[A-8] Solid Rocket & Detonation Engine

[2022-a-32] Development and Flight Test of Small Solid Rocket Motor Using Glycidyl Azide Polymer/Ammonium Perchlorate Propellant

*Kazuki Nagao¹, Tamiaki Takasago¹, Masaya Fujita², Yutaka Wada², Kaiichi Baba³, Tatsuya Oda³, Katsuya Hasegawa⁴, Keiichi Hori⁴ (1. Graduate School of Chiba Institute of Technology, Japan, 2. Chiba Institute of Technology, Japan, 3. NOF CORPORATION, Japan, 4. JAXA, Japan)

キーワード：Solid rocket motor, High-energy materials, Flight test, GAP