Bell X-1 Research Model on Single Support Strut in 7 x 10 Foot Wind Tu...
Modified Bell X-1 model pioneered variable-sweep studies in 1947. Photograph published in Sixty Years of Aeronautical Research 1917-1977 By David A. Anderton. A NASA publication, page 52.
Various Components of Goodyear Inflatable Airplane in Full Scale Tunne...
Various Components of Goodyear Inflatable Airplane in Full Scale Tunnel building 643 Test 238
Water Type Muffler Test NASA history collection
Water Type Muffler Test Public domain photograph of NASA experimental aircraft development, free to use, no copyright restrictions image - Picryl description
WS-110A "Brown Bomber" NASA history collection
WS-110A "Brown Bomber" Public domain photograph related to NASA research activity, space exploration, free to use, no copyright restrictions image - Picryl description
Test 1869 Medli/Meads, NASA Langley research center
Test 1869 Medli/Meads 7 hole probe mounted on a 10inch Arm.
The Unitary Plan Wind Tunnel(UPWT) Test 1891 Space Launch System
Stage Separation Test of the Space Launch System(SLS) in the Langley Unitary Plan Wind Tunnel (UPWT). The model used High Pressure air blown through the solid rocket boosters. (SRB) to simulate the booster sepa... More
KENNEDY SPACE CENTER, FLA. - KSC Deputy Director James W. Kennedy rec...
KENNEDY SPACE CENTER, FLA. - KSC Deputy Director James W. Kennedy receives the news of his appointment as the next director of the NASA Kennedy Space Center (KSC) before a group of KSC employees assembled in t... More
Crew Module Water Landing Model Assessment
Crew Module Water Landing Model Assessment (CMWLMA) Test site photos at Aberdeen Test Center Aberdeen Maryland
Crew Module Water Landing Model Assessment
Crew Module Water Landing Model Assessment (CMWLMA) Test site photos at Aberdeen Test Center Aberdeen Maryland
Crew Module Water Landing Model Assessment
Crew Module Water Landing Model Assessment (CMWLMA) Test site photos at Aberdeen Test Center Aberdeen Maryland
Crew Module Water Landing Model Assent (CMWLMA)
Crew Module Water Landing Model Assent Test site photos at Aberdeen Test Center (Aberdeen, MD)
Crew Module Water Landing Model Assent (CMWLMA)
Crew Module Water Landing Model Assent Test site photos at Aberdeen Test Center (Aberdeen, MD)
Crew Module Water Landing Model Assent (CMWLMA)
Crew Module Water Landing Model Assent Test site photos at Aberdeen Test Center (Aberdeen, MD)
Crew Model Water Landing Module Assessment
Crew Model Water Landing Module Assessment Photographs taken at Aberdeen Test Facility Aberdeen MD.
Crew Model Water Landing Module Assessment
Crew Model Water Landing Module Assessment Photographs taken at Aberdeen Test Facility Aberdeen MD.
Crew Model Water Landing Module Assessment
Crew Model Water Landing Module Assessment Photographs taken at Aberdeen Test Facility Aberdeen MD.
Crew Model Water Landing Module Assessment
Crew Model Water Landing Module Assessment Photographs taken at Aberdeen Test Facility Aberdeen MD.
Crew Model Water Landing Module Assessment
Crew Model Water Landing Module Assessment Photographs taken at Aberdeen Test Facility Aberdeen MD.
Crew Model Water Landing Module Assessment
Crew Model Water Landing Module Assessment Photographs taken at Aberdeen Test Facility Aberdeen MD.
Crew Model Water Landing Module Assessment
Crew Model Water Landing Module Assessment Photographs taken at Aberdeen Test Facility Aberdeen MD.
Crew Model Water Landing Module Assessment
Crew Model Water Landing Module Assessment Photographs taken at Aberdeen Test Facility Aberdeen MD.
Crew Model Water Landing Module Assessment
Crew Model Water Landing Module Assessment Photographs taken at Aberdeen Test Facility Aberdeen MD.
Crew Module Water Landing Model Assessment
Crew Module Water Landing Model Assessment (CMWLMA) Test site photos at Aberdeen Test Center Aberdeen Maryland
Crew Module Water Landing Model Assessment
Crew Module Water Landing Model Assessment (CMWLMA) Test site photos at Aberdeen Test Center Aberdeen Maryland
Crew Module Water Landing Model Assessment
Crew Module Water Landing Model Assessment (CMWLMA) Test site photos at Aberdeen Test Center Aberdeen Maryland
Crew Module Water Landing Model Assessment
Crew Module Water Landing Model Assessment (CMWLMA) Test site photos at Aberdeen Test Center Aberdeen Maryland
Crew Model Water Landing Module Assessment
Crew Model Water Landing Module Assessment Photographs taken at Aberdeen Test Facility Aberdeen MD.
Crew Model Water Landing Module Assessment
Crew Model Water Landing Module Assessment Photographs taken at Aberdeen Test Facility Aberdeen MD.
ORION Project-(SPLASH) Structural Passive Landing Attenuation fo
ORION Project-(SPLASH) Structural Passive Landing Attenuation for Survivability of Human Crew (BTA) Boiler Plate Test Article Water Impact Test-Pot Phase"0" Test POT#2 Tested at the Hydro Impact Basin at the L... More
ORION Project-(SPLASH) Structural Passive Landing Attenuation fo
ORION Project-(SPLASH) Structural Passive Landing Attenuation for Survivability of Human Crew (BTA) Boiler Plate Test Article Water Impact Test-Pot Phase"0" Test POT#2 Tested at the Hydro Impact Basin at the L... More
ORION Project-(SPLASH) Structural Passive Landing Attenuation fo
ORION Project-(SPLASH) Structural Passive Landing Attenuation for Survivability of Human Crew (BTA) Boiler Plate Test Article Water Impact Test-Pot Phase"0" Test POT#2 Tested at the Hydro Impact Basin at the L... More
ORION Project-(SPLASH) Structural Passive Landing Attenuation fo
ORION Project-(SPLASH) Structural Passive Landing Attenuation for Survivability of Human Crew (BTA) Boiler Plate Test Article Water Impact Test-Pot Phase"0" Test POT#2 Tested at the Hydro Impact Basin at the L... More
Orion Project SPLASH BTA Water Impact POT #3
Orion Project SPLASH BTA Water Impact POT Boiler Plate Test Article (BTA) (SPLASH) Structural Passive Landing Attenuation for Survivability of Human Crew. (POT) Phase "0" Test Water Impact Test #3
Orion Project SPLASH BTA Water Impact POT #3
Orion Project SPLASH BTA Water Impact POT Boiler Plate Test Article (BTA) (SPLASH) Structural Passive Landing Attenuation for Survivability of Human Crew. (POT) Phase "0" Test Water Impact Test #3
Orion Project SPLASH BTA Water Impact POT #3
Orion Project SPLASH BTA Water Impact POT Boiler Plate Test Article (BTA) (SPLASH) Structural Passive Landing Attenuation for Survivability of Human Crew. (POT) Phase "0" Test Water Impact Test #3
Orion Project SPLASH BTA Water Impact POT #3
Orion Project SPLASH BTA Water Impact POT Boiler Plate Test Article (BTA) (SPLASH) Structural Passive Landing Attenuation for Survivability of Human Crew. (POT) Phase "0" Test Water Impact Test #3
Orion Project SPLASH BTA Water Impact POT #3
Orion Project SPLASH BTA Water Impact POT Boiler Plate Test Article (BTA) (SPLASH) Structural Passive Landing Attenuation for Survivability of Human Crew. (POT) Phase "0" Test Water Impact Test #3
Osprey UAV, NASA Langley research center
Osprey (UAV) Unmanned Aerial Vehicle ; flight vehicle test at 14x22 tunnel. Test number 605 from Eglin AFB. Take at 14x22 Subsonic Tunnel
ORION Project-(SPLASH) Structural Passive Landing Attenuation fo
ORION Project-(SPLASH) Structural Passive Landing Attenuation for Survivability of Human Crew (BTA) Boiler Plate Test Article Water Impact Test-Pot Phase"0" Test Tested at the Hydro Impact Basin at the Landing... More
ORION Project-(SPLASH) Structural Passive Landing Attenuation fo
ORION Project-(SPLASH) Structural Passive Landing Attenuation for Survivability of Human Crew (BTA) Boiler Plate Test Article Water Impact Test-Pot Phase"0" Test Tested at the Hydro Impact Basin at the Landing... More
ORION Project-(SPLASH) Structural Passive Landing Attenuation fo
ORION Project-(SPLASH) Structural Passive Landing Attenuation for Survivability of Human Crew (BTA) Boiler Plate Test Article Water Impact Test-Pot Phase"0" Test Tested at the Hydro Impact Basin at the Landing... More
ORION Project-(SPLASH) Structural Passive Landing Attenuation fo
ORION Project-(SPLASH) Structural Passive Landing Attenuation for Survivability of Human Crew (BTA) Boiler Plate Test Article Water Impact Test-P1T#2 Tested at the Hydro Impact Basin at the Landing and Impact ... More
ORION Project-(SPLASH) Structural Passive Landing Attenuation fo
ORION Project-(SPLASH) Structural Passive Landing Attenuation for Survivability of Human Crew (BTA) Boiler Plate Test Article Water Impact Test-P1T#2 Tested at the Hydro Impact Basin at the Landing and Impact ... More
ORION Project-(SPLASH) Structural Passive Landing Attenuation fo
ORION Project-(SPLASH) Structural Passive Landing Attenuation for Survivability of Human Crew (BTA) Boiler Plate Test Article Water Impact Test-P1T#2 Tested at the Hydro Impact Basin at the Landing and Impact ... More
ORION Project-(SPLASH) Structural Passive Landing Attenuation fo
ORION Project-(SPLASH) Structural Passive Landing Attenuation for Survivability of Human Crew (BTA) Boiler Plate Test Article Water Impact Test-Pot Phase"0" Test Tested at the Hydro Impact Basin at the Landing... More
ORION Project-(SPLASH) Structural Passive Landing Attenuation fo
ORION Project-(SPLASH) Structural Passive Landing Attenuation for Survivability of Human Crew (BTA) Boiler Plate Test Article Water Impact Test-PIT Test-2 Tested at the Hydro Impact Basin at the Landing and Im... More
ORION Project-(SPLASH) Structural Passive Landing Attenuation fo
ORION Project-(SPLASH) Structural Passive Landing Attenuation for Survivability of Human Crew (BTA) Boiler Plate Test Article Water Impact Test-PIT Test-2 Tested at the Hydro Impact Basin at the Landing and Im... More
ORION Project-(SPLASH) Structural Passive Landing Attenuation fo
ORION Project-(SPLASH) Structural Passive Landing Attenuation for Survivability of Human Crew (BTA) Boiler Plate Test Article Water Impact Test-PIT Test-2 Tested at the Hydro Impact Basin at the Landing and Im... More
ORION Project-(SPLASH) Structural Passive Landing Attenuation fo
ORION Project-(SPLASH) Structural Passive Landing Attenuation for Survivability of Human Crew (BTA) Boiler Plate Test Article Water Impact Test-PIT Test-2 Tested at the Hydro Impact Basin at the Landing and Im... More
ORION Project-(SPLASH) Structural Passive Landing Attenuation fo
ORION Project-(SPLASH) Structural Passive Landing Attenuation for Survivability of Human Crew (BTA) Boiler Plate Test Article Water Impact Test-PIT Test-2 Tested at the Hydro Impact Basin at the Landing and Im... More
ORION Project-(SPLASH) Structural Passive Landing Attenuation fo
ORION Project-(SPLASH) Structural Passive Landing Attenuation for Survivability of Human Crew (BTA) Boiler Plate Test Article Water Impact Test-PIT Test-2 Tested at the Hydro Impact Basin at the Landing and Im... More
CAPE CANAVERAL, Fla. -- A view of one of the work stands in the Operat...
CAPE CANAVERAL, Fla. -- A view of one of the work stands in the Operations and Checkout O&C Facility at NASA's Kennedy Space Center in Florida where the Orion ground test vehicle has arrived. The vehicle travel... More
CAPE CANAVERAL, Fla. -- Lockheed Martin crews assist as a crane lowers...
CAPE CANAVERAL, Fla. -- Lockheed Martin crews assist as a crane lowers the Orion ground test vehicle on to a work stand in the Operations and Checkout O&C Facility at NASA's Kennedy Space Center in Florida. The... More
CAPE CANAVERAL, Fla. -- A view of the high bay in the Operations and C...
CAPE CANAVERAL, Fla. -- A view of the high bay in the Operations and Checkout O&C Facility at NASA’s Kennedy Space Center in Florida where the Orion ground test vehicle has arrived. The vehicle traveled more th... More
Aerials of NASA Langley Research Center
Aerial view of NASA Langley Research Center west side
Aerials of NASA Langley Research Center
Aerial of NASA Langley Reaseach Center west side
Aerials of NASA Langley Research Center
Aerial of NASA Langley Reaseach Center west side
Orion SPLASH BTA Phase 2 Vertical Tests 9: at NASA Langley Resea
SPLASH BTA Phase 2 Vertical Tests 9: Documentation of preparation, set up and results of full scale BTA (Boilerplate Test Article) vertical drop test series performed in 2012 at the LaRC Hydro Impact Basin (HIB)
Orion SPLASH BTA Phase 2 Vertical Tests 9: at NASA Langley Resea
SPLASH BTA Phase 2 Vertical Tests 9: Documentation of preparation, set up and results of full scale BTA (Boilerplate Test Article) vertical drop test series performed in 2012 at the LaRC Hydro Impact Basin (HIB)
Orion SPLASH BTA Phase 2 Vertical Tests 9: at NASA Langley Resea
SPLASH BTA Phase 2 Vertical Tests 9: Documentation of preparation, set up and results of full scale BTA (Boilerplate Test Article) vertical drop test series performed in 2012 at the LaRC Hydro Impact Basin (HIB)
Orion SPLASH BTA Phase 2 Vertical Tests 9: at NASA Langley Resea
SPLASH BTA Phase 2 Vertical Tests 9: Documentation of preparation, set up and results of full scale BTA (Boilerplate Test Article) vertical drop test series performed in 2012 at the LaRC Hydro Impact Basin (HIB)
Orion SPLASH P1 Test 7 Swing Test at NASA Langley Research Cente
SPLASH P1 Test 7 Swing Test: Documentation of preparation, set up and results of full scale BTA (Boilerplate Test Article) vertical drop test series performed in 2012 at the LaRC Hydro Impact Basin (HIB)
Orion SPLASH P1 Test 7 Swing Test at NASA Langley Research Cente
SPLASH P1 Test 7 Swing Test: Documentation of preparation, set up and results of full scale BTA (Boilerplate Test Article) vertical drop test series performed in 2012 at the LaRC Hydro Impact Basin (HIB)
Orion SPLASH P1 Test 7 Swing Test at NASA Langley Research Cente
SPLASH P1 Test 7 Swing Test: Documentation of preparation, set up and results of full scale BTA (Boilerplate Test Article) vertical drop test series performed in 2012 at the LaRC Hydro Impact Basin (HIB)
Orion SPLASH P1 Test 7 Swing Test at NASA Langley Research Cente
SPLASH P1 Test 7 Swing Test: Documentation of preparation, set up and results of full scale BTA (Boilerplate Test Article) vertical drop test series performed in 2012 at the LaRC Hydro Impact Basin (HIB)
(NTF) National Transonic Facility Test 213-SFW Flow Control II,
(NTF) National Transonic Facility Test 213-SFW Flow Control II, Fast-MAC Model: The fundamental Aerodynamics Subsonic Transonic-Modular Active Control (Fast-MAC) Model was tested for the 2nd time in the NTF. ... More
CAPE CANAVERAL, Fla. – Near the Shuttle Landing Facility at NASA's Ken...
CAPE CANAVERAL, Fla. – Near the Shuttle Landing Facility at NASA's Kennedy Space Center in Florida, a technician installs hazard avoidance instrumentation on a Huey helicopter. Led by the Johnson Space Cen... More
CAPE CANAVERAL, Fla. – Near the Shuttle Landing Facility at NASA's Ken...
CAPE CANAVERAL, Fla. – Near the Shuttle Landing Facility at NASA's Kennedy Space Center in Florida, hazard avoidance instrumentation it being prepared for installation on a Huey helicopter. Led by the John... More
CAPE CANAVERAL, Fla. – Near the Shuttle Landing Facility at NASA's Ken...
CAPE CANAVERAL, Fla. – Near the Shuttle Landing Facility at NASA's Kennedy Space Center in Florida, a space agency team installed and tested hazard avoidance instrumentation on a Huey helicopter. Led by the Joh... More
CAPE CANAVERAL, Fla. – Near the Shuttle Landing Facility at NASA's Ken...
CAPE CANAVERAL, Fla. – Near the Shuttle Landing Facility at NASA's Kennedy Space Center in Florida, a space agency team installed and tested hazard avoidance instrumentation on a Huey helicopter. Led by the Joh... More
CAPE CANAVERAL, Fla. – Near the Shuttle Landing Facility at NASA's Ken...
CAPE CANAVERAL, Fla. – Near the Shuttle Landing Facility at NASA's Kennedy Space Center in Florida, a space agency team installed and tested hazard avoidance instrumentation on a Huey helicopter. Led by the Joh... More
1.2 meter Multi-Mission Earth Entry Vehicle (MMEEV)
1.2 meter Multi-Mission Earth Entry Vehicle (MMEEV): Tethered and free flying test in 20 foot Vertical Spin Tunnel
Aeronautic Academy Continuous Trailing Edge Flap
Aeronautic Academy Continuous Trailing Edge Flap Public domain photograph of NASA experimental aircraft development, free to use, no copyright restrictions image - Picryl description
L-59 RC Kit Model/ Learn to Fly Test
L59 RC Kit Model/Learn to fly test technique and modeling development Persons in the picture: Left to right: Jay Brandon, Sue Grafton, Wes O'Neal, Mark Croom, Earl Harris, and Eric Viken
The Orion Test Capsule at NASA's Langley Research Center's Hydro
The Orion Test Capsule spent 4 hour in the water tank under NASA Langley's gantry to prove it is ready for the open water recovery test at Norfolk Naval Station.
The Orion Test Capsule and a number of other items used in the c
The Orion Test Capsule and a number of other items used in the capsule recovery at being transported down the James River on a Navy INLS "Improved Navy Lighterage System" from Fort Eustis from where it was load... More
NASA and the U.S. Navy conducted a stationary Recovery Test on t
On August 15, 2013, at the Naval Station Norfolk near NASA’s Langley Research Center in Virginia, NASA and the U.S. Navy conducted a stationary recovery test on the Orion boilerplate test article in the water n... More
(TRACT) Transport Rotorcraft Aircraft Testbed
(TRACT) Transport Rotorcraft Aircraft Testbed: Helicopter airframe drop test at NASA Langley's Landing and Impact Research Facility (LandIR)
(TRACT) Transport Rotorcraft Aircraft Testbed
(TRACT) Transport Rotorcraft Aircraft Testbed: Helicopter airframe drop test at NASA Langley's Landing and Impact Research Facility (LandIR)
MIT N+3 D8 1/11 Scale Model in the 14x22 Foot Subsonic Tunnel
Doublebubble MIT N+3 D8 1/11 Scale Model in the 14x22 Foot Subsonic Tunnel
13.1 Foot Diameter Fluted-Core Sandwich Composite Test Article
White light shape and measurement of a 13.1 Foot diameter fluted-core sandwich composite test article designed by LaRC and fabricated by Boeing Under Space Act Agreement SAA1-737, Annex 14. to be tested in LaRC... More
13.1 Foot Diameter Fluted-Core Sandwich Composite Test Article
White light shape and measurement of a 13.1 Foot diameter fluted-core sandwich composite test article designed by LaRC and fabricated by Boeing Under Space Act Agreement SAA1-737, Annex 14. to be tested in LaRC... More
Hybrid Wing Body Particle Image Velocimetry Test in LaRC 14x22 F
Hybrid Wing Body Particle Image Velocimetry Test in LaRC 14x22 Foot Tunnel: PIV measurement of HWB-N2A model in Langley 14x22 Foot Tunnel
(SLAP) Scanning L-band Active Passive Installed on NASA UC-12B A
SLAP antenna and external fairing mounted on UC-12B; view looking aft
(NESC) NASA Engineering and Safety Center Orion Heat Shield Carr
(NESC) NASA Engineering and Safety Center Orion Heat Shield Carrier Structure: Titanium Orthogrid heat shield sub-component dynamic test article : person in the photo Jim Jeans (Background: Mike Kirsch, James ... More
The 2014 Annual(MCWG)Annual Metrology and Calibration Working Gr
Annual Metrology and Calibration Working Group Face to Face meeting held at Langley Research Center; Front Row (L to R): Stacy Sigmon – LaRC, Brent Watling – JSC, Ralph Hickman – WFF, Kirk Foster – MSFC, Don ... More
TRACT 2 Frame Drop Test AT NASA Langley Research Center's Landin
TRACT 2 Frame Drop Test AT NASA Langley Research Center's Landing and Impact Research (LandIR) Facility
TRACT 2 Frame Drop Test AT NASA Langley Research Center's Landin
TRACT 2 Frame Drop Test AT NASA Langley Research Center's Landing and Impact Research (LandIR) Facility
TRACT 2 Frame Drop Test AT NASA Langley Research Center's Landin
TRACT 2 Frame Drop Test AT NASA Langley Research Center's Landing and Impact Research (LandIR) Facility
TRACT 2 Frame Drop Test AT NASA Langley Research Center's Landin
(Tract)2 Transport Rotorcraft Airframe Crash Testbed; Full Frame Drop Test: rotary wing crash worthiness, impact research at NASA Langley Research Center's Landing and Impact Research (LandIR) Facility Building 1297
TRACT 2 Frame Drop Test AT NASA Langley Research Center's Landin
TRACT 2 Frame Drop Test AT NASA Langley Research Center's Landing and Impact Research (LandIR) Facility
TRACT 2 Frame Drop Test AT NASA Langley Research Center's Landin
(Tract)2 Transport Rotorcraft Airframe Crash Testbed; Full Frame Drop Test: rotary wing crash worthiness, impact research at NASA Langley Research Center's Landing and Impact Research (LandIR) Facility Building 1297
5.75% Scale Boeing BWB-0009G Model in NASA Langley 14x22 Foot Tu
5.75% Scale Boeing BWB-0009G Model in NASA Langley 14x22 Foot Tunnel: Low speed aerodynamics test of BWB model with flow-thru nacelles in Langley 14x22 foot tunnel(test 617)
5.75% Scale Boeing BWB-0009G Model in NASA Langley 14x22 Foot Tu
5.75% Scale Boeing BWB-0009G Model in NASA Langley 14x22 Foot Tunnel: Low speed aerodynamics test of BWB model with flow-thru nacelles in Langley 14x22 foot tunnel(test 617)
Construction of the 30 x 60 Foot Wind Tunnel at Langley
Full Description: This photograph from 1930 shows the 30 x 60 Foot Tunnel during construction. Smith J. de France, a NACA engineer, was in charge of the design team for the new tunnel. Planning involved the con... More
Bell X-1 Research Model on Single Support Strut in 7 x 10 Foot Wind Tu...
Modified Bell X-1 model pioneered variable-sweep studies in 1947. Photograph published in Sixty Years of Aeronautical Research 1917-1977 By David A. Anderton. A NASA publication, page 52.
Bell X-1 Research Model on Single Support Strut in 7 x 10 Foot Wind Tu...
Modified Bell X-1 model pioneered variable-sweep studies in 1947. Photograph published in Sixty Years of Aeronautical Research 1917-1977 By David A. Anderton. A NASA publication, page 52.
Bell X-1 Research Model on Single Support Strut in 7 x 10 Foot Wind Tu...
Modified Bell X-1 model pioneered variable-sweep studies in 1947. Photograph published in Sixty Years of Aeronautical Research 1917-1977 By David A. Anderton. A NASA publication, page 52.
North American X-15 Drop Model. NASA public domain image colelction.
North American X-15 Drop Model Public domain photograph of NASA experimental aircraft development, free to use, no copyright restrictions image - Picryl description
Water Type Muffler Test NASA history collection
Water Type Muffler Test Public domain photograph related to NASA research activity, space exploration, free to use, no copyright restrictions image - Picryl description