NASA GLENN/NASA LANGLEY LOADS COMPARISON TEST WITH 6 COMPONENT FORCE/MOMENT BALANCE AND 1.7% HIGH SPEED RESEARCH MODEL 5. in the 10x10 super sonic wind tunnel
NASA GLENN/NASA LANGLEY LOADS COMPARISON TEST WITH 6 COMPONENT FORCE/MOMENT BALANCE AND 1.7% HIGH SPEED RESEARCH MODEL 5.
NASA Administrator Jared Isaacman is seen sitting in his jet ready to take off from Cleveland Hopkins Airport. Seated in the back seat is rider Heather Brown.  This is part of the 2026 NASA Inspiration Tours
Freedom 250 flights
Carolyn Thiemann works on the Cobra data system in the IRT control room
Carolyn Thiemann works on the Cobra data system in the IRT control room
Parametric Inlet Model in 10x10 Wind Tunnel
GRC-2004-C-00378
NASA GLENN/NASA LANGLEY LOADS COMPARISON TEST WITH 6 COMPONENT FORCE/MOMENT BALANCE AND 1.7% HIGH SPEED RESEARCH MODEL 5.
NASA GLENN/NASA LANGLEY LOADS COMPARISON TEST WITH 6 COMPONENT FORCE/MOMENT BALANCE AND 1.7% HIGH SPEED RESEARCH MODEL 5.
February 17, 2021, The Terminal Tower is illuminated in red to commemorate the Landing of NASA’s Perseverance Rover on the surface of Mars, February 18, 2021.  Terminal Tower is a 52-story, (771 ft), landmark skyscraper located on Public Square in downtown Cleveland, Ohio.  Cleveland is also the home of the NASA Glenn Research Center.
Terminal Tower illuminated in red to commemorate the Mars Landing of Perseverance Rover
NASA GLENN/NASA LANGLEY LOADS COMPARISON TEST WITH 6 COMPONENT FORCE/MOMENT BALANCE AND 1.7% HIGH SPEED RESEARCH MODEL 5.
NASA GLENN/NASA LANGLEY LOADS COMPARISON TEST WITH 6 COMPONENT FORCE/MOMENT BALANCE AND 1.7% HIGH SPEED RESEARCH MODEL 5.
NASA Glenn/NASA Langley, Loads Comparison Test With 6 Component Force/Moment Balance and 1.7% High Speed Research, HSR Model 5. In the Glenn Research Center 10x10 Foot Supersonic Wind Tunnel, SWT
NASA Glenn/NASA Langley Loads Comparison Test with 6 Component Force/Moment Balance and 1.7% High Speed Research, HSR Model 5
NASA GLENN/NASA LANGLEY LOADS COMPARISON TEST WITH 6 COMPONENT FORCE/MOMENT BALANCE AND 1.7% HIGH SPEED RESEARCH MODEL 5.
NASA GLENN/NASA LANGLEY LOADS COMPARISON TEST WITH 6 COMPONENT FORCE/MOMENT BALANCE AND 1.7% HIGH SPEED RESEARCH MODEL 5.
NASA GLENN/NASA LANGLEY LOADS COMPARISON TEST WITH 6 COMPONENT FORCE/MOMENT BALANCE AND 1.7% HIGH SPEED RESEARCH MODEL 5.
NASA GLENN/NASA LANGLEY LOADS COMPARISON TEST WITH 6 COMPONENT FORCE/MOMENT BALANCE AND 1.7% HIGH SPEED RESEARCH MODEL 5.
A spectrally resolved Rayleigh/Mie scattering diagnostic was developed to measure temperature and wingspan wise velocity in the vicinity of an ASTOVL aircraft model tested in the Lewis, now Glenn, 9x15 Low Speed Wind Tunnel.  This was done for the Phase III hot gas ingestion study of ground-effect flow-field on such aircraft during hover or vertical landing.
ASTOVL (advanced short takeoff vertical landing) aircraft test laser develpment. Phase III hot gas ingestion study of ground-effect flow-field on such aircraft during hover or vertical landing
NASA GRC PSL, Propulsion System Lab, control room with operations personnel
NASA GRC PSL, Propulsion System Lab, control room
Photographs taken from the T-34 of the PC-12 in flight over the technology corridor and the Honda motor company and the Honda test track
Pilatus PC-12 aircraft in flight over the Cleveland area and the
Cleveland’s Terminal Tower as seen from Public Square was lit up “Mars Red” leading up the Perseverance Rover’s arrival on Mars Wednesday night February 18th and Thursday morning.
GRC-2021-C-00208
The 9x15 low speed tunnel tests take off and landing of aircraft.  The laser velocimetry system for flow measurement show here, with the color blue and green lasers, measures engine exhaust that comes back up from the ground.  The STOVL model n the 9x15 low speed wind tunnel, building 39, is similar to the British Harrier aircraft.
STOVL (Short Take Off Vertical Landing) Phase III Hot Gas Ingestion Into Engine Intake Test in the 9x15 Low Speed Wind Tunnel
NASA GLENN/NASA LANGLEY LOADS COMPARISON TEST WITH 6 COMPONENT FORCE/MOMENT BALANCE AND 1.7% HIGH SPEED RESEARCH MODEL 5.
NASA GLENN/NASA LANGLEY LOADS COMPARISON TEST WITH 6 COMPONENT FORCE/MOMENT BALANCE AND 1.7% HIGH SPEED RESEARCH MODEL 5.
NASA GLENN/NASA LANGLEY LOADS COMPARISON TEST WITH 6 COMPONENT FORCE/MOMENT BALANCE AND 1.7% HIGH SPEED RESEARCH MODEL 5.
NASA GLENN/NASA LANGLEY LOADS COMPARISON TEST WITH 6 COMPONENT FORCE/MOMENT BALANCE AND 1.7% HIGH SPEED RESEARCH MODEL 5.
February 17, 2021, The Terminal Tower is illuminated in red to commemorate the Landing of NASA’s Perseverance Rover on the surface of Mars, February 18, 2021.  Terminal Tower is a 52-story, (771 ft), landmark skyscraper located on Public Square in downtown Cleveland, Ohio.  Cleveland is also the home of the NASA Glenn Research Center.
Terminal Tower illuminated in red to commemorate the Mars Landing of Perseverance Rover
February 17, 2021, The Terminal Tower is illuminated in red to commemorate the Landing of NASA’s Perseverance Rover on the surface of Mars, February 18, 2021.  Terminal Tower is a 52-story, (771 ft), landmark skyscraper located on Public Square in downtown Cleveland, Ohio.  Cleveland is also the home of the NASA Glenn Research Center.
Terminal Tower illuminated in red to commemorate the Mars Landing of Perseverance Rover
February 17, 2021, The Terminal Tower is illuminated in red to commemorate the Landing of NASA’s Perseverance Rover on the surface of Mars, February 18, 2021.  Terminal Tower is a 52-story, (771 ft), landmark skyscraper located on Public Square in downtown Cleveland, Ohio.  Cleveland is also the home of the NASA Glenn Research Center.
Terminal Tower illuminated in red to commemorate the Mars Landing of Perseverance Rover
NASA GLENN/NASA LANGLEY LOADS COMPARISON TEST WITH 6 COMPONENT FORCE/MOMENT BALANCE AND 1.7% HIGH SPEED RESEARCH MODEL 5.
NASA GLENN/NASA LANGLEY LOADS COMPARISON TEST WITH 6 COMPONENT FORCE/MOMENT BALANCE AND 1.7% HIGH SPEED RESEARCH MODEL 5.
Cleveland’s Terminal Tower as seen from Voinovich Bicentennial Park was lit up “Mars Red” leading up the Perseverance Rover’s arrival on Mars Wednesday night February 18th and Thursday morning.
GRC-2021-C-00202
Shigehiro Nishino -- Visiting faculty fellow Dr. Shigehiro Nishino introduced the Lewis team to a unique chemical vapor deposition (CVD) strategy to grow silicon carbide crystals on silicon wafers.
CHEMICAL VAPOR DEPOSITION CVD REACTION CHAMBER
February 17, 2021, The Terminal Tower is illuminated in red to commemorate the Landing of NASA’s Perseverance Rover on the surface of Mars, February 18, 2021.  Terminal Tower is a 52-story, (771 ft), landmark skyscraper located on Public Square in downtown Cleveland, Ohio.  Cleveland is also the home of the NASA Glenn Research Center.
Terminal Tower illuminated in red to commemorate the Mars Landing of Perseverance Rover
SFD (Subsonic Flight Demonstrator) of SLD (Super Large Drop) testing in IRT (Icing Research Tunnel).  Drop size shown on computer from detection probe during test. Cloud drops imaged by probe displayed on computer screen
FY26-2225-SFD Droplet Testing in IRT
SFD (Subsonic Flight Demonstrator) of SLD (Supercooled Large Drop) Instrumentation Test - Particle Size Measurement in the IRT (Icing Research Tunnel), June 8-11, 2026. Drop size shown on computer from Drop Sizing Probe seen in the IRT test section.
FY26-2225-SFD Droplet Testing in IRT
Ice collection seen on un-heated sections of the 1D2D-X ice drop detection probe in the test section of the IRT (Icing Research Tunnel). Drop Size Probe testing - SFD (Subsonic Flight Demonstrator) of SLD (Supercooled Large Drop) Instrumentation Test in IRT (Icing Research Tunnel) – Particle Size Distribution Entry, June 8-11, 2026 Large Drop Testing in IRT
FY26-2225-SFD Droplet Testing in IRT
Ice collection seen on un-heated sections of the 1D2D-X ice drop detection probe in the test section of the IRT (Icing Research Tunnel). Drop Size Probe testing - SFD (Subsonic Flight Demonstrator) of SLD (Supercooled Large Drop) Instrumentation Test in IRT (Icing Research Tunnel) – Particle Size Distribution Entry, June 8-11, 2026 Large Drop Testing in IRT
FY26-2225-SFD Droplet Testing in IRT
SFD (Subsonic Flight Demonstrator) of SLD (Supercooled Large Drop Instrumentation Test - Particle Size Measurements. Installation of 1D2D-X probe in the IRT. Probe supplied by Science Engineering Associates (SEA)
FY26-2225-SFD Droplet Testing in IRT
Ice collection seen on un-heated sections of the 1D2D-X ice drop detection probe in the test section of the IRT (Icing Research Tunnel). Drop Size Probe testing - SFD (Subsonic Flight Demonstrator) of SLD (Supercooled Large Drop) Instrumentation Test in IRT (Icing Research Tunnel) – Particle Size Distribution Entry, June 8-11, 2026 Large Drop Testing in IRT
FY26-2225-SFD Droplet Testing in IRT
Installation of 1D2D-X  probe in the IRT.  Probe supplied by Science Engineering Associates (SEA). SFD (Subsonic Flight Demonstrator) of SLD (Supercooled Large Drop Instrumentation Test - Particle Size Measurements. Particle Size Distribution Entry, June 8-11, 2026 Large Drop Testing in IRT
FY26-2225-SFD Droplet Testing in IRT
SFD (Subsonic Flight Demonstrator) test of SLD (Supercooled Large Drop) Instrumentation Test - Particle Size Measurements Testing in IRT (Icing Research Tunnel). Installation of probe in the IRT. Installation of 1D2D-X probe in the IRT.  Probe supplied by Science Engineering Associates (SEA)
FY26-2225-SFD Droplet Testing in IRT
SFD (Subsonic Flight Demonstrator) of SLD (Supercooled Large Drop) Instrumentation Test - Particle Size Measurement in the IRT (Icing Research Tunnel), June 8-11, 2026. Drop size shown on computer from Drop Sizing Probe seen in the IRT test section.
FY26-2225-SFD Droplet Testing in IRT
Ice collection seen on un-heated sections of the ice drop detection probe in the test section of the IRT (Icing Research Tunnel). Drop Size Probe testing - SFD (Subsonic Flight Demonstrator) of SLD (Supercooled Large Drop) Instrumentation Test in IRT (Icing Research Tunnel) – Particle Size Distribution Entry, June 8-11, 2026
FY26-2225-SFD Droplet Testing in IRT
Commercial Supersonic Transport, CST Project, X-59 Sonic Boom Test Model, in the 8x6-foot Supersonic Wind Tunnel, SWT
X-59
Commercial Supersonic Transport, CST Project, X-59 Sonic Boom Test Model, in the 8x6-foot Supersonic Wind Tunnel, SWT
X-59
Commercial Supersonic Transport, CST Project, X-59 Sonic Boom Test Model, in the 8x6-foot Supersonic Wind Tunnel, SWT
X-59
Commercial Supersonic Transport, CST Project, X-59 Sonic Boom Test Model, in the 8x6-foot Supersonic Wind Tunnel, SWT
X-59
Commercial Supersonic Transport, CST Project, X-59 Sonic Boom Test Model, in the 8x6-foot Supersonic Wind Tunnel, SWT
X-59
Commercial Supersonic Transport, CST Project, X-59 Sonic Boom Test Model, in the 8x6-foot Supersonic Wind Tunnel, SWT
X-59
Commercial Supersonic Transport, CST Project, X-59 Sonic Boom Test Model, in the 8x6-foot Supersonic Wind Tunnel, SWT
X-59
Commercial Supersonic Transport, CST Project, X-59 Sonic Boom Test Model, in the 8x6-foot Supersonic Wind Tunnel, SWT
X-59
Commercial Supersonic Transport, CST Project, X-59 Sonic Boom Test Model, in the 8x6-foot Supersonic Wind Tunnel, SWT
X-59
Commercial Supersonic Transport, CST Project, X-59 Sonic Boom Test Model, in the 8x6-foot Supersonic Wind Tunnel, SWT
X-59
Commercial Supersonic Transport, CST Project, X-59 Sonic Boom Test Model, in the 8x6-foot Supersonic Wind Tunnel, SWT
X-59
Commercial Supersonic Transport, CST Project, X-59 Sonic Boom Test Model, in the 8x6-foot Supersonic Wind Tunnel, SWT
X-59
Commercial Supersonic Transport, CST Project, X-59 Sonic Boom Test Model, in the 8x6-foot Supersonic Wind Tunnel, SWT
X-59
Commercial Supersonic Transport, CST Project, X-59 Sonic Boom Test Model, in the 8x6-foot Supersonic Wind Tunnel, SWT
X-59
Commercial Supersonic Transport, CST Project, X-59 Sonic Boom Test Model, in the 8x6-foot Supersonic Wind Tunnel, SWT
X-59
Commercial Supersonic Transport, CST Project, X-59 Sonic Boom Test Model, in the 8x6-foot Supersonic Wind Tunnel, SWT
X-59
Commercial Supersonic Transport, CST Project, X-59 Sonic Boom Test Model, in the 8x6-foot Supersonic Wind Tunnel, SWT
X-59
Commercial Supersonic Transport, CST Project, X-59 Sonic Boom Test Model, in the 8x6-foot Supersonic Wind Tunnel, SWT
X-59
Commercial Supersonic Transport, CST Project, X-59 Sonic Boom Test Model, in the 8x6-foot Supersonic Wind Tunnel, SWT
X-59
Commercial Supersonic Transport, CST Project, X-59 Sonic Boom Test Model, in the 8x6-foot Supersonic Wind Tunnel, SWT
X-59
Commercial Supersonic Transport, CST Project, X-59 Sonic Boom Test Model, in the 8x6-foot Supersonic Wind Tunnel, SWT
X-59
Commercial Supersonic Transport, CST Project, X-59 Sonic Boom Test Model, in the 8x6-foot Supersonic Wind Tunnel, SWT
X-59
Commercial Supersonic Transport, CST Project, X-59 Sonic Boom Test Model, in the 8x6-foot Supersonic Wind Tunnel, SWT
X-59
Commercial Supersonic Transport, CST Project, X-59 Sonic Boom Test Model, in the 8x6-foot Supersonic Wind Tunnel, SWT
X-59
Commercial Supersonic Transport, CST Project, X-59 Sonic Boom Test Model, in the 8x6-foot Supersonic Wind Tunnel, SWT
X-59
Commercial Supersonic Transport, CST Project, X-59 Sonic Boom Test Model, in the 8x6-foot Supersonic Wind Tunnel, SWT
X-59
Commercial Supersonic Transport, CST Project, X-59 Sonic Boom Test Model, in the 8x6-foot Supersonic Wind Tunnel, SWT
X-59
Commercial Supersonic Transport, CST Project, X-59 Sonic Boom Test Model, in the 8x6-foot Supersonic Wind Tunnel, SWT
X-59
Commercial Supersonic Transport, CST Project, X-59 Sonic Boom Test Model, in the 8x6-foot Supersonic Wind Tunnel, SWT
X-59
Commercial Supersonic Transport, CST Project, X-59 Sonic Boom Test Model, in the 8x6-foot Supersonic Wind Tunnel, SWT
X-59
Commercial Supersonic Transport, CST Project, X-59 Sonic Boom Test Model, in the 8x6-foot Supersonic Wind Tunnel, SWT
X-59
Commercial Supersonic Transport, CST Project, X-59 Sonic Boom Test Model, in the 8x6-foot Supersonic Wind Tunnel, SWT
X-59
Commercial Supersonic Transport, CST Project, X-59 Sonic Boom Test Model, in the 8x6-foot Supersonic Wind Tunnel, SWT
X-59
Commercial Supersonic Transport, CST Project, X-59 Sonic Boom Test Model, in the 8x6-foot Supersonic Wind Tunnel, SWT
X-59
Commercial Supersonic Transport, CST Project, X-59 Sonic Boom Test Model, in the 8x6-foot Supersonic Wind Tunnel, SWT
X-59
Commercial Supersonic Transport, CST Project, X-59 Sonic Boom Test Model, in the 8x6-foot Supersonic Wind Tunnel, SWT
X-59
Commercial Supersonic Transport, CST Project, X-59 Sonic Boom Test Model, in the 8x6-foot Supersonic Wind Tunnel, SWT
X-59
Commercial Supersonic Transport, CST Project, X-59 Sonic Boom Test Model, in the 8x6-foot Supersonic Wind Tunnel, SWT
X-59
Commercial Supersonic Transport, CST Project, X-59 Sonic Boom Test Model, in the 8x6-foot Supersonic Wind Tunnel, SWT
X-59
Supersonic Short Take Off Vertical Landing Hot Gas Ingestion Model Testing in the 9x15-foot Low Speed Wind Tunnel, LSWT
GRC-1993-C-07355
Commercial Supersonic Transport, CST Project, X-59 Sonic Boom Test Model, in the 8x6-foot Supersonic Wind Tunnel, SWT
X-59
Commercial Supersonic Transport, CST Project, X-59 Sonic Boom Test Model, in the 8x6-foot Supersonic Wind Tunnel, SWT
GRC-2021-C-03339
Commercial Supersonic Transport, CST Project, X-59 Sonic Boom Test Model, in the 8x6-foot Supersonic Wind Tunnel, SWT
GRC-2021-C-03331
Commercial Supersonic Transport, CST Project, X-59 Sonic Boom Test Model, in the 8x6-foot Supersonic Wind Tunnel, SWT
GRC-2021-C-03327
Commercial Supersonic Transport, CST Project, X-59 Sonic Boom Test Model, in the 8x6-foot Supersonic Wind Tunnel, SWT
GRC-2021-C-03366
Commercial Supersonic Transport, CST Project, X-59 Sonic Boom Test Model, in the 8x6-foot Supersonic Wind Tunnel, SWT
GRC-2021-C-03332
Commercial Supersonic Transport, CST Project, X-59 Sonic Boom Test Model, in the 8x6-foot Supersonic Wind Tunnel, SWT
GRC-2021-C-03326
Commercial Supersonic Transport, CST Project, X-59 Sonic Boom Test Model, in the 8x6-foot Supersonic Wind Tunnel, SWT
GRC-2021-C-03342
Commercial Supersonic Transport, CST Project, X-59 Sonic Boom Test Model, in the 8x6-foot Supersonic Wind Tunnel, SWT
GRC-2021-C-03333
Commercial Supersonic Transport, CST Project, X-59 Sonic Boom Test Model, in the 8x6-foot Supersonic Wind Tunnel, SWT
GRC-2021-C-03350
Commercial Supersonic Transport, CST Project, X-59 Sonic Boom Test Model, in the 8x6-foot Supersonic Wind Tunnel, SWT
GRC-2021-C-03356
Commercial Supersonic Transport, CST Project, X-59 Sonic Boom Test Model, in the 8x6-foot Supersonic Wind Tunnel, SWT
GRC-2021-C-03351
Commercial Supersonic Transport, CST Project, X-59 Sonic Boom Test Model, in the 8x6-foot Supersonic Wind Tunnel, SWT
GRC-2021-C-03344
Commercial Supersonic Transport, CST Project, X-59 Sonic Boom Test Model, in the 8x6-foot Supersonic Wind Tunnel, SWT
GRC-2021-C-03346
Commercial Supersonic Transport, CST Project, X-59 Sonic Boom Test Model, in the 8x6-foot Supersonic Wind Tunnel, SWT
GRC-2021-C-03359
Commercial Supersonic Transport, CST Project, X-59 Sonic Boom Test Model, in the 8x6-foot Supersonic Wind Tunnel, SWT
GRC-2021-C-03354
The Sierra Space Plane, Dream Chaser, suspended by a crane sits just inside the overhead door of the ISP (In Space Propulsion) test facility at NASA GRC-ATF.  Once lifted and lowered into the test chamber, it will be exposed to the harsh cold conditions of space for testing in extended periods of time.
The Sierra Space Plane, Dream Chaser, is ready to be lifted into
Commercial Supersonic Transport, CST Project, X-59 Sonic Boom Test Model, in the 8x6-foot Supersonic Wind Tunnel, SWT
GRC-2021-C-03349
Commercial Supersonic Transport, CST Project, X-59 Sonic Boom Test Model, in the 8x6-foot Supersonic Wind Tunnel, SWT
GRC-2021-C-03363
Commercial Supersonic Transport, CST Project, X-59 Sonic Boom Test Model, in the 8x6-foot Supersonic Wind Tunnel, SWT
GRC-2021-C-03347
Commercial Supersonic Transport, CST Project, X-59 Sonic Boom Test Model, in the 8x6-foot Supersonic Wind Tunnel, SWT
GRC-2021-C-03343
Commercial Supersonic Transport, CST Project, X-59 Sonic Boom Test Model, in the 8x6-foot Supersonic Wind Tunnel, SWT
GRC-2021-C-03341
A Congressional Member of Congress visited Glenn research Center.  The Congressman engaged with GRC industry partners and researchers in the MIC (Mission Integration Center) Auditorium.  Pictured is GRC Center Director, James Kenyon.
GRC-2023-C-07693
Commercial Supersonic Transport, CST Project, X-59 Sonic Boom Test Model, in the 8x6-foot Supersonic Wind Tunnel, SWT
GRC-2021-C-03345
Commercial Supersonic Transport, CST Project, X-59 Sonic Boom Test Model, in the 8x6-foot Supersonic Wind Tunnel, SWT
GRC-2021-C-03364
Commercial Supersonic Transport, CST Project, X-59 Sonic Boom Test Model, in the 8x6-foot Supersonic Wind Tunnel, SWT
GRC-2021-C-03358