Aero-Thermodynamic Flight Environment of "HITEN" Spacecraft at the Aerobrake Experiment
Application of nearfield acoustic holography for evaluating the design of engine cover
Application of Nearfield Acoustic Holography for Evaluating the Design of Engine Cover
Application of the Magnetic Flow Control System for Aerobraking Flight of the Re-entry Vehicle
Compact Energetic Light Particle Detector and Spectrometer
Design of high-average-power clean EUV light source based on laser-produced Xenon plasma [5196-29]
Experiment on inflatable decelerators towed in a supersonic flow
Influence of the Hall Effect on the Electrodynamic Heat Shield System for Reentry Vehicles
Magnetospheric Electron Temperature Obtained by AKEBONO Satellite
On factors of noise emitted by a small vehicle and noise level simulation of pass-by test
Performance of liquid xenon jet laser-produced-plasma light source for EUV lithography [5662-58]
RADIO FREQUENCY BLACKOUT POSSIBILITY FOR AN INFLATABLE REENTRY VEHICLE
Reentry Heating Mitigation by Utilizing the Hall Effect
Space Demonstration of Bare Electrodynamic Tape-Tether Technology on the Sounding Rocket S520-25
Super-orbital Flight Vehicle and Plasma Flow around It
The Ford Motor Company Spin-Torsional NVH Test Facility