[M-3] Flight Demonstraion of Detonation Engine

[2022-m-11] In-Space Flight Demonstration Results of a Detonation Engine System on Sounding Rocket S-520-31: Flight Path and Attitude

*Hiroaki Watanabe¹, Koichi Matsuyama¹, Ken Matsuoka¹, Akira Kawasaki¹, Noboru Itouyama¹, Keisuke Goto¹, Kazuki Ishihara¹, Valentin Buyakofu¹, Tomoyuki Noda¹, Shiro Ito¹, Jiro Kasahara¹, Akiko Matsuo², Ikkoh Funaki³, Daisuke Nakata⁴, Masaharu Uchiumi⁴, Hiroto Habu³, Shinsuke Takeuchi³, Satoshi Arakawa³, Junichi Masuda³, Kenzi Maehara³, Tatsuro Nakao⁵, Kazuhiko Yamada³ (1. Nagoya University, Department of Aerospace Engineering, 2. Keio University, Department of Mechanical Engineering, 3. Japan Aerospace Exploration Agency, Institute of Space and Astronautical Science, 4. Muroran Institute of Technology, Aerospace Plane Research Center, 5. Japan Aerospace Exploration Agency)

Keywords:Detonation Engine, Sousing Rocket, Engineering Demonstration