Solar Thermal Thrusters Made of Single Crystal Refractory Metals
6-3 Improvements of Accelerometer Force Measurement Technique
Free-flight Tests of Reentry Capsule Models in Free-piston Shock Tunnel
Free-Flight Aerodynamic Test with Projectile-Onboard Data Recorder in a Ballistic Range
Effect of Wall Catalycity on Aerodynamic Heating of Flat Plates in a High Enthalpy Shock Tunnel
Single Crystal Mo Solar Thermal Thruster for Microsatellites
Single crystal Mo solar thermal thruster for microsatellites
Aerodynamic Testing with Accelerometers in the High Enthalpy Shock Tunnel HIEST
STUDY ON AERODYNAMIC CHARACTERISTICS OF A HIGH ENTHALPY FLOW AROUND BLUNT-NOSED BODY
Heat Flux Measurement of Apollo Capsule Model in the Free-Piston Shock Tunnel HIEST
AEROHEATING MEASUREMENT OF A RE-ENTRY CAPSULE MODEL IN FREE-PISTON SHOCK TUNNEL HIEST
Improvement of Scramjet Combustor Performance at Hypervelocity Condition over Mach 10 Flight
MEASUREMENT OF HYPERSONIC HIGH-ENTHALPY BOUNDARY LAYER TRANSITION ON 7^o CONE MODEL
Free-flight Force Measurement Technique in Shock Tunnel
5-2 Experimental Investigations of the Flow Field around a Generic Re-entry Capsule in HIEST
Influence of Thermal Non-Equilibrium on Nozzle Flow Condition of High Enthalpy Shock Tunnel HIEST
Flow Characterization of High Enthalpy Shock Tunnel Based on Shock Stand-Off Distance
JSUS Solar Thermal Thruster and Its Integration with Thermionic Power Converter