@inproceedings{oai:jaxa.repo.nii.ac.jp:00005330,
 author = {都木, 恭一郎 and 篠原, 俊二郎 and 谷川, 隆夫 and 羽田, 亨 and 船木, 一幸 and 田中, 良和 and 山口, 晃弘 and Toki, Kyoichiro and Shinohara, Shunjiro and Tanikawa, Takao and Hada, Tohru and Funaki, Ikkoh and Tanaka, Yoshikazu and Yamaguchi, Akihiro and Shamrai, Kostiantyn P.},
 book = {宇宙航空研究開発機構特別資料: 大電力化/モジュール化電気推進に関する研究会, JAXA Special Publication},
 month = {Feb},
 note = {大電力化/モジュール化電気推進に関する研究会(2008年10月21日. 東京国際フォーラム). 主催: 宇宙航空研究開発機構. 後援: 無人宇宙実験システム研究開発機構., One of the promising candidates for high power / modular electric propulsions in the future is an electrodeless Magneto-Plasma-Dynamic Thruster. The electrodeless plasma acceleration as well as the plasma production was examined from the viewpoint of electromagnetic acceleration which is different from the VASIMR magnetic nozzle expansion. A proposal of continuous electromagnetic acceleration 'Lissajous' was fully understood by estimating the thrust and specific impulse. A few preliminary experiments for plasma production and acceleration were also performed as the proof-of-concept level., 形態: カラー図版あり, 資料番号: AA0064241013, レポート番号: JAXA-SP-08-013},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {ヘリコンプラズマ源を用いた無電極MPDスラスタの検討},
 volume = {JAXA-SP-08-013},
 year = {2009}
}