@inproceedings{oai:jaxa.repo.nii.ac.jp:00016690,
 author = {岡町, 悠介 and 中川, 定紀 and 田原, 弘一 and 長田, 泰一 and 増田, 井出夫 and Okamachi, Yusuke and Nakagawa, Sadanori and Tahara, Hirokazu and Nagata, Taiichi and Masuda, Ideo},
 book = {宇宙輸送シンポジウム: 講演集録, Proceedings of Space Transportation Symposium},
 month = {Jan},
 note = {平成21年度宇宙輸送シンポジウム(2010年1月14日-15日, 宇宙航空研究開発機構宇宙科学研究本部), Space Transportation Symposium (January 14-15, 2010. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency(JAXA)),  Sagamihara, Kanagawa Japan, Hydrazine is used as a propellant of spacecraft thruster. However, hydrazine is a high toxicity liquid. Spacecraft researchers need a low toxicity propellant. Hydroxyl Ammonium Nitrate (HAN: NH3OHNO3) is proposed as low toxicity propellant. The propellant causes the severe chemical reaction, and the electrode is consumed for electic thrusters. In this study, the capability of HAN for DC Arcjet Thruster's propellant is examined. As a result, although the erosion rate of the electrode was severe, after improvement the long-time operation was achieved., 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: AA0064741120},
 publisher = {宇宙航空研究開発機構宇宙科学研究本部, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)},
 title = {直流アークジェットスラスタの低毒性推薬分解ガス適合性に関する研究},
 volume = {平成21年度},
 year = {2010}
}