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

Presentation information

Oral Session

a) Chemical Propulsion and Air-breathing Engines

Thu. Jun 8, 2023 9:00 AM - 10:40 AM The large Meeting Room 1 5F (The large Meeting Room 1 5F)

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

9:40 AM - 10:00 AM

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

Keywords:Hybrid rocket, Acceleration condition, Swirl flow, Space launch