FULL-LENGTH PAPERS - Concept and Preliminary Flight Testing of a Fully Reusable Rocket Vehicle
Toward a Piloted, Sub-Orbital, VTOL Demonstrator: Test-Flights 1999 - 2001
Flight Testing and Turnaroud Lessons of Reusable Rocket Vehicle
Technical Demonstrations for Reusable Sounding Rocket System (AAS 12-580)
Flight Demonstration and a Concept for the Readiness of Fully Reusable Rocket Vehicles (AAS 01-545)
Flight Demonstration and a Concept for the Readiness of Fully Reusable Rocket Vehicles (AAS 01-545)
RTEX: Reentry Technology Experimental of Express Capsule
Aerodynamic Characteristics and Thermal Protections for Vertical Landing Rocket Vehicle
Onboard Reentry Flight Measurement of DASH Capsule and Analysis of Thermal Protection System
Effect of the Internal Gas Pressure on the Ablator Performance
MHD Analysis of Magnetosphere around Magneto Plasma Sail
Measurement of No Rotational and Vibrational Temperatures in Arc Heated Air Flow by LIF Spectroscopy
A Concept of Reusable Sounding Rocket with Enhanced Maneuverability and Operability
System Design and Technical Demonstrations for Reusable Sounding Rocket
Experimental Study on Effects of Fuselage Configurations for RLV on Aerodynamic Characteristics
Experimental Study on Effects of Fuselage Configurations for RLV on Aerodynamic Characteristics
Multi Objective Optimization of a Synthetic Jet Acting on a Separated Flow Over a Hump
Aerodynamic Studies on Vertical Landing of Reusable Rocket Vehicle
Prediction of Aerodynamic Characteristics of M-V Launch Vehicle
Experimental Study of Supersonic Parachute and Reentry Capsule
Post-Flight Analysis of Hayabusa; Asteroid Sample Return Capsule (AAS 12-579)
Measurement of 2-Dimentional Velocity Distribution of Arc-Heated Flow by Cu-LIF
Inductively-coupled High Enthalpy Flow Generator for Planetary Entry Probes
Computations of Opposing Jet from Vertical Landing Rocket Vehicle
Aerodynamics of Vertical Landing Rocket Vehicle in Landing Phase (AAS 03-438)
A Concept and Its Aerodynamic Design of a Sub-Orbital Reusable Rocket
MHD Analysis of Flow Fields Around Magneto Plasma Sail AIAA Paper
Numerical Analysis of Shock Wave with Precursor Heating AIAA Paper
R & D Status and Future Plan of the Japanese Reusable Launch System
Sounding rockets and ballooning activities of Japan in 2001 and 2002
Throttling Dynamic Response of LH2 Rocket Engine for Vertical Landing Rocket Vehicle
Thermal Response of Ablative Test Piece in Arc-Heated Wind Tunnel
Aerodynamics of Vertical Landing Rocket Vehicle with Engine Thrust in Landing Phase (AIAA 2006-0256)
Numerical and Experimental Investigation on Sloshing in Rocket Tanks with Damping Devices AIAA Paper
Dynamic Behavior of Liquid Propellant in Reusable Rocket Vehicle
A Lightweight Heat Shield System using a Phenol CFRP Material
Development of USERS/REM Heat Shield System and its Evaluation after Re-entry
Development and flight test of metal-lined CFRP cryogenic tank for reusable rocket