@inproceedings{oai:jaxa.repo.nii.ac.jp:00016795,
 author = {山田, 峰嗣 and 池田, 知行 and 清水, 雅治 and 藤原, 達也 and 川口, 司 and 田原, 弘一 and Yamada, Minetsugu and Ikeda, Tomoyuki and Shimizu, Masaharu and Fujiwara, Tatsuya and Kawaguchi, Tsukasa and Tahara, Hirokazu},
 book = {宇宙輸送シンポジウム: 講演集録, Proceedings of Space Transportation Symposium},
 month = {},
 note = {平成20年度宇宙輸送シンポジウム(2009年1月19日-20日, 宇宙航空研究開発機構宇宙科学研究本部), 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 10-kg small satellite with electrothermal pulsed plasma thrusters (PPTs), named JOSHO, will be launched in 2010. The main mission is to achieve powered flight of small satellite by electric thruster . In this paper, the present progress is shown., 形態: カラー図版あり, 資料番号: AA0064292102},
 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 = {大阪工業大学・電気推進ロケットエンジン搭載小型スペースシッププロジェクトの進捗状況},
 volume = {平成20年度},
 year = {2009}
}