Paper information
- Paper code
- Order
34
- Room
IP Area
- Title
The Effect of fuel length on the regression rate in swirling-oxidizer-flow-type hybrid rocket using a liquefying fuel
- abstract
- Session
IP. Interactive Presentations - IAF SPACE PROPULSION SYMPOSIUM
- symposium
C4. IAF SPACE PROPULSION SYMPOSIUM
- congress
IAC-19
- Type of presentation
interactive
Mr. Yo Kawabata, Chiba Institute of Technology, Japan
Mr. Kazunari Onagano, Chiba Institute of Technology, Japan;
Dr. Yutaka Wada, Chiba Institute of Technology, Japan;
Mr. Nobuji Kato, Katazen Corporation, Japan;
Prof. Keiichi Hori, Japan Aerospace Exploration Agency (JAXA), Japan;
Prof. Ryo Nagase, Chiba Institute of Technology, Japan;