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

Material type: 文書・図像類

Author: 羽田, 亨ほか

Publisher: 宇宙航空研究開発機構

Publication date: 2010-02-26

Material Format: Digital

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Note (General)：: 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 FY2008Electric thrusters, characterized with high specific impulse...

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Material Type: 文書・図像類
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
Author/Editor: 羽田, 亨
篠原, 俊二郎
都木, 恭一郎
谷川, 隆夫
船木, 一幸
Hada, Tohru
Shinohara, Shunjiro
Toki, Kyoichiro
Tanikawa, Takao
Funaki, Ikko
Author Heading: 羽田, 亨
篠原, 俊二郎
都木, 恭一郎
谷川, 隆夫
船木, 一幸
Hada, Tohru
Shinohara, Shunjiro
Toki, Kyoichiro
Tanikawa, Takao
Funaki, Ikko
Publication, Distribution, etc.: 宇宙航空研究開発機構
Publication Date: 2010-02-26
Publication Date (W3CDTF): 2010-02-26
Alternative Title: Theoretical Modeling of Next Generation Electrodeless Plasma Thrusters Driven By External Electromagnetic Field
Periodical title: 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
No. or year of volume/issue: JAXA-RR-09-003
Volume: JAXA-RR-09-003
ISSN (Periodical Title): ISSN : 1349-1113
Text Language Code: jpn
Subject Heading: electrodeless plasma thruster, compact helicon source
Target Audience: 一般
Note (General): 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
Access Restrictions: 限定公開
Periodical Title (NCID): AA1192675X
https://ci.nii.ac.jp/ncid/AA1192675X
Data Provider (Database): 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）
https://irdb.nii.ac.jp
Original Data Provider (Database): 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