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