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 〜

[OS1-4] Oxidizer flow and tank

Fri. Mar 4, 2022 11:00 AM - 12:40 PM Meeting Room4 (BF1)

Chair:Toru Shimada(JAXA), Kenichi Takahashi(Nihon University)

12:00 PM - 12:20 PM

[2022-o-1-20] Thrust Response of Hybrid Rocket Engine with Pressure Drop in Oxidizer Tank

*Donghoon Chae1, Changjin Lee1 (1. Department of Aerospace Engineering, Konkuk University)

Keywords:Thrust Response, Tank Pressure Drop, Hybrid Rocket Engine (HRE), VTVL

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