The University of Tokyo
Department of Space Flight Systems, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)
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)
ADN-based three-component non-solvent ionic liquid has good characteristics, low toxicity and high stability, and is suitable to apply for liquid propellant. On the one hand, its flame temperature is too high. In the case of contact-ignition, for example heater or catalyst, it is easy to break the engine system. From these reason, we focused on the laser ignition. It can achieve high energy density and non-contact energy input. In this study, we evaluated the possibility of combination ADN-based ionic liquid propellant and Laser ignition. As the result, it was found that propellant became gas compound from droplet with pulse laser.
内容記述
形態: カラー図版あり
内容記述(英)
Physical characteristics: Original contains color illustrations