[A-5] Liquid Rocket 1

[2022-a-19] Thermal Behavior of Eutectic Mixture of Ammonium Dinitramide and Hydrazide Compounds

*Hiroki Matsunaga¹, Mamoru Hayata², Hiroto Habu³, Masaru Noda¹, Atsumi Miyake⁴ (1. Fukuoka Univ. Department of Chemical Engineering, 2. Carlit Holdings Co., Ltd, 3. JAXA/ISAS. Division of Space Flight Systems, 4. Yokohama National Univ. Graduate School of Environment and Information Sciences)

Keywords:Energetic ionic liquid, Ammonium dinitramide, Liquid rocket propellant, Ignition