Faculty of System Design, Tokyo Metropolitan University
Graduate School of System Design, Tokyo Metropolitan University
Graduate School of System Design, Tokyo Metropolitan University
Graduate School of System Design, Tokyo Metropolitan University
Graduate School of System Design, Tokyo Metropolitan University
Graduate School of System Design, Tokyo Metropolitan University
出版者
宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)
出版者（英）
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)
雑誌名
平成24年度宇宙輸送シンポジウム: 講演集録
雑誌名(英)
Proceedings of Space Transportation Symposium: FY2012
Space Transportation FY2012 (January 17-18, 2013. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan
抄録（英）
Discharge plasma is proposed as a reaction initiation system for green monopropellants, especially for hydroxylammonium nitrate (HAN) based liquid monopropellant. This reaction initiation system has been researched as substitution of conventional catalytic decomposition system. In this study, laboratory model (LM) of the reaction initiation system were designed and built. The fundamental characteristics were investigated experimentally, based on the effects of frequency and helium mass flow rate on power consumptions. 25 W of power consumption were achieved at 5000 Hz of frequency and 0.02 g/s of helium mass flow rate.
放電プラズマを用いたグリーンプロペラントの反応誘起機構の試作
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