@techreport{oai:jaxa.repo.nii.ac.jp:00002097,
 author = {羽田, 亨 and 篠原, 俊二郎 and 都木, 恭一郎 and 谷川, 隆夫 and 船木, 一幸 and Hada, Tohru and Shinohara, Shunjiro and Toki, Kyoichiro and Tanikawa, Takao and Funaki, Ikko},
 month = {Feb},
 note = {2007年12月19日および2008年12月16日開催の研究会における講演より10編の査読論文を収録, Space Plasma Symposium FY2007 and FY2008, Electric thrusters, characterized with high specific impulse, are suited to long duration operations such as planetary missions. On the other hand, the performance of many of the conventional electric thrusters is severely limited by electrode wastage. In order to overcome this difficulty, some novel methods of electrodeless discharge and electromagnetic acceleration have been proposed by making use of a compact helicon plasma source. With this application in mind, we here discuss some basic elements on the behaviour of a collisional, cylindrical plasma, when it is driven by an external time-varying electromagnetic field. By introducing a linear response function, we argue that the external field can resonantly drive the plasma to large amplitude oscillations, which may be utilized for the next generation thrusters., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA0064669006, レポート番号: JAXA-RR-09-003},
 title = {次世代電気推進機関のための外部電磁場によるプラズマ電流励起モデル},
 year = {2010}
}