@inproceedings{oai:jaxa.repo.nii.ac.jp:00016231,
 author = {浅沼, 和貴 and 柳田, 直人 and 武中, 駿 and 堀澤, 秀之 and Asanuma, Kazuki and Yanagida, Naoto and Takenaka, Satoshi and Horisawa, Hideyuki},
 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, In this study, development of water-Al fed arcjet, for which water and aluminium were fed to the thruster as the propellant, was conducted. As the first step, chemical equilibrium computation of a water-Al fed arcjet was performed, in which plenum temperature, chemical composition, specific impulse, etc, were obtained. From the results, it was shown that thrust performance of the water-Al fed arcjet was as well as that of hydrazine arcjet., 形態: カラー図版あり, 形態: PDF, Translation title: Study on the performance of DC arcjet thruster with chemical equilibrium composition application, Physical characteristics: Original contains color illustrations, Physical characteristics: PDF, 資料番号: AA0061856095, レポート番号: STEP-2012-012},
 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 = {化学援用DCアークジェット推進機},
 year = {2013}
}