Control Methods for Electrically Driven Pump-Fed Hybrid Rocket Motor

Tadayoshi Shoyama

Presentation information

Oral Session

OS-1) Hybrid Rocket 〜 Essentially Non-Explosive Propulsion for Future Fail-Safe Space Transportation Systems 〜

[OS1-1] Development and experiment of engine 1

Thu. Mar 3, 2022 11:00 AM - 12:20 PM Meeting Room4 (BF1)

Chair:Harunori Nagata(Hokkaido University), Koki Kitagawa(Kyushu Institute of Technology)

11:00 AM - 11:20 AM

[2022-o-1-01] Control Methods for Electrically Driven Pump-Fed Hybrid Rocket Motor

*Tadayoshi Shoyama¹, Masaya Kimura¹,Shuichi Tanabe¹, Yutaka Wada¹, Takafumi Matsui¹ (1. Chiba Institute of Technology, Planetary Exploration Research Center)

Keywords:Hybrid Rocket, Turbopump, Thrust Pattern, O/F Shift, Burning Rate

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