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THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES | 論文
- 発振回路を用いた新型ひずみセンサーの開発
- A Study on Combustion Efficiency Improvement of Low Melting Temperature Thermoplastics as a Hybrid Rocket Fuel
- Initial Operation and Deployment Experiment of Inflatable Extension Mast in SIMPLE on JEM Exposure Platform in ISS
- Experimental Study on Hypersonic Aerodynamic Characteristics of Parachutes for the Suborbital Plane
- Breakdown Phenomena in SD Cards Exposed to Proton Irradiation
- Morphable Beam Device and Beam Shape Generation Algorithm
- Multidisciplinary Design Optimization of Long or Short Range Hypersonic Aircraft
- Influence of Detonation Cell Size on Propagation of Cylindrical Detonation Wave
- Development and Flight Demonstration of 5 kN Thrust Class CAMUI Type Hybrid Rocket
- Dynamically Distributed Genetic Algorithm and Its Application to Diversely Selectable Trajectory Optimization of Winged Rockets
- Investigation of Plasma Characteristics and Ion Beam Extraction for a Micro RF Ion Thruster
- Thermal Condition of ASTRO-H under Air-cooled Environment before Launch
- Attitude and Rate Estimation of a Spacecraft by Using Magnetometers
- 構造物のある地面近傍でホバリングするヘリコプタロータの空力性能に対する横風の影響
- Iterative Learning Identification with Reducing Non-Zero Initial States and Application to Estimation of Aerodynamic Derivatives
- Ka-band High-speed Communication Systems on Small Satellites for Future Advanced Communication Networks and Earth Observations
- Japanese Contribution for Mid-Latitude Long Duration Balloon Flights
- Flow Characteristics of Plasma Wind Tunnel Using Magnetic Nozzle
- Generalized System of Mono- and Bi-Propellant Propulsion for Microsatellite
- Robust Control of Spacecraft with Mobile Appendages