Modeling of Hybrid Rocket Combustion Using Variable Wall Temperature Model

Takakazu Morita

Presentation information

Oral Session

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

[OS1-2] Numerical model and combustion instability

Thu. Mar 3, 2022 4:00 PM - 5:40 PM Meeting Room4 (BF1)

Chair:Ichiro Nakagawa(Tokai University), Yo Kawabata(Fukuoka University)

5:00 PM - 5:20 PM

[2022-o-1-11] Modeling of Hybrid Rocket Combustion Using Variable Wall Temperature Model

*Takakazu Morita¹, Yansheng Yang², Jungpyo Lee³ (1. Tokai Univ. Department of Aeronautics and Astronautics, 2. Tokai Univ. Graduate School of Engineering , 3. Univ. of Brasília)

Keywords:Hybrid Rocket, Combustion, Fuel Regression Rate

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