@inproceedings{oai:jaxa.repo.nii.ac.jp:00016510,
 author = {藤田, 雄也 and 岡町, 悠介 and 下城, 礼央 and 中川, 和哉 and 田原, 弘一 and 長田, 泰一 and 増田, 井出夫 and Fujita, Katsuya and Okamachi, Yusuke and Shimojo, Reo and Nakagawa, Kazuya and Tahara, Hirokazu and Nagata, Taiichi and Masuda, Ideo},
 book = {平成22年度宇宙輸送シンポジウム: 講演集録, Proceedings of Space Transportation Symposium: FY2010},
 month = {},
 note = {平成22年度宇宙輸送シンポジウム(2011年1月20-21日. 宇宙航空研究開発機構宇宙科学研究所), 相模原市, 神奈川県, Space Transportation FY2010 (January 20-21, 2011. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency(JAXA)(ISAS)), Sagamihara, Kanagawa Japan, Hydrazine is used as a propellant of spacecraft thruster. However, hydrazine high toxicity liquid. Spacecraft researchers need a low toxicity propellant. Hydroxyl Ammonium Nitrate (HAN: NH3OHNO3) is proposed as low toxicity propellant. The propellant caused the severe reaction, and the electrode is consumed for electic thrusters. In this study, the capability of HAN for DC Arcjet Arcjet Thruster's propellant is examined. As a result, the stable operation was achieved with HAN although the thrust performance was very low., 形態: カラー図版あり, 形態: CD-ROM1枚, Physical characteristics: Original contains color illustrations, Note: One CD-ROM, 資料番号: AA0065073063, レポート番号: STCP-2010-076},
 publisher = {宇宙航空研究開発機構宇宙科学研究所, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)},
 title = {低毒性推薬HANを用いた直流アークジェットスラスタの性能特性},
 year = {2011}
}