PRESENT STATUS AND PROSPECTS OF JAXA'S RESEARCH ON FUTURE SPACE TRANSPORTATION SYSTEM
THE SCRAMSPACE I SCRAMJET FLIGHT EXPERIMENT DESIGN AND CONSTRUCTION
ANALYSIS OF THE ERROR IN LIQUID-FUEL RAMJET COMBUSTION EFFICIENCY CALCULATION
SIMULATION OF HIGH MACH NUMBER SCRAMJET FLOW CONDITIONS USING THE X2 EXPANSION TUBE
ANALYSIS AND CORRELATION OF FLAME STABILITY LIMITS IN SUPERSONIC FLOW WITH CAVITY FLAMEHOLDER
WATER INJECTION PRE-COMPRESSOR COOLING ASSIST SPACE ACCESS
THE THEORETICAL STUDY OF THE AERO-THERMODYNAMICS CHARACTERISTICS FOR SCRAMJET COMBUSTOR
RAPID THREE-DIMENSIONAL CONSTRAINED TRAJECTORY GENERATION FOR NEAR SPACE HYPERSONIC VEHICLES
THERMAL PROTECTION AND HYDROGEN PRODUCTION ON BOARD OF THE HYPERSONIC VEHICLE
LARGE-EDDY SIMULATION OF PSEUDO-SHOCK WAVE IN A SQUARE DUCT
ASCENT TRAJECTORY OPTIMISATION FOR A SINGLE-STAGE-TO-ORBIT VEHICLE WITH HYBRID PROPULSION
MULTI-OBJECTIVE OPTIMIZATION OF HYPERSONIC VEHICLES UNDER ASYMMETRIC BOUNDARY-LAYER CONDITIONS
VALIDATION OF PIV MEASUREMENTS USING SUPERSONIC TURBULENT BOUNDARY LAYER
TOWARDS ROBUST AERO-THERMODYNAMIC PREDICTIONS FOR RE-USABLE SINGLE-STAGE TO ORBIT VEHICLES
AERODYNAMIC HEATING RATE EVALUATION OF MACH 5 HYPERSONIC AIRPLANES
RESEARCHES ON HEAT TRANSFER CORRELATIONS OF HYDROCARBON FUEL UNDER SUPERCRITICAL PRESSURE