33rd International Symposium on Space Technology and Science, 10th Nano-Satellite Symposium & 14th IAA Low-Cost Planetary Missions Conference

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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)

4:00 PM - 4:20 PM

[2022-o-1-07] Numerical Estimation of Discharge Coefficient of Nitrous Oxide Flow inside an Injector for Hybrid Rocket Engine

*Rikio Watanabe1, Yoshiki Shimizu1, Kazuki Yasuda2, Daisuke Nakata2 (1. Tokyo City University, Department of Mech. Sys. Engr., 2. Muroran Institute of Technology, Aerospace Plane Research Center)

Keywords:Hybrid Rocket, Oxidizer, Nitrous Oxide, Discharge Coefficient

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