@inproceedings{oai:jaxa.repo.nii.ac.jp:00049523,
 author = {古谷, 楓真 and 笹井, 優衣 and 飯干, 壮馬 and 澤邊, 陽 and 池本, 凌 and 田原, 弘一 and 桃沢, 愛 and 中田, 大将 and 鷹尾, 良行 and 池田, 知行 and 野川, 雄一郎 and 脇園, 堯 and 外山, 雅也 and FURUTANI, Fuma and SASAI, Yui and IIBOSHI, Soma and SAWABE, Ataru and IKEMOTO, Ryo and TAHARA, Hirokazu and MOMOZAWA, Ai and NAKATA, Daisuke and TAKAO, Yoshiyuki and IKEDA, Tomoyuki and NOGAWA, Yuichiro and WAKIZONO, Takashi and TOYAMA, Masaya},
 book = {令和4年度宇宙輸送シンポジウム: 講演集録, Proceedings of Space Transportation Symposium FY2022},
 month = {Jan},
 note = {令和4年度宇宙輸送シンポジウム（2023年1月12日-13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 Symposium FY2022 (January 12-13, 2023. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan, The direct-current (DC) arcjet thruster is one of electric propulsion for satellite attitude control and orbital transfer. Hydrazine is mainly used as the propellant because it can be used together with chemical thrusters. In this study, performance characteristics of a low-power (0.1-2.0 kW) anode-radiation-cooled arcjet thruster were measured using special gases of carbon dioxide, methane, ammonia and water as original materials in planets and satellites in the Solar System; that is, propellant can be supplied just on the planets and satellites of Moon, Mars and Jupiter Moons, although light gases of hydrazine and hydrogen are normally used with higher performance; argon and nitrogen are also used in basic experiments. Because the performances with carbon dioxide and methane were lower than that with the light gas of ammonia, the structure and operational condition should be examined to design a thruster suitable with acceptable performance for transportation in the Solar System. As for water propellant, steady-state operation was achieved with stable supply of vapor using a metal glow-plug heater or a new water-vaporing system, which was developed with a long, narrow passage and a large sheet-type heater., 著者人数: 13名, 資料番号: SA6000184067, STEP-2022-015},
 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 = {直流アークジェットスラスタの作動特性と高性能化: 太陽系惑星・衛星に存在する物資：二酸化炭素，メタン，アンモニア， 水素，ヘリウム，空気，氷・水などの推進剤への利用},
 year = {2023}
}