RTEX: Reentry Technology Experimental of Express Capsule
Experimental Study of Supersonic Parachute and Reentry Capsule
On the flight verification of the hyperbolic re-entry capsule via the sounding rocket
A Concept of Reusable Sounding Rocket with Enhanced Maneuverability and Operability
Measurement of No Rotational and Vibrational Temperatures in Arc Heated Air Flow by LIF Spectroscopy
Prediction of Aerodynamic Characteristics of M-V Launch Vehicle
Measurement of 2-Dimentional Velocity Distribution of Arc-Heated Flow by Cu-LIF
Throttling Dynamic Response of LH2 Rocket Engine for Vertical Landing Rocket Vehicle
Flight Testing and Turnaroud Lessons of Reusable Rocket Vehicle
Effect of the Internal Gas Pressure on the Ablator Performance
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 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)
Aerodynamic Characteristics and Thermal Protections for Vertical Landing Rocket Vehicle
Onboard Reentry Flight Measurement of DASH Capsule and Analysis of Thermal Protection System
R & D Status and Future Plan of the Japanese Reusable Launch System