Prediction of Aerodynamic Characteristics of M-V Launch Vehicle
Experimental Study of Supersonic Parachute and Reentry Capsule
On the flight verification of the hyperbolic re-entry capsule via the sounding rocket
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)
Experimental Study on Effects of Fuselage Configurations for RLV on Aerodynamic Characteristics
Numerical and Experimental Investigation on Sloshing in Rocket Tanks with Damping Devices AIAA Paper
Dynamic Behavior of Liquid Propellant in Reusable Rocket Vehicle