A Study on Hybrid Rocket Engine with Multi-Section Swirl Injection Method and Counter-Swirl Injection Method with Application to Fully Reusable Launch Vehicles

Shigeru Aso

講演情報

Oral Session

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

[OS1-1] Development and experiment of engine 1

2022年3月3日(木) 11:00 〜 12:20 Meeting Room4 (BF1)

Chair:Harunori Nagata(Hokkaido University), Koki Kitagawa(Kyushu Institute of Technology)

11:40 〜 12:00

[2022-o-1-03] A Study on Hybrid Rocket Engine with Multi-Section Swirl Injection Method and Counter-Swirl Injection Method with Application to Fully Reusable Launch Vehicles

*Shigeru Aso¹, Ryutaro Sakamoto¹, Seiya Hodokami¹, Rikiya Mifune¹, Masayuki Katayama¹ (1. Kurume Institute of Technology Department of Traffic & Mechanical Engineering)

キーワード：hybrid rocket, swirl flow, combustion

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