並列タイトル等Theoretical Modeling of Next Generation Electrodeless Plasma Thrusters Driven By External Electromagnetic Field
タイトル（掲載誌）宇宙航空研究開発機構研究開発報告: 2007/2008年度宇宙関連プラズマ研究会講演集 = JAXA Research and Development Report
一般注記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
一次資料へのリンクURLhttps://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=2097&item_no=1&attribute_id=31&file_no=1
連携機関・データベース国立情報学研究所 : 学術機関リポジトリデータベース（IRDB）（機関リポジトリ）
提供元機関・データベース宇宙航空研究開発機構 : 宇宙航空研究開発機構リポジトリ