Osaka Institute of Technology
Osaka Institute of Technology
Osaka Institute of Technology
Osaka Institute of Technology
Osaka Institute of Technology
Japan Aerospace Exploration Agency (JAXA)
Japan Aerospace Exploration Agency (JAXA)
出版者
宇宙航空研究開発機構宇宙科学研究所
出版者（英）
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)
雑誌名
平成22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: FY2010
Space Transportation FY2010 (January 20-21, 2011. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency(JAXA)(ISAS)), Sagamihara, Kanagawa Japan
抄録（英）
Hydrazine is used as a propellant of spacecraft thruster. However, hydrazine is high toxicity liquid. Spacecraft researchers need a low toxicity propellant. Hydroxyl Ammonium Nitrate (HAN: NH3OHNO3) is proposed as need a low toxicity propellant. The propellant causes the severe reaction, and electrode is consumed for electic thrusters. In this study, the capability of HAN for DC Arcjet Thruster's propellant is examined. As a result, the stable operation was achieved with HAN although the thrust performance was very low.
内容記述
形態: カラー図版あり
形態: CD-ROM1枚
内容記述（英）
Physical characteristics: Original contains color illustrations
Note: One CD-ROM
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
