Yokohama National University
Yokohama National University
Yokohama National University
Fukuoka University
Department of Space Flight Systems, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)
Yokohama National University
出版者
宇宙航空研究開発機構(JAXA)
出版者（英）
Japan Aerospace Exploration Agency (JAXA)
雑誌名
宇宙航空研究開発機構研究開発報告: 高エネルギー物質研究会: 平成28年度研究成果報告書
雑誌名(英)
JAXA Research and Development Report: Technical Report of The Research Activity for High Energy Materials (2016)
Ammonium dinitramide based ionic liquid propellants have been studied as monopropellant in terms of high specific impulse, low melting point and low toxicity. The purpose of this study is construction prediction method of ignition delay and combustion temperature against heating rate of propellants for establishment of combustion control technique. The prediction method of ignition delay and combustion temperature is constructed by combination of thermal analysis method and combustion simulation. From the result of prediction, ignition delay is 0.5-4.5 s and combustion temperature is around 2000 C in the case of heating rate is 50-600 Ks(exp -1).
内容記述
形態: カラー図版あり
内容記述（英）
Physical characteristics: Original contains color illustrations
熱特性解析によるアンモニウムジニトラミド系イオン液体の着火遅れ時間予測
AA1630043005.pdf
(2.04MB)
