Evaluation Tests of Thermal Shock Test Facility for Reusable Rocket Engine Materials
LE-7A Engine Nozzle Separation Phenomenon during the Transient Process
Evaluation of Weight Reduction of LE-5B for Reusable Rocket Engine
Effects of Fluids and Systems on Rotor Vibration of LE-7A Oxygen Turbopump
Development of waterbome white conductive primer for bumper (First Report)
Smart Distributed Minimization of the Volume of Discrete Structures
Onboard Autonomous Path Planning for a Planetary Exploration Rover (AIAA 2013-4825)
Experiments of a Space Robot in the Free-Fall Environment
Influence of a Gap for Film Cooling in Rocket Engine Nozzles on Transient Flow Characteristics
The ONERA RESSAC Unmanned Helicopter : Towards a Safe Autonomous Operation in an Urban Environment
Design of NAL New High Enthalpy Wind Tunnel Heated by Inductively Coupled Plasma
Spectral and Heating Characteristics in the Arc Column of the 0.75MW Arc-Heated Wind Tunnel
Saving Power by Demand Capacity Controlled Compressor