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)

12:20 PM - 12:40 PM

[2022-o-1-21] Evaluation of Heat Transfer Characteristics of Liquid Oxygen Flow in a Thin Tube under High Heat Flux Conditions

*Koki Kitagawa1, Kohei Matsui1 (1. Kyushu Institute of Technology, Department of Space Systems Engineering)

Keywords:Hybrid rocket, Regenerative cooling nozzle, Joule heating, Two phase flow

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