkward for the crew to deal with ISS assembly will continue with the truss build and the addition of International Partner Laboratories. Also, Node 2 and 3 will be added. The Node 2 module will provide additional stowage volume and room for more crew sleep quarters. The Node 3 module will provide additional Environmental Control and Life Support Capability. The purpose of the ISS is to perform research and a major area of emphasis is the effects of long duration space flight on humans, a result of this research they will determine what are the habitability requirements for long duration space flight.
System and method for controlling engine knock using electro-hydraulic valve actuation
Brennan, Daniel G
2013-12-10
A control system for an engine includes a knock control module and a valve control module. The knock control module adjusts a period that one or more of an intake valve and an exhaust valve of a cylinder are open based on engine knock corresponding to the cylinder. The valve control module, based on the adjusted period, controls the one or more of the intake valve and the exhaust valve using one or more hydraulic actuators.
The ribbon-cutting ceremony unveils the reactivated altitude chamber inside the O&C high bay
NASA Technical Reports Server (NTRS)
1999-01-01
At a ribbon-cutting ceremony inside the Operations and Checkout Building high bay, Sterling Walker, director of Engineering Development, introduces the project team members responsible for renovating an altitude chamber formerly used on the Apollo program. In addition, management, media and onlookers are present for the ceremony. Seated in the front row left are (left to right) Terry Smith, director of Engineering, Boeing Space Coast Operations; Steve Francois, director, Space Station and Shuttle Payloads; Jay Greene, International Space Station manager for Technical; and Roy Bridges, center director. The chamber was reactivated, after a 24-year hiatus, to perform leak tests on International Space Station pressurized modules at the launch site. Originally, two chambers were built to test the Apollo command and lunar service modules. They were last used in 1975 during the Apollo-Soyuz Test Project. After installation of new vacuum pumping equipment and controls, a new control room, and a new rotation handling fixture, the chamber again became operational in February 1999. The chamber, which is 33 feet in diameter and 50 feet tall, is constructed of stainless steel. The first module that will be tested for leaks is the U.S. Laboratory. No date has been determined for the test.
Federal Register 2010, 2011, 2012, 2013, 2014
2012-10-30
... (RFHM), Ignition Node Module (IGNM), Engine Control Module, Body Controller Module, Sentry Key... disable engine operation and immobilize the vehicle after two seconds of running. This process is also...
Effective Engineering Outreach through an Undergraduate Mentoring Team and Module Database
ERIC Educational Resources Information Center
Young, Colin; Butterfield, Anthony E.
2014-01-01
The rising need for engineers has led to increased interest in community outreach in engineering departments nationwide. We present a sustainable outreach model involving trained undergraduate mentors to build ties with K-12 teachers and students. An associated online module database of chemical engineering demonstrations, available to educators…
2014-06-06
CAPE CANAVERAL, Fla. -- Inside the Operations and Checkout Building high bay at NASA's Kennedy Space Center in Florida, a Lockheed Martin technician monitors the progress as a crane is used to lift the Orion service module from a test stand and move it to the Final Assembly and System Testing, or FAST, cell further down the aisle. The Orion crew module will be stacked on the service module in the FAST cell and then both modules will be put through their final system tests for Exploration Flight Test-1, or EFT-1, prior to rolling out of the facility for integration with the United Launch Alliance Delta IV Heavy rocket. Orion is the exploration spacecraft designed to carry astronauts to destinations not yet explored by humans, including an asteroid and Mars. It will have emergency abort capability, sustain the crew during space travel and provide safe re-entry from deep space return velocities. The first unpiloted test flight of Orion, EFT-1, is scheduled to launch later this year atop a Delta IV rocket from Cape Canaveral Air Force Station in Florida to an altitude of 3,600 miles above the Earth's surface. The two-orbit, four-hour flight test will help engineers evaluate the systems critical to crew safety including the heat shield, parachute system and launch abort system. For more information, visit http://www.nasa.gov/orion. Photo credit: NASA/Glenn Benson
A TMS320-based modem for the aeronautical-satellite core data service
NASA Astrophysics Data System (ADS)
Moher, Michael L.; Lodge, John H.
The International Civil Aviation Organization (ICAO) Future Air Navigation Systems (FANS) committee, the Airlines Electronics Engineering Committee (AEEC), and Inmarsat have been developing standards for an aeronautical satellite communications service. These standards encompass a satellite communications system architecture to provide comprehensive aeronautical communications services. Incorporated into the architecture is a core service capability, providing only low rate data communications, which all service providers and all aircraft earth terminals are required to support. In this paper an implementation of the physical layer of this standard for the low data rate core service is described. This is a completely digital modem (up to a low intermediate frequency). The implementation uses a single TMS320C25 chip for the transmit baseband functions of scrambling, encoding, interleaving, block formatting and modulation. The receiver baseband unit uses a dual processor configuration to implement the functions of demodulation, synchronization, de-interleaving, decoding and de-scrambling. The hardware requirements, the software structure and the algorithms of this implementation are described.
SeaDataNet network services monitoring: Definition and Implementation of Service availability index
NASA Astrophysics Data System (ADS)
Lykiardopoulos, Angelos; Mpalopoulou, Stavroula; Vavilis, Panagiotis; Pantazi, Maria; Iona, Sissy
2014-05-01
SeaDataNet (SDN) is a standardized system for managing large and diverse data sets collected by the oceanographic fleets and the automatic observation systems. The SeaDataNet network is constituted of national oceanographic data centres of 35 countries, active in data collection. SeaDataNetII project's objective is to upgrade the present SeaDataNet infrastructure into an operationally robust and state-of-the-art infrastructure; therefore Network Monitoring is a step to this direction. The term Network Monitoring describes the use of system that constantly monitors a computer network for slow or failing components and that notifies the network administrator in case of outages. Network monitoring is crucial when implementing widely distributed systems over the Internet and in real-time systems as it detects malfunctions that may occur and notifies the system administrator who can immediately respond and correct the problem. In the framework of SeaDataNet II project a monitoring system was developed in order to monitor the SeaDataNet components. The core system is based on Nagios software. Some plug-ins were developed to support SeaDataNet modules. On the top of Nagios Engine a web portal was developed in order to give access to local administrators of SeaDataNet components, to view detailed logs of their own service(s). Currently the system monitors 35 SeaDataNet Download Managers, 9 SeaDataNet Services, 25 GeoSeas Download Managers and 23 UBSS Download Managers . Taking advantage of the continuous monitoring of SeaDataNet system components a total availability index will be implemented. The term availability can be defined as the ability of a functional unit to be in a state to perform a required function under given conditions at a given instant of time or over a given time interval, assuming that the required external resources are provided. Availability measures can be considered as a are very important benefit becauseT - The availability trends that can be extracted from the stored availability measurements will give an indication of the condition of the service modules. - Will help in planning upgrades planning - and the maintenance of the network service. - It is a prerequisite in case of signing a Service Level Agreement. To construct the service availability index, a method for measuring availability of SeaDataNet network is developed and a database is implemented to store the measured values. Although the measurements of availability of a single component in a network service can be considered as simple (is a percentage of time in a year that the service is available to the users), the ipmlementation of a method to measure the total availability of a composite system can be complicated and there is no a standardized method to deal with it. The method followed to calculate the total availability index in case of SeaDataNet can be described as follows: The whole system was divided in operational modules providing a single service in which the availability can be measured by monitoring portal. Next the dependences between these modules were defined in order to formulate the influence of availability of each module against the whole system. For each module a weight coefficient depending on module's involvement in total system productivity was defined. A mathematical formula was developed to measure the index.
Stationary Engineers Apprenticeship. Related Training Modules. 13.1-13.7 Pumps.
ERIC Educational Resources Information Center
Lane Community Coll., Eugene, OR.
This learning module, one in a series of 20 related training modules for apprentice stationary engineers, deals with pumps. Addressed in the individual instructional packages included in the module are the following topics: types, classifications, and applications of pumps; pump construction; procedures for calculating pump heat and pump flow;…
Stationary Engineers Apprenticeship. Related Training Modules. 3.1-3.4 Drawing.
ERIC Educational Resources Information Center
Lane Community Coll., Eugene, OR.
This packet of four learning modules on drawing is one of 20 such packets developed for apprenticeship training for stationary engineers. Introductory materials are a complete listing of all available modules and a supplementary reference list. Each module contains some or all of these components: goal, performance indicators, study guide (a…
Stationary Engineers Apprenticeship. Related Training Modules. 10.1-10.5 Machine Components.
ERIC Educational Resources Information Center
Lane Community Coll., Eugene, OR.
This packet of five learning modules on machine components is one of 20 such packets developed for apprenticeship training for stationary engineers. Introductory materials are a complete listing of all available modules and a supplementary reference list. Each module contains some or all of these components: goal, performance indicators, statement…
Stationary Engineers Apprenticeship. Related Training Modules. 15.1-15.5 Turbines.
ERIC Educational Resources Information Center
Lane Community Coll., Eugene, OR.
This learning module, one in a series of 20 related training modules for apprentice stationary engineers, deals with turbines. addressed in the individual instructional packages included in the module are the following topics: types and components of steam turbines, steam turbine auxiliaries, operation and maintenance of steam turbines, and gas…
Stationary Engineers Apprenticeship. Related Training Modules. 8.1-8.13 Hydraulics.
ERIC Educational Resources Information Center
Lane Community Coll., Eugene, OR.
This packet of 13 learning modules on hydraulics is one of 20 such packets developed for apprenticeship training for stationary engineers. Introductory materials are a complete listing of all available modules and a supplementary reference list. Each module contains some or all of these components: goal, performance indicators, study guide (a…
Stationary Engineers Apprenticeship. Related Training Modules. 9.1-9.6 Refrigeration.
ERIC Educational Resources Information Center
Lane Community Coll., Eugene, OR.
This packet of six learning modules on refrigeration is one of 20 such packets developed for apprenticeship training for stationary engineers. Introductory materials are a complete listing of all available modules and a supplementary reference list. Each module contains some or all of these components: goal, performance indicators, statement of…
Stationary Engineers Apprenticeship. Related Training Modules. 12.1-12.9. Boilers.
ERIC Educational Resources Information Center
Lane Community Coll., Eugene, OR.
This learning module, one in a series of 20 related training modules for apprentice stationary engineers, deals with boilers. Addressed in the individual instructional packages included in the module are the following topics: firetube and watertube boilers; boiler construction; procedures for operating and cleaning boilers; and boiler fittings,…
Stationary Engineers Apprenticeship. Related Training Modules. 16.1-16.5 Combustion.
ERIC Educational Resources Information Center
Lane Community Coll., Eugene, OR.
This learning module, one in a series of 20 related training modules for apprentice stationary engineers, deals with combustion. Addressed in the individual instructional packages included in the module are the following topics: the combustion process, types of fuel, air and flue gases, heat transfer during combustion, and wood combustion. Each…
Stationary Engineers Apprenticeship. Related Training Modules. 5.1-5.17 Electricity/Electronics.
ERIC Educational Resources Information Center
Lane Community Coll., Eugene, OR.
This packet of 17 learning modules on electricity/electronics is one of 20 such packets developed for apprenticeship training for stationary engineers. Introductory materials are a complete listing of all available modules and a supplementary reference list. Each module contains some or all of these components: goal, performance indicators,…
Stationary Engineers Apprenticeship. Related Training Modules. 4.1-4.5 Tools.
ERIC Educational Resources Information Center
Lane Community Coll., Eugene, OR.
This packet of five learning modules on tools is one of 20 such packets developed for apprenticeship training for stationary engineers. Introductory materials are a complete listing of all available modules and a supplementary reference list. Each module contains some or all of these components: a lesson goal, performance indicators, study guide…
NASA Astrophysics Data System (ADS)
Yang, Yanchao; Jiang, Hong; Liu, Congbin; Lan, Zhongli
2013-03-01
Cognitive radio (CR) is an intelligent wireless communication system which can dynamically adjust the parameters to improve system performance depending on the environmental change and quality of service. The core technology for CR is the design of cognitive engine, which introduces reasoning and learning methods in the field of artificial intelligence, to achieve the perception, adaptation and learning capability. Considering the dynamical wireless environment and demands, this paper proposes a design of cognitive engine based on the rough sets (RS) and radial basis function neural network (RBF_NN). The method uses experienced knowledge and environment information processed by RS module to train the RBF_NN, and then the learning model is used to reconfigure communication parameters to allocate resources rationally and improve system performance. After training learning model, the performance is evaluated according to two benchmark functions. The simulation results demonstrate the effectiveness of the model and the proposed cognitive engine can effectively achieve the goal of learning and reconfiguration in cognitive radio.
NASA Technical Reports Server (NTRS)
Seiler, James; Brasfield, Fred; Cannon, Scott
2008-01-01
Ares is an integral part of NASA s Constellation architecture that will provide crew and cargo access to the International Space Station as well as low earth orbit support for lunar missions. Ares replaces the Space Shuttle in the post 2010 time frame. Ares I is an in-line, two-stage rocket topped by the Orion Crew Exploration Vehicle, its service module, and a launch abort system. The Ares I first stage is a single, five-segment reusable solid rocket booster derived from the Space Shuttle Program's reusable solid rocket motor. The Ares second or upper stage is propelled by a J-2X main engine fueled with liquid oxygen and liquid hydrogen. This paper describes the advanced systems engineering and planning tools being utilized for the design, test, and qualification of the Ares I first stage element. Included are descriptions of the current first stage design, the milestone schedule requirements, and the marriage of systems engineering, detailed planning efforts, and roadmapping employed to achieve these goals.
Federal Register 2010, 2011, 2012, 2013, 2014
2011-11-03
...), Ignition Node Module (IGNM), Engine Control Module (ECM), Body Controller Module (BCM), Sentry Key..., Chrysler stated that the RFHM sends an invalid key message to the ECM, which will disable engine operation...
Unstart Coupling Mechanism Analysis of Multiple-Modules Hypersonic Inlet
Wang, Lei; Cao, Shibin
2013-01-01
The combination of multiplemodules in parallel manner is an important way to achieve the much higher thrust of scramjet engine. For the multiple-modules scramjet engine, when inlet unstarted oscillatory flow appears in a single-module engine due to high backpressure, how to interact with each module by massflow spillage, and whether inlet unstart occurs in other modules are important issues. The unstarted flowfield and coupling characteristic for a three-module hypersonic inlet caused by center module II and side module III were, conducted respectively. The results indicate that the other two hypersonic inlets are forced into unstarted flow when unstarted phenomenon appears on a single-module hypersonic inlet due to high backpressure, and the reversed flow in the isolator dominates the formation, expansion, shrinkage, and disappearance of the vortexes, and thus, it is the major factor of unstart coupling of multiple-modules hypersonic inlet. The coupling effect among multiple modules makes hypersonic inlet be more likely unstarted. PMID:24348146
BMTC: --A Tool for Standardized Tissue Engineering on Ground and in Space ---
NASA Astrophysics Data System (ADS)
Kern, Peter; Kemmerle, Kurt; Jones, David
ESA is developing the BMTC (Biotechnology Mammalian Tissue Culture Facility) as ground demonstrator in order to: • establish a well characterised terrestrial platform for tissue engineer-ing under defined, reproducible conditions • prepare for future tissue engineering experiments in space using proven, well characterised, modular equipment. In the beginning the facility will be dedicated to support research of bone and cartilage growth under controlled mechanical and/or biochemical stimulation. Meanwhile, the industrial BMTC team has finalised the first model. The BMTC is highly automated system which provides standardized experiment hardware for tissue cultivation and stimulation under controlled conditions and the reproducible execution of the experiment according pre-programmed protocols. The BMTC consists of an incubator for the control of the experiment environment. Internally it offers all experiment relevant subsystems: • two Cultivation Units, each with eight Experiment Chamber Modules optical in-situ sensors for pO2 and pH • the Liquid Handling Device for medium exchange and sample taking • the handling devices for the internal transport of the experiment chamber modules to different experiment services • workstations for uni-axial loading of tissue samples; ZETOS (for bone tissue) / CHONDROS (for cartilage tissue) provision of reproducible displacement profiles measurement of the resulting forces computation of the visco-eleastic properties of the samples provision of flow induced shear stress fluorescence microscope • two different reactor types are included in the baseline flat reactor for 2D-and flat 3D-cultures with flow induced shear stress stimulation compatible with microscope cylindrical 3D-reactor for cultivation of vital bone and cartilage samples compatible with un-directional stimulation / analysis by ZETOS / CHONDROS. The modular, flexible design of the system allows the servicing and accommodation of a wide range of other experiment specific reactors. The functional principles and the essential features for controlled experiments will be reported. This facility complements the research done on ground on osteoporosis and the bone and muscle loss during bed rest studies during space flights. It is considered to become a new in-orbit research tool for tissue engineering and the verification of mechanical or pharmaceutical countermeasures.
Kaleri sets up Russian MBI-12 Payload in the SM
2010-12-09
ISS026-E-008718 (8 Dec. 2010) --- Russian cosmonaut Alexander Kaleri, Expedition 26 flight engineer, sets up the Russian MBI-12 payload for a Sonokard experiment session in the Zvezda Service Module of the International Space Station. Kaleri used a sports shirt from the Sonokard kit with a special device in the pocket for testing a new method for acquiring physiological data without using direct contact on the skin. Measurements are recorded on a data card for return to Earth.
Kondratvez sets up Sonokard Experiment in the SM during Expedition 26
2011-01-03
ISS026-E-014250 (3 Jan. 2011) --- Russian cosmonaut Dmitry Kondratyev, Expedition 26 flight engineer, sets up the Russian MBI-12 payload for a Sonokard experiment session in the Zvezda Service Module of the International Space Station. Kondratyev used a sports shirt from the Sonokard kit with a special device in the pocket for testing a new method for acquiring physiological data without using direct contact on the skin. Measurements are recorded on a data card for return to Earth.
2000-01-31
The optical bench for the Fluids Integrated Rack section of the Fluids and Combustion Facility (FCF) is shown extracted for servicing. The FCF will be installed, in phases, in the Destiny, the U.S. Laboratory Module of the International Space Station (ISS), and will accommodate multiple users for a range of investigations. This is an engineering mockup; the flight hardware is subject to change as designs are refined. The FCF is being developed by the Microgravity Science Division (MSD) at the NASA Glenn Research Center. (Photo credit: NASA/Marshall Space Flight Center)
2000-01-31
The combustion chamber for the Combustion Integrated Rack section of the Fluids and Combustion Facility (FCF) is shown extracted for servicing. The FCF will be installed, in phases, in the Destiny, the U.S. Laboratory Module of the International Space Station (ISS), and will accommodate multiple users for a range of investigations. This is an engineering mockup; the flight hardware is subject to change as designs are refined. The FCF is being developed by the Microgravity Science Division (MSD) at the NASA Glenn Research Center. (Photo credit: NASA/Marshall Space Flight Center)
Liu, Shenglin; Zhang, Xutian; Wang, Guohong; Zhang, Qiang
2012-03-01
Based on specified demands on medical devices maintenance for clinical engineers and Browser/Server architecture technology, a medical device maintenance information platform was developed, which implemented the following modules such as repair, preventive maintenance, accessories management, training, document, system management and regional cooperation. The characteristics of this system were summarized and application in increase of repair efficiency, improvement of preventive maintenance and cost control was introduced. The application of this platform increases medical device maintenance service level.
Tyurin works with the TORU teleoperated control system in the SM during Expedition 14
2007-01-20
ISS014-E-12482 (19 Jan. 2007) --- Cosmonaut Mikhail Tyurin, Expedition 14 flight engineer representing Russia's Federal Space Agency, practices docking procedures with the TORU teleoperated control system in the Zvezda Service Module of the International Space Station in preparation for the docking of the Progress 24 spacecraft. Tyurin, using the Simvol-TS screen and hand controllers, could manually dock the Progress to the station in the event of a failure of the Kurs automated docking system.
Expedition Three, Expedition Four and STS-108 crews eat a meal in Zvezda
2001-12-15
ISS003-E-8385 (15 December 2001) --- Astronaut Carl E. Walz (left), Expedition Four flight engineer; cosmonaut Yuri I. Onufrienko, Expedition Four mission commander; along with astronauts Dominic L. Gorie, STS-108 mission commander, and Frank L. Culbertson, Jr., Expedition Three mission commander, pose for a group photo in the Zvezda Service Module on the International Space Station (ISS). Various food items are visible in the foreground. The image was taken with a digital still camera.
ERIC Educational Resources Information Center
Barrett, Bradford S.; Moran, Angela L.; Woods, John E.
2014-01-01
Background: Given the continued need to educate the public on both the meteorological and engineering hazards posed by the severe winds of a tornado, an interdisciplinary science, technology, engineering, and mathematics (STEM) module designed by the faculty from the Oceanography and Mechanical Engineering Departments at the United States Naval…
ERIC Educational Resources Information Center
Human Engineering Inst., Cleveland, OH.
THIS MODULE OF A 30-MODULE COURSE IS DESIGNED TO DEVELOP AN UNDERSTANDING OF DIFFERENCES BETWEEN TWO AND FOUR CYCLE ENGINES, THE OPERATION AND MAINTENANCE OF THE DIESEL ENGINE FUEL SYSTEM, AND THE PROCEDURES FOR DIESEL ENGINE REMOVAL. TOPICS ARE (1) REVIEW OF TWO CYCLE AND FOUR CYCLE CONCEPT, (2) SOME BASIC CHARACTERISTICS OF FOUR CYCLE ENGINES,…
ERIC Educational Resources Information Center
Minnesota State Dept. of Education, St. Paul. Div. of Vocational and Technical Education.
THIS MODULE OF A 30-MODULE COURSE IS DESIGNED TO DEVELOP AN UNDERSTANDING OF DIESEL ENGINE TUNE-UP PROCEDURES AND THE DESIGN OF FRONT END SUSPENSION AND AXLES USED ON DIESEL ENGINE EQUIPMENT. TOPICS ARE (1) PRE-TUNE-UP CHECKS, (2) TIMING THE ENGINE, (3) INJECTOR PLUNGER AND VALVE ADJUSTMENTS, (4) FUEL PUMP ADJUSTMENTS ON THE ENGINE (PTR AND PTG),…
ERIC Educational Resources Information Center
Rains, Larry
This engine performance (emission control systems) module is one of a series of competency-based modules in the Missouri Auto Mechanics Curriculum Guide. Topics of this module's five units are: positive crankcase ventilation (PCV) and evaporative emission control systems; exhaust gas recirculation (EGR); air injection and catalytic converters;…
7 CFR 1724.30 - Borrowers' requirements-engineering services.
Code of Federal Regulations, 2010 CFR
2010-01-01
... 7 Agriculture 11 2010-01-01 2010-01-01 false Borrowers' requirements-engineering services. 1724.30... SERVICE, DEPARTMENT OF AGRICULTURE ELECTRIC ENGINEERING, ARCHITECTURAL SERVICES AND DESIGN POLICIES AND PROCEDURES Engineering Services § 1724.30 Borrowers' requirements—engineering services. The provisions of...
7 CFR 1724.30 - Borrowers' requirements-engineering services.
Code of Federal Regulations, 2011 CFR
2011-01-01
... 7 Agriculture 11 2011-01-01 2011-01-01 false Borrowers' requirements-engineering services. 1724.30... SERVICE, DEPARTMENT OF AGRICULTURE ELECTRIC ENGINEERING, ARCHITECTURAL SERVICES AND DESIGN POLICIES AND PROCEDURES Engineering Services § 1724.30 Borrowers' requirements—engineering services. The provisions of...
7 CFR 1724.30 - Borrowers' requirements-engineering services.
Code of Federal Regulations, 2012 CFR
2012-01-01
... 7 Agriculture 11 2012-01-01 2012-01-01 false Borrowers' requirements-engineering services. 1724.30... SERVICE, DEPARTMENT OF AGRICULTURE ELECTRIC ENGINEERING, ARCHITECTURAL SERVICES AND DESIGN POLICIES AND PROCEDURES Engineering Services § 1724.30 Borrowers' requirements—engineering services. The provisions of...
7 CFR 1724.30 - Borrowers' requirements-engineering services.
Code of Federal Regulations, 2013 CFR
2013-01-01
... 7 Agriculture 11 2013-01-01 2013-01-01 false Borrowers' requirements-engineering services. 1724.30... SERVICE, DEPARTMENT OF AGRICULTURE ELECTRIC ENGINEERING, ARCHITECTURAL SERVICES AND DESIGN POLICIES AND PROCEDURES Engineering Services § 1724.30 Borrowers' requirements—engineering services. The provisions of...
NASA Technical Reports Server (NTRS)
Ankenman, Bruce; Ermer, Donald; Clum, James A.
1994-01-01
Modules dealing with statistical experimental design (SED), process modeling and improvement, and response surface methods have been developed and tested in two laboratory courses. One course was a manufacturing processes course in Mechanical Engineering and the other course was a materials processing course in Materials Science and Engineering. Each module is used as an 'experiment' in the course with the intent that subsequent course experiments will use SED methods for analysis and interpretation of data. Evaluation of the modules' effectiveness has been done by both survey questionnaires and inclusion of the module methodology in course examination questions. Results of the evaluation have been very positive. Those evaluation results and details of the modules' content and implementation are presented. The modules represent an important component for updating laboratory instruction and to provide training in quality for improved engineering practice.
7 CFR 1724.30 - Borrowers' requirements-engineering services.
Code of Federal Regulations, 2014 CFR
2014-01-01
... 7 Agriculture 11 2014-01-01 2014-01-01 false Borrowers' requirements-engineering services. 1724.30... SERVICE, DEPARTMENT OF AGRICULTURE ELECTRIC ENGINEERING, ARCHITECTURAL SERVICES AND DESIGN POLICIES AND PROCEDURES Engineering Services § 1724.30 Borrowers' requirements—engineering services. Link to an amendment...
Model documentation report: Commercial Sector Demand Module of the National Energy Modeling System
DOE Office of Scientific and Technical Information (OSTI.GOV)
NONE
1998-01-01
This report documents the objectives, analytical approach and development of the National Energy Modeling System (NEMS) Commercial Sector Demand Module. The report catalogues and describes the model assumptions, computational methodology, parameter estimation techniques, model source code, and forecast results generated through the synthesis and scenario development based on these components. The NEMS Commercial Sector Demand Module is a simulation tool based upon economic and engineering relationships that models commercial sector energy demands at the nine Census Division level of detail for eleven distinct categories of commercial buildings. Commercial equipment selections are performed for the major fuels of electricity, natural gas,more » and distillate fuel, for the major services of space heating, space cooling, water heating, ventilation, cooking, refrigeration, and lighting. The algorithm also models demand for the minor fuels of residual oil, liquefied petroleum gas, steam coal, motor gasoline, and kerosene, the renewable fuel sources of wood and municipal solid waste, and the minor services of office equipment. Section 2 of this report discusses the purpose of the model, detailing its objectives, primary input and output quantities, and the relationship of the Commercial Module to the other modules of the NEMS system. Section 3 of the report describes the rationale behind the model design, providing insights into further assumptions utilized in the model development process to this point. Section 3 also reviews alternative commercial sector modeling methodologies drawn from existing literature, providing a comparison to the chosen approach. Section 4 details the model structure, using graphics and text to illustrate model flows and key computations.« less
Large liquid rocket engine transient performance simulation system
NASA Technical Reports Server (NTRS)
Mason, J. R.; Southwick, R. D.
1989-01-01
Phase 1 of the Rocket Engine Transient Simulation (ROCETS) program consists of seven technical tasks: architecture; system requirements; component and submodel requirements; submodel implementation; component implementation; submodel testing and verification; and subsystem testing and verification. These tasks were completed. Phase 2 of ROCETS consists of two technical tasks: Technology Test Bed Engine (TTBE) model data generation; and system testing verification. During this period specific coding of the system processors was begun and the engineering representations of Phase 1 were expanded to produce a simple model of the TTBE. As the code was completed, some minor modifications to the system architecture centering on the global variable common, GLOBVAR, were necessary to increase processor efficiency. The engineering modules completed during Phase 2 are listed: INJTOO - main injector; MCHBOO - main chamber; NOZLOO - nozzle thrust calculations; PBRNOO - preburner; PIPE02 - compressible flow without inertia; PUMPOO - polytropic pump; ROTROO - rotor torque balance/speed derivative; and TURBOO - turbine. Detailed documentation of these modules is in the Appendix. In addition to the engineering modules, several submodules were also completed. These submodules include combustion properties, component performance characteristics (maps), and specific utilities. Specific coding was begun on the system configuration processor. All functions necessary for multiple module operation were completed but the SOLVER implementation is still under development. This system, the Verification Checkout Facility (VCF) allows interactive comparison of module results to store data as well as provides an intermediate checkout of the processor code. After validation using the VCF, the engineering modules and submodules were used to build a simple TTBE.
Efficient Parallel Engineering Computing on Linux Workstations
NASA Technical Reports Server (NTRS)
Lou, John Z.
2010-01-01
A C software module has been developed that creates lightweight processes (LWPs) dynamically to achieve parallel computing performance in a variety of engineering simulation and analysis applications to support NASA and DoD project tasks. The required interface between the module and the application it supports is simple, minimal and almost completely transparent to the user applications, and it can achieve nearly ideal computing speed-up on multi-CPU engineering workstations of all operating system platforms. The module can be integrated into an existing application (C, C++, Fortran and others) either as part of a compiled module or as a dynamically linked library (DLL).
Apollo 9 Command/Service Modules photographed from Lunar Module
NASA Technical Reports Server (NTRS)
1969-01-01
The Apollo 9 Command/Service Modules photographed from the Lunar Module, 'Spider', on the fifth day of the Apollo 9 earth-orbital mission. Docking mechanism is visible in nose of the Command Module, 'Gumdrop'. Object jutting out from the Service Module aft bulkhead is the high-gain S-Band antenna.
ERIC Educational Resources Information Center
Human Engineering Inst., Cleveland, OH.
THIS MODULE OF A 30-MODULE COURSE IS DESIGNED TO DEVELOP AN UNDERSTANDING OF THE OPERATION AND MAINTENANCE OF DIESEL ENGINE STARTING ENGINES. TOPICS ARE (1) STARTING ENGINE MAGNETO (WICO), (2) MAGNETO MAINTENANCE, (3) SPARK PLUGS, (4) GENERAL DESCRIPTION (STARTING DEVICES), (5) OPERATING (STARTING DEVICES), (6) LUBRICATION (STARTING DEVICES), (7)…
AUTOMOTIVE DIESEL MAINTENANCE 1. UNIT IX, ENGINE COMPONENTS.
ERIC Educational Resources Information Center
Human Engineering Inst., Cleveland, OH.
THIS MODULE OF A 30-MODULE COURSE IS DESIGNED TO DEVELOP AN UNDERSTANDING OF THE CONSTRUCTION, FUNCTION, AND MAINTENANCE OF DIESEL ENGINE CRANKSHAFTS, CAMSHAFTS, AND ASSOCIATED BEARINGS. TOPICS ARE SHAFTS AND BEARINGS, CAMSHAFTS, BEARINGS AND THEIR MAINTENANCE, AND DETECTING FAILURE. THE MODULE CONSISTS OF A SELF-INSTRUCTIONAL BRANCH PROGRAMED…
Modular Aero-Propulsion System Simulation
NASA Technical Reports Server (NTRS)
Parker, Khary I.; Guo, Ten-Huei
2006-01-01
The Modular Aero-Propulsion System Simulation (MAPSS) is a graphical simulation environment designed for the development of advanced control algorithms and rapid testing of these algorithms on a generic computational model of a turbofan engine and its control system. MAPSS is a nonlinear, non-real-time simulation comprising a Component Level Model (CLM) module and a Controller-and-Actuator Dynamics (CAD) module. The CLM module simulates the dynamics of engine components at a sampling rate of 2,500 Hz. The controller submodule of the CAD module simulates a digital controller, which has a typical update rate of 50 Hz. The sampling rate for the actuators in the CAD module is the same as that of the CLM. MAPSS provides a graphical user interface that affords easy access to engine-operation, engine-health, and control parameters; is used to enter such input model parameters as power lever angle (PLA), Mach number, and altitude; and can be used to change controller and engine parameters. Output variables are selectable by the user. Output data as well as any changes to constants and other parameters can be saved and reloaded into the GUI later.
Engineering Design Modules as Physics Teaching Tools
ERIC Educational Resources Information Center
Oliver, Douglas L.; Kane, Jackie
2011-01-01
Pre-engineering is increasingly being taught as a high school subject. This development presents challenges as well as opportunities for the physics education community. If pre-engineering is taught as a separate class, it may divert resources and students from traditional physics classes. However, design modules can be used as physics teaching…
7 CFR 1724.31 - Engineering services contracts.
Code of Federal Regulations, 2010 CFR
2010-01-01
... 7 Agriculture 11 2010-01-01 2010-01-01 false Engineering services contracts. 1724.31 Section 1724..., DEPARTMENT OF AGRICULTURE ELECTRIC ENGINEERING, ARCHITECTURAL SERVICES AND DESIGN POLICIES AND PROCEDURES Engineering Services § 1724.31 Engineering services contracts. The provisions of this section apply only to...
7 CFR 1753.17 - Engineering services.
Code of Federal Regulations, 2014 CFR
2014-01-01
... 7 Agriculture 11 2014-01-01 2014-01-01 false Engineering services. 1753.17 Section 1753.17... AGRICULTURE TELECOMMUNICATIONS SYSTEM CONSTRUCTION POLICIES AND PROCEDURES Engineering Services § 1753.17 Engineering services. (a)(1) All engineering services required by a borrower to support its application for a...
7 CFR 1724.31 - Engineering services contracts.
Code of Federal Regulations, 2014 CFR
2014-01-01
... 7 Agriculture 11 2014-01-01 2014-01-01 false Engineering services contracts. 1724.31 Section 1724..., DEPARTMENT OF AGRICULTURE ELECTRIC ENGINEERING, ARCHITECTURAL SERVICES AND DESIGN POLICIES AND PROCEDURES Engineering Services § 1724.31 Engineering services contracts. The provisions of this section apply only to...
7 CFR 1724.31 - Engineering services contracts.
Code of Federal Regulations, 2011 CFR
2011-01-01
... 7 Agriculture 11 2011-01-01 2011-01-01 false Engineering services contracts. 1724.31 Section 1724..., DEPARTMENT OF AGRICULTURE ELECTRIC ENGINEERING, ARCHITECTURAL SERVICES AND DESIGN POLICIES AND PROCEDURES Engineering Services § 1724.31 Engineering services contracts. The provisions of this section apply only to...
7 CFR 1753.17 - Engineering services.
Code of Federal Regulations, 2010 CFR
2010-01-01
... 7 Agriculture 11 2010-01-01 2010-01-01 false Engineering services. 1753.17 Section 1753.17... AGRICULTURE TELECOMMUNICATIONS SYSTEM CONSTRUCTION POLICIES AND PROCEDURES Engineering Services § 1753.17 Engineering services. (a)(1) All engineering services required by a borrower to support its application for a...
7 CFR 1753.17 - Engineering services.
Code of Federal Regulations, 2011 CFR
2011-01-01
... 7 Agriculture 11 2011-01-01 2011-01-01 false Engineering services. 1753.17 Section 1753.17... AGRICULTURE TELECOMMUNICATIONS SYSTEM CONSTRUCTION POLICIES AND PROCEDURES Engineering Services § 1753.17 Engineering services. (a)(1) All engineering services required by a borrower to support its application for a...
7 CFR 1724.31 - Engineering services contracts.
Code of Federal Regulations, 2013 CFR
2013-01-01
... 7 Agriculture 11 2013-01-01 2013-01-01 false Engineering services contracts. 1724.31 Section 1724..., DEPARTMENT OF AGRICULTURE ELECTRIC ENGINEERING, ARCHITECTURAL SERVICES AND DESIGN POLICIES AND PROCEDURES Engineering Services § 1724.31 Engineering services contracts. The provisions of this section apply only to...
7 CFR 1753.17 - Engineering services.
Code of Federal Regulations, 2013 CFR
2013-01-01
... 7 Agriculture 11 2013-01-01 2013-01-01 false Engineering services. 1753.17 Section 1753.17... AGRICULTURE TELECOMMUNICATIONS SYSTEM CONSTRUCTION POLICIES AND PROCEDURES Engineering Services § 1753.17 Engineering services. (a)(1) All engineering services required by a borrower to support its application for a...
7 CFR 1753.17 - Engineering services.
Code of Federal Regulations, 2012 CFR
2012-01-01
... 7 Agriculture 11 2012-01-01 2012-01-01 false Engineering services. 1753.17 Section 1753.17... AGRICULTURE TELECOMMUNICATIONS SYSTEM CONSTRUCTION POLICIES AND PROCEDURES Engineering Services § 1753.17 Engineering services. (a)(1) All engineering services required by a borrower to support its application for a...
7 CFR 1724.31 - Engineering services contracts.
Code of Federal Regulations, 2012 CFR
2012-01-01
... 7 Agriculture 11 2012-01-01 2012-01-01 false Engineering services contracts. 1724.31 Section 1724..., DEPARTMENT OF AGRICULTURE ELECTRIC ENGINEERING, ARCHITECTURAL SERVICES AND DESIGN POLICIES AND PROCEDURES Engineering Services § 1724.31 Engineering services contracts. The provisions of this section apply only to...
NASA Astrophysics Data System (ADS)
Baldwin, K. A.; Hauge, R.; Dechaine, J. M.; Varrella, G.; Egger, A. E.
2013-12-01
The development and adoption of the Next Generation Science Standards (NGSS) raises a challenge in teacher preparation: few current teacher preparation programs prepare students to teach science the way it is presented in the NGSS, which emphasize systems thinking, interdisciplinary science, and deep engagement in the scientific process. In addition, the NGSS include more geoscience concepts and methods than previous standards, yet this is a topic area in which most college students are traditionally underprepared. Although nationwide, programmatic reform is needed, there are a few targets where relatively small, course-level changes can have a large effect. One of these targets is the 'science methods' course for pre-service elementary teachers, a requirement in virtually all teacher preparation programs. Since many elementary schools, both locally and across the country, have adopted a kit based science curriculum, examining kits is often a part of a science methods course. Unfortunately, solely relying on a kit based curriculum may leave gaps in science content curriculum as one prepares teachers to meet the NGSS. Moreover, kits developed at the national level often fall short in connecting geoscientific content to the locally relevant societal issues that engage students. This highlights the need to train pre-service elementary teachers to supplement kit curriculum with inquiry based geoscience investigations that consider relevant societal issues, promote systems thinking and incorporate connections between earth, life, and physical systems. We are developing a module that teaches geoscience concepts in the context of locally relevant societal issues while modeling effective pedagogy for pre-service elementary teachers. Specifically, we focus on soils, an interdisciplinary topic relevant to multiple geoscience-related societal grand challenges (e.g., water, food) that is difficult to engage students in. Module development is funded through InTeGrate, NSF's STEP Center in the geosciences. The module goals are: 1) Pre-service teachers will apply classification methods, testing procedures and interdisciplinary systems thinking to analyze and evaluate a relevant societal issue in the context of soils, 2) Pre-service teachers will design, develop, and facilitate a standards-based K-8 soils unit, incorporating a relevant broader societal issue that applies authentic geoscientific data, and incorporates geoscientific habits of mind. In addition, pre-service teachers will look toward the NGSS and align activities with content standards, systems thinking, and science and engineering practices. This poster will provide an overview of module development to date as well as a summary of pre-semester survey results indicating pre-service elementary teachers' ideas (beliefs, attitudes, preconceptions, and content knowledge) about teaching soils, and making science relevant in a K-8 classroom.
1981-12-08
o 14 A& B:2.1 Function Driver Module.. ..... .... 14’ ’: B:2.2 Shared Services Module . . . o o . 0 -15 M’ 5:3 Software Decision Module...2.1.13 Weapon Release Functions... ........24 C:2.l.14 Ground Test Functions .. ........... 24 C:2.2 Shared Services Module Decomposition. ........24 C...Driver (FD) Module supported by a Shared Services (SS) Module. B:2.1 FUNCTION DRIVER MODULE The Function Driver Module consists of a set of individual
ERIC Educational Resources Information Center
Minnesota State Dept. of Education, St. Paul. Div. of Vocational and Technical Education.
THIS MODULE OF A 30-MODULE COURSE IS DESIGNED TO DEVELOP AN UNDERSTANDING OF THE CONSTRUCTION AND OPERATION OF DIESEL ENGINE STARTING ENGINES AND BRAKE SYSTEMS USED ON DIESEL POWERED VEHICLES. TOPICS ARE (1) GENERAL DESCRIPTION, (2) OPERATION, (3) COMBUSTION SPACE AND VALVE ARRANGEMENT (STARTING ENGINES), (4) TYPES OF BRAKES, AND (5) DOUBLE…
ERIC Educational Resources Information Center
Minnesota State Dept. of Education, St. Paul. Div. of Vocational and Technical Education.
THIS MODULE OF A 30-MODULE COURSE IS DESIGNED TO DEVELOP AN UNDERSTANDING OF DIESEL ENGINE GEARS AND GEARING PRINCIPLES AND THE OPERATING PRINCIPLES AND MAINTENANCE OF POWER DIVIDERS (GEAR BOXES) USED IN DIESEL ENGINE POWER TRANSMISSION. TOPICS ARE (1) THE PURPOSE OF THE ENGINE GEARS, (2) INSPECTING FOR GEAR FAILURES, (3) INSPECTING FOR SHAFT…
Currently available medical engineering degrees in the UK. Part 1: Undergraduate degrees.
Joyce, T
2009-05-01
This paper reviews mechanical-engineering-based medical engineering degrees which are currently provided at undergraduate level in the UK. At present there are 14 undergraduate degree programmes in medical engineering, offered by the University of Bath, University of Birmingham, University of Bradford, Cardiff University, University of Hull, Imperial College London, University of Leeds, University of Nottingham, University of Oxford, Queen Mary University of London, University of Sheffield, University of Southampton, University of Surrey, and Swansea University. All these undergraduate courses are delivered on a full-time basis, both 3 year BEng and 4 year MEng degrees. Half of the 14 degree courses share a core first 2 years with a mechanical engineering stream. The other seven programmes include medical engineering modules earlier in their degrees. Within the courses, a very wide range of medical-engineering-related modules are offered, although more common modules include biomaterials, biomechanics, and anatomy and physiology.
Taniguchi, Hironori; Okano, Kenji; Honda, Kohsuke
2017-06-01
Bio-based chemical production has drawn attention regarding the realization of a sustainable society. In vitro metabolic engineering is one of the methods used for the bio-based production of value-added chemicals. This method involves the reconstitution of natural or artificial metabolic pathways by assembling purified/semi-purified enzymes in vitro . Enzymes from distinct sources can be combined to construct desired reaction cascades with fewer biological constraints in one vessel, enabling easier pathway design with high modularity. Multiple modules have been designed, built, tested, and improved by different groups for different purpose. In this review, we focus on these in vitro metabolic engineering modules, especially focusing on the carbon metabolism, and present an overview of input modules, output modules, and other modules related to cofactor management.
NASA Astrophysics Data System (ADS)
The present conference on global telecommunications discusses topics in the fields of Integrated Services Digital Network (ISDN) technology field trial planning and results to date, motion video coding, ISDN networking, future network communications security, flexible and intelligent voice/data networks, Asian and Pacific lightwave and radio systems, subscriber radio systems, the performance of distributed systems, signal processing theory, satellite communications modulation and coding, and terminals for the handicapped. Also discussed are knowledge-based technologies for communications systems, future satellite transmissions, high quality image services, novel digital signal processors, broadband network access interface, traffic engineering for ISDN design and planning, telecommunications software, coherent optical communications, multimedia terminal systems, advanced speed coding, portable and mobile radio communications, multi-Gbit/second lightwave transmission systems, enhanced capability digital terminals, communications network reliability, advanced antimultipath fading techniques, undersea lightwave transmission, image coding, modulation and synchronization, adaptive signal processing, integrated optical devices, VLSI technologies for ISDN, field performance of packet switching, CSMA protocols, optical transport system architectures for broadband ISDN, mobile satellite communications, indoor wireless communication, echo cancellation in communications, and distributed network algorithms.
Virtual and flexible digital signal processing system based on software PnP and component works
NASA Astrophysics Data System (ADS)
He, Tao; Wu, Qinghua; Zhong, Fei; Li, Wei
2005-05-01
An idea about software PnP (Plug & Play) is put forward according to the hardware PnP. And base on this idea, a virtual flexible digital signal processing system (FVDSPS) is carried out. FVDSPS is composed of a main control center, many sub-function modules and other hardware I/O modules. Main control center sends out commands to sub-function modules, and manages running orders, parameters and results of sub-functions. The software kernel of FVDSPS is DSP (Digital Signal Processing) module, which communicates with the main control center through some protocols, accept commands or send requirements. The data sharing and exchanging between the main control center and the DSP modules are carried out and managed by the files system of the Windows Operation System through the effective communication. FVDSPS real orients objects, orients engineers and orients engineering problems. With FVDSPS, users can freely plug and play, and fast reconfigure a signal process system according to engineering problems without programming. What you see is what you get. Thus, an engineer can orient engineering problems directly, pay more attention to engineering problems, and promote the flexibility, reliability and veracity of testing system. Because FVDSPS orients TCP/IP protocol, through Internet, testing engineers, technology experts can be connected freely without space. Engineering problems can be resolved fast and effectively. FVDSPS can be used in many fields such as instruments and meter, fault diagnosis, device maintenance and quality control.
A WPS Based Architecture for Climate Data Analytic Services (CDAS) at NASA
NASA Astrophysics Data System (ADS)
Maxwell, T. P.; McInerney, M.; Duffy, D.; Carriere, L.; Potter, G. L.; Doutriaux, C.
2015-12-01
Faced with unprecedented growth in the Big Data domain of climate science, NASA has developed the Climate Data Analytic Services (CDAS) framework. This framework enables scientists to execute trusted and tested analysis operations in a high performance environment close to the massive data stores at NASA. The data is accessed in standard (NetCDF, HDF, etc.) formats in a POSIX file system and processed using trusted climate data analysis tools (ESMF, CDAT, NCO, etc.). The framework is structured as a set of interacting modules allowing maximal flexibility in deployment choices. The current set of module managers include: Staging Manager: Runs the computation locally on the WPS server or remotely using tools such as celery or SLURM. Compute Engine Manager: Runs the computation serially or distributed over nodes using a parallelization framework such as celery or spark. Decomposition Manger: Manages strategies for distributing the data over nodes. Data Manager: Handles the import of domain data from long term storage and manages the in-memory and disk-based caching architectures. Kernel manager: A kernel is an encapsulated computational unit which executes a processor's compute task. Each kernel is implemented in python exploiting existing analysis packages (e.g. CDAT) and is compatible with all CDAS compute engines and decompositions. CDAS services are accessed via a WPS API being developed in collaboration with the ESGF Compute Working Team to support server-side analytics for ESGF. The API can be executed using either direct web service calls, a python script or application, or a javascript-based web application. Client packages in python or javascript contain everything needed to make CDAS requests. The CDAS architecture brings together the tools, data storage, and high-performance computing required for timely analysis of large-scale data sets, where the data resides, to ultimately produce societal benefits. It is is currently deployed at NASA in support of the Collaborative REAnalysis Technical Environment (CREATE) project, which centralizes numerous global reanalysis datasets onto a single advanced data analytics platform. This service permits decision makers to investigate climate changes around the globe, inspect model trends, compare multiple reanalysis datasets, and variability.
22 CFR 228.17 - Special procurement rules for construction and engineering services.
Code of Federal Regulations, 2012 CFR
2012-04-01
... engineering services. 228.17 Section 228.17 Foreign Relations AGENCY FOR INTERNATIONAL DEVELOPMENT RULES FOR... construction and engineering services. Advanced developing countries, as defined in § 228.01, which USAID has... engineering services are not eligible to furnish USAID-financed construction and engineering services unless...
22 CFR 228.17 - Special procurement rules for construction and engineering services.
Code of Federal Regulations, 2013 CFR
2013-04-01
... engineering services. 228.17 Section 228.17 Foreign Relations AGENCY FOR INTERNATIONAL DEVELOPMENT RULES FOR... construction and engineering services. Advanced developing countries, as defined in § 228.01, which USAID has... engineering services are not eligible to furnish USAID-financed construction and engineering services unless...
22 CFR 228.17 - Special procurement rules for construction and engineering services.
Code of Federal Regulations, 2014 CFR
2014-04-01
... engineering services. 228.17 Section 228.17 Foreign Relations AGENCY FOR INTERNATIONAL DEVELOPMENT RULES FOR... construction and engineering services. Advanced developing countries, as defined in § 228.01, which USAID has... engineering services are not eligible to furnish USAID-financed construction and engineering services unless...
Engineering evaluation of a sodium hydroxide thermal energy storage module
NASA Technical Reports Server (NTRS)
Perdue, D. G.; Gordon, L. H.
1980-01-01
An engineering evaluation of thermal energy storage prototypes was performed in order to assess the development status of latent heat storage media. The testing and the evaluation of a prototype sodium hydroxide module is described. This module stored off-peak electrical energy as heat for later conversion to domestic hot water needs.