Paper information
- Paper code
- Order
6
- Title
Experimental and Numerical Study on Feasibility of 5kN Thrust Level Hybrid Rocket Motor using the Low-Melting-Point Thermoplastic Fuel
- abstract
- Session
4. Solid and Hybrid Propulsion (2)
- symposium
C4. IAF SPACE PROPULSION SYMPOSIUM
- congress
IAC-20
- Type of presentation
oral
Dr. Yo Kawabata, Japan
Mr. Masaya Kimura, Chiba Institute of Technology, Japan;
Dr. Yutaka Wada, Chiba Institute of Technology, Japan;
Prof. Ryo Nagase, Chiba Institute of Technology, Japan;
Dr. Takeshi Yasuda, Tokyo Metropolitan Institute of Technology, Japan;
Mr. Nobuji Kato, Katazen Corporation, Japan;
Prof. Keiichi Hori, Japan Aerospace Exploration Agency (JAXA), Japan;
Prof. takafumi matsui, Chiba Institute of Technology, Japan;