[A-6] Liquid Rocket 2

[2022-a-23] Research on Bi-propellant Mode Operation of Microsatellite-Friendly Multi-Purpose PROPulsion System (MFMP-PROP)

*Ryusei Hayatomo¹, Kazuki Hirayama¹, Hiroyoshi Yasuhira¹, Haruki Sashida¹, Kohdai Ono¹, Takuto Iijima¹, Hironori Sahara¹, Yuya Ikeda², Takeru Yuzawa², Toshiaki Iizuka², Suzuki Daisuke³ (1. Tokyo Metropolitan university, 2. National Institute of Technology, Oyama College, 3. ALE Co., Ltd)

キーワード：Low-Toxic Propulsion System, Hydrogen Peroxide, Bi-Propellant, Microsatellite