Muroran Institute of Technology
Muroran Institute of Technology
Muroran Institute of Technology
Muroran Institute of Technology
Muroran Institute of Technology
出版者
宇宙航空研究開発機構宇宙科学研究所
出版者（英）
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)
雑誌名
平成22年度宇宙輸送シンポジウム: 講演集録
雑誌名(英)
Proceedings of Space Transportation Symposium: FY2010
Space Transportation FY2010 (January 20-21, 2011. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency(JAXA)(ISAS)), Sagamihara, Kanagawa Japan
抄録（英）
With the aims of creating and validating innovative fundamental technologies for high-speed atmospheric flights, a small scale supersonic experimental vehicle is designed as a flying test bed. Several aerodynamic configurations were proposed and analyzed by wind-tunnel tests. A twin-engine configuration was selected as the baseline. Its flight capability was predicted by mass point analysis on the basis of aerodynamic characterization and performance estimation of the turbojet engine to be installed. In addition, a prototype vehicle with the equivalent configuration and dimension is designed and fabricated for verification of subsonic flight characteristics. Its first flight test was carried out in August 2010 and good flight capability was demonstrated.
内容記述
形態: カラー図版あり
形態: CD-ROM1枚
内容記述（英）
Physical characteristics: Original contains color illustrations
Note: One CD-ROM
フライングテストベッドとしての小型超音速飛行実験機の設計およびプロトタイプの試作と試験飛行
