@inproceedings{oai:jaxa.repo.nii.ac.jp:00016796,
 author = {高木, 宏樹 and 山本, 剛史 and 石井, 悠介 and 田原, 弘一 and Takagi, Hiroki and Yamamoto, Tsuyoshi and Ishii, Yusuke 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 powered flight of small satellite by electric thruster itself. This study aims at improvement in performance by changing configuration of PPTs．The PPT with a discharge room diameter of 3.0 mm and an insulator length of 10.0 mm stably generated the highest impulse bit of 350 microNs., 形態: カラー図版あり, 資料番号: AA0064292103},
 pages = {1--5},
 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・小型スペースシップ搭載用電熱加速型パルスプラズマスラスタの性能測定},
 volume = {平成20年度},
 year = {2009}
}