[a-10] Liquid Rocket 2

[2023-a-41] Modeling of Shutdown Transient State for Space Propulsion System Simulation

*Yu Daimon¹, Kohji Tominaga¹, Go Fujii¹, Taiichi Nagata¹, Yoshiki Matsuura², Yasuhito Kano², Erika Uchiyama² (1. Japan Aerospace Exploration Agency, 2. IHI AEROSPACE Co., Ltd.)

キーワード：Space propulsion system, Thruster, Visualization study of combustion test, CFD