Paper information

Paper code

IAC-20,C4,4,6,x58747

Order

6

Title

Experimental and Numerical Study on Feasibility of 5kN Thrust Level Hybrid Rocket Motor using the Low-Melting-Point Thermoplastic Fuel

abstract

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Session

4. Solid and Hybrid Propulsion (2)

symposium

C4. IAF SPACE PROPULSION SYMPOSIUM

congress

IAC-20

Type of presentation

oral

Main author

Dr. Yo Kawabata, Japan

Co-authors

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;