@inproceedings{oai:jaxa.repo.nii.ac.jp:00016292,
 author = {陳, 煥俊 and 村岡, 力夫 and 田中, 慎人 and 木咲, 秀彌 and 田原, 弘一 and 脇園, 堯 and Chen, Huanjun and Muraoka, Rikio and Tanaka, Masato and Kisaki, Shuya and Tahara, Hirokazu and Wakizono, Takashi},
 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, The Project of Osaka-Institute-of-Technology Electric-Rocket-Engine onboard Small Space Ship (PROITERES) was started at Osaka Institute of Technology in 2007. In PROITERES, a 14.5-kg nano satellite with electrothermal pulsed plasma thrusters (PPT) was launched on September 9th 2012. The main mission is powered flight of nano satellite by electric thruster itself. Now, we will be trying to establish a contact to satellite. After establishing satellite ignitions by command the thruster will be operated from the ground. In this paper, the performance is predicted by numerical simulation and ground experiment. Furthermore, the 2nd PROITERES satellite with high-power PPT systems was introduced., 形態: カラー図版あり, 形態: PDF, Physical characteristics: Original contains color illustrations, Physical characteristics: PDF, 資料番号: AA0061856156, レポート番号: STEP-2012-073},
 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 = {数値計算による大阪工業大学プロイテレス衛星1、2号機搭載電熱加速型パルスプラズマスラスタの性能予測},
 year = {2013}
}