The Facility Aerodynamics Validation and Operational Research (FAVOR) model, mounted in the Glenn Research Center 8- by 6-Foot Supersonic Wind…
FAVOR Model and Team
The Facility Aerodynamics Validation and Operational Research (FAVOR) model, mounted in the Ames Research Center 11- by 11-Foot Unitary Plan…
Photogrammetry testing of the Tension Cone Inflatable Aerodynamic Decelerator at NASA's Langley Reseach Center Transonic Dynamics Tunnel.
Photogrammetry of the Supersonic Parachute used to land the Mars Curiosity Rover, tested in NASA's Glenn Research Center 10- by…
These four galaxy clusters were part of a large survey of over 300 clusters used to investigate dark energy, the…
Liquid Hydrogen Tanker Flex Hose Fit Check at Launch Pad 39B
Schlieren image of the Large-Scale Low-Boom (LSLB) Inlet in the 8- by 6-Foot Supersonic Wind Tunnel at NASA’s Glenn Research…
Test section of the 9- by 7-foot Unitary Plan Supersonic Wind Tunnel at NASA's Ames Research Center, set up to…
Polystyrene Particles (PSL’s) being developed at NASA’s Langley Research Center for improved Particle Image Velocimetry Measurements