A Study on Hybrid Rocket Engine with Multi-Section Swirl Injection Method and Aft Counter-Swirl Injection Method under Acceleration Conditions for Space Launch

講演情報

Oral Session

a) Chemical Propulsion and Air-breathing Engines

2023年6月8日(木) 09:00 〜 10:40 The large Meeting Room 1 5F (The large Meeting Room 1 5F)

Takashi Sakurai (Tokyo Metropolitan University),Yo Kawabata (Fukuoka University)

09:40 〜 10:00

*Rikiya Mifune¹, Shigeru Aso¹, Ryutaro Sakamoto¹, Masayuki Katayama¹ (1. Kurume Institute of Technology)

キーワード：Hybrid rocket, Acceleration condition, Swirl flow, Space launch