@inproceedings{oai:jaxa.repo.nii.ac.jp:00016667,
 author = {小紫, 公也 and 川嶋, 嶺 and 横田, 茂 and 荒川, 義博 and Schonherr, Tony and Komurasaki, Kimiya and Kawashima, Rei and Yokota, Shigeru and Arakawa, Yoshihiro and Lau, Matthias and Herdrich, Georg and Roser, Hans-Peter},
 book = {宇宙輸送シンポジウム: 講演集録, Proceedings of Space Transportation Symposium},
 month = {Jan},
 note = {平成21年度宇宙輸送シンポジウム(2010年1月14日-15日, 宇宙航空研究開発機構宇宙科学研究本部), Space Transportation Symposium (January 14-15, 2010. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency(JAXA)),  Sagamihara, Kanagawa Japan, The pulsed plasma thruster SIMP?LEX is developed at IRS of the University of Stuttgart in close cooperation with the University of Tokyo in order to serve as main propulsion system for the planned small satellite missions Perseus and Lunar Mission BW1. Following the development of an engineering model and several researches at IRS, the project was extended into this international cooperation for an improved insight into the physics and the discharge behavior of the thruster. A short overview about the project and former researches is given, and details about the setup in Japan are provided. Further, first researches aiming at the characterization of the discharge and its dependencies are explained and the results shown., 形態: カラー図版あり, 形態: CD-ROM1枚, Physical characteristics: Original contains color illustrations, Note: One CD-ROM, 資料番号: AA0064741097},
 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 = {SIMP-LEX: A German-Japanese Pulsed Plasma Thruster Project},
 volume = {平成21年度},
 year = {2010}
}