Kakuda Space Center, Japan Aerospace Exploration Agency (JAXA)(KSPC)
Kakuda Space Center, Japan Aerospace Exploration Agency (JAXA)(KSPC)
Kakuda Space Center, Japan Aerospace Exploration Agency (JAXA)(KSPC)
Kakuda Space Center, Japan Aerospace Exploration Agency (JAXA)(KSPC)
Kakuda Space Center, Japan Aerospace Exploration Agency (JAXA)(KSPC)
Kakuda Space Center, Japan Aerospace Exploration Agency (JAXA)(KSPC)
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）
System analysis upon a TSTO launch vehicle equipping a Rocket-Based Combined Cycle Engine was conducted, to evaluate the benefits of hypersonic air-breathing technology upon the performance of the launch vehicle. Upon the results of aerodynamic performance prediction, structure analysis as well as the supply system analysis was conducted. Though a high Isp performance of the engine system was predicted, the resulting payload capability of the launch system was found to depend highly on the airframe weight including the engine weight, and ranged from less than 1% to 4% of the take-off weight. The analysis method and primary results are herein reported
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
RBCC エンジンのシステム解析の現状について
