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 〜

[OS1-3] 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)

9:40 AM - 10:00 AM

[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)

Keywords:Hybrid rocket, Low melting point fuel, Swirling oxidizer, High regression rate

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