Experimental Study on Effect of Swirling Oxidizer Flow on Average and Local Regression Rate of Low-Melting-Point Thermoplastic Fuel for Hybrid Rockets

Yo Kawabata

講演情報

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

2022年3月4日(金) 09:00 〜 10:40 Meeting Room4 (BF1)

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

09:40 〜 10:00

[2022-o-1-14] Experimental Study on Effect of Swirling Oxidizer Flow on Average and Local Regression Rate of Low-Melting-Point Thermoplastic Fuel for Hybrid Rockets

*Yo Kawabata¹, Yutaka Wada², Nobuji Kato³, Keiichi Hori⁴ (1. Fukuoka Univ. Department of Mechanical Engineering, 2. Chiba Institute of Technology, Department of Innovative Mechanical and Electronic Engineering, 3. Katazen Corporation, 4. JAXA)

キーワード：Hybrid rocket, Low melting point fuel, Swirling oxidizer, High regression rate

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