@inproceedings{oai:jaxa.repo.nii.ac.jp:00016217,
 author = {河端, 駿典 and 飯塚, 俊明 and 進藤, 崇央 and 佐藤, 雄太 and 青柳, 潤一郎 and 竹ヶ原, 春貴 and Kawabata, Shunsuke and Iizuka, Toshiaki and Shindo, Takahiro and Sato, Yuta and Aoyagi, Junichiro and Takegahara, Haruki},
 book = {平成24年度宇宙輸送シンポジウム: 講演集録, Proceedings of Space Transportation Symposium: FY2012},
 month = {Jan},
 note = {平成24年度宇宙輸送シンポジウム (2013年1月17日-1月18日. 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)), 相模原市, 神奈川県, Space Transportation FY2012 (January 17-18, 2013. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan, 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., 形態: PDF, Physical characteristics: PDF, 資料番号: AA0061856081, レポート番号: STCP-2012-081},
 pages = {1--3},
 publisher = {宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS), Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)},
 title = {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},
 year = {2013}
}