[M-3] Flight Demonstraion of Detonation Engine

[2022-m-12] In-Space Flight Demonstration Results of a Detonation Engine System on Sounding Rocket S-520-31: Rotating Detonation Engine

*Keisuke Goto¹, Koichi Matsuyama¹, Ken Matsuoka², Akira Kawasaki², Hiroaki Watanabe², Noboru Itouyama¹, Kazuki Ishihara², Valentin Buyakofu², Tomoyuki Noda², Jiro Kasahara², Akiko Matsuo³, Ikkoh Funaki⁴, Daisuke Nakata⁵, Masaharu Uchiumi⁵, Hiroto Habu⁴, Shinsuke Takeuchi⁴, Satoshi Arakawa⁴, Junichi Masuda⁴, Kenji Maehara⁴, Tatsuro Nakao⁶, Kazuhiko Yamada⁴ (1. Nagoya Univ. Institute of Materials and Systems for Sustainability, 2. Nagoya Univ. Department of Aerospace Engineering, 3. Keio Univ. Department of Mechanical Engineering, 4. Japan Aerospace Exploration Agency, Institute of Space and Astronautical Science, 5. Muroran Institute of Technology, Aerospace Plane Research Center, 6. Japan Aerospace Exploration Agency, Unit I, Research and Development Directorate)

キーワード：Detonation Engine, Sounding Rocket, Engineering Demonstration