Tohoku University
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）
Aerodynamic tests of small scale rocket combined cycle engine models were carried out to evaluate their performance and at rocket mode operation. In the experiment, thrust force of four models was measured on condition that environmental pressure was set up 4 kPa, rocket chamber pressure ranged up to 3MPa. Nitrogen gas was exhausted as the substitution for the actual rocket gas. As a result, thrust force of four models differentiated and thrust force of rocket combined cycle engine was lower than that of calculated value of conical rocket nozzle. Flow structures of rocket combined cycle engine nozzle were investigated to discuss the performance variation.
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エンジンのノズル特性について
