Postflight Thermal Protection System Analysis of Hayabusa Reentry Capsule
Technical Demonstrations for Reusable Sounding Rocket System (AAS 12-580)
Multi Objective Optimization of a Synthetic Jet Acting on a Separated Flow Over a Hump
Post-Flight Analysis of Hayabusa; Asteroid Sample Return Capsule (AAS 12-579)
System Design and Technical Demonstrations for Reusable Sounding Rocket
Discussion on Momentum Transfer Difficulty of a Magnetoplasma Sail
MHD Analysis of Flow Fields Around Magneto Plasma Sail AIAA Paper
Numerical Analysis of Shock Wave with Precursor Heating AIAA Paper
Numerical and Experimental Investigation on Sloshing in Rocket Tanks with Damping Devices AIAA Paper
MHD Analysis of Magnetosphere around Magneto Plasma Sail
Aerodynamic Studies on Vertical Landing of Reusable Rocket Vehicle
Computations of Opposing Jet from Vertical Landing Rocket Vehicle
Aerodynamics of Vertical Landing Rocket Vehicle with Engine Thrust in Landing Phase (AIAA 2006-0256)
Development and flight test of metal-lined CFRP cryogenic tank for reusable 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
Inductively-coupled High Enthalpy Flow Generator for Planetary Entry Probes
Aerodynamics of Vertical Landing Rocket Vehicle in Landing Phase (AAS 03-438)