Nagaoka University of Technology
Nagaoka University of Technology
Nagaoka University of Technology
Nagaoka University of Technology
Nagaoka University of Technology
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: 令和2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 (2020)
In recent years, energetic ionic liquid based ammonium dinitramide (ADN) is drawing attention as green monopropellant alternate of hydrazine. Energetic ionic liquid is promising new monopropellant because it has high density, high specific impulse, and low toxicity. However, it is difficult to atomize due to its high viscosity. Therefore, it has ignition and combustion characteristics issue and not in practical use. In this study, we tried adding an additive to decrease viscosity of ADN-based energetic ionic liquid to improve its atomization characteristics. Viscosity measurement and chemical calculation by NASA CEA were performed to find suitable additive material for ADN-based green propellant. As a result, it is found that 20 wt% of methanol is suitable for additive because of viscosity, atomization characteristics, and exhaust characteristics velocity.
内容記述
形態: カラー図版あり
内容記述(英)
Physical characteristics: Original contains color illustrations