Super-orbital Flight Vehicle and Plasma Flow around It
Effect of Models for Transport Properties on the Hypersonic Reentry Heating Environment
Reentry Environment Advanced Diagnostics (READ) Flight Experiment on USERS Reentry Vehicle
FLUID DYNAMICS - Effective Test Time Evaluation in High-Enthalpy Expansion Tube
Suppression of light degradation of carrier lifetimes in low-resistivity CZ-Si solar cells
Rotational State-to-state Relaxation and Dissociation of Nitrogen behind a Strong Shock Wave
An Electromagnetic-wave Code for the Assessment of Plasma-plume Impact on Microwave Communication
2-D Numerical Simulation of Side Loads in Rocket Nozzles
Microwave Attenuation Measurement of Full-scale Solid Rocket Motor Plumes
Concept Study of the Flight Test for ATREX Engine Demonstration
Conceptual Study of Piggyback Atmospheric Reentry Flight Testbed (PARTT)
FLUID DYNAMICS - Numerical Investigation of High-Enthalpy Flows Generated by Expansion Tube
Experiment on inflatable decelerators towed in a supersonic flow
Plasmasphere electron temperature model based on Akebono data
Plasmasphere electron temperature model based on Akebono data
Generation of high-density plasma in the polar cap observed by the Akebono satellite
Generation of high-density plasma in the polar cap observed by the Akebono satellite
Reentry Heating Mitigation by Utilizing the Hall Effect
Development of new 2,2 liter turbocharged diesel engine for the Euro IV standards
Experimental Investigation of the Shock Layer Associated with the Super-orbital Reentry Velocity
Development of New 2.2-liter Turbocharged Diesel Engine for the EURO-IV Standards
Design of high-average-power clean EUV light source based on laser-produced Xenon plasma [5196-29]
Performance of liquid xenon jet laser-produced-plasma light source for EUV lithography [5662-58]
Compact Energetic Light Particle Detector and Spectrometer
Influence of the Hall Effect on the Electrodynamic Heat Shield System for Reentry Vehicles
Generation of high-density plasma in the polar cap observed by the Akebono satellite
CuInS2-In2S3 thin film solar cell using spray pyrolysis technique having 9.5% efficiency