Unsteady Heat Transfer Analysis and Experimental Evaluation of LOX Regenerative-cooling Nozzle for SOFT Hybrid Rocket Engines

Presentation information

Oral Session

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

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

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

11:00 AM - 11:20 AM

*Hitomi Ozaki¹, Kodai Kurachi¹, Takashi Sakurai¹ (1. Tokyo Metropolitan University)

Keywords:LOX Regenerative-cooling Nozzle, Heat transfer analysis, Hybrid Rocket Engine

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