Design and Investigation of High-Expansion-Ratio Bell Nozzle for Hybrid Kick Motor

Yamato Itoigawa

Presentation information

Oral Session

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

[OS1-3] Development and experiment of engine 2

Fri. Mar 4, 2022 9:00 AM - 10:40 AM Meeting Room4 (BF1)

Chair:Shigeru Aso(Kurume Institute of Technology), Daisuke Nakata(Muroran Institute of Technology)

9:20 AM - 9:40 AM

[2022-o-1-13] Design and Investigation of High-Expansion-Ratio Bell Nozzle for Hybrid Kick Motor

*Yamato Itoigawa¹, Shota Hirai², Landon Kamps², Harunori Nagata² (1. Hokkaido Univ. Department of Mechanical and Intelligent System Engineering, 2. Hokkaido Univ. Faculty of Engineering)

Keywords:Bell shaped nozzle, Hybrid rocket, Vacuum

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