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
This mid-afternoon, 360-degree panorama was acquired by the Mast Camera (Mastcam) on NASA’s Curiosity Mars rover on April 4, 2016,…
Jet Exit Rig Balance: A flow-through force balance used to measure aerodynamic or propulsive forces/moments at NASA’s Glenn Research Center.
Jet Exit Rig Balance: A flow-through force balance used to measure aerodynamic or propulsive forces/moments at NASA’s Glenn Research Center.