[A-8] Solid Rocket & Detonation Engine

[2022-a-35] Thrust Performance of Rotating Detonation Engines Using a Methane-Oxygen Mixture

*Kazuma Kawasaki¹, Haruhiro Kawana¹, Kanta Ohno¹, Kazuhiro Ishii¹, Makoto Kojima², Hideto Kawashima² (1. Yokohama National Univ. Department of Mechanical Engineering , 2. JAXA)

キーワード：Detonation wave, Rotating detonation engine, Thrust measurement