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回転電場を用いたプラズマ推進機の粒子シミュレーション
https://jaxa.repo.nii.ac.jp/records/16277
https://jaxa.repo.nii.ac.jp/records/16277628e69fd-a45c-4534-95cb-4d5c4ea442d3
名前 / ファイル | ライセンス | アクション |
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61856141.pdf (769.5 kB)
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Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 回転電場を用いたプラズマ推進機の粒子シミュレーション | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Electrodeless Plasma Thruster | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Lissajous Acceleration | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Helicon Plasma | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_5794 | |||||
資源タイプ | conference paper | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Particle Simulation of Plasma Thruster with Rotating Electric Field | |||||
著者 |
野村, 亮介
× 野村, 亮介× 大西, 直文× 中村, 隆宏× 西田, 浩之× Nomura, Ryosuke× Onishi, Naofumi× Nakamura, Takahiro× Nishida, Hiroyuki |
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著者所属 | ||||||
東北大学工学部 | ||||||
著者所属 | ||||||
東北大学工学部 | ||||||
著者所属 | ||||||
東京農工大学工学部 | ||||||
著者所属 | ||||||
東京農工大学工学部 | ||||||
著者所属(英) | ||||||
en | ||||||
Faculty of Engineering, Tohoku University | ||||||
著者所属(英) | ||||||
en | ||||||
Faculty of Engineering, Tohoku University | ||||||
著者所属(英) | ||||||
en | ||||||
Faculty of Engineering, Tokyo University of Agriculture and Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Faculty of Engineering, Tokyo University of Agriculture and Technology | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS) | |||||
出版者(英) | ||||||
出版者 | Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS) | |||||
書誌情報 |
平成24年度宇宙輸送シンポジウム: 講演集録 en : Proceedings of Space Transportation Symposium: FY2012 発行日 2013-01 |
|||||
会議概要(会議名, 開催地, 会期, 主催者等) | ||||||
内容記述タイプ | Other | |||||
内容記述 | 平成24年度宇宙輸送シンポジウム (2013年1月17日-1月18日. 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)), 相模原市, 神奈川県 | |||||
会議概要(会議名, 開催地, 会期, 主催者等)(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Space Transportation FY2012 (January 17-18, 2013. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Two-dimensional simulations of Lissajous acceleration were conducted by a code based on Particle-In-Cell (PIC) method for understanding plasma motion in acceleration area and for finding an optimal condition of an electrodeless plasma thruster with rotating electric field. Obtained results show that azimuthal current in the acceleration area depends on ratio of electron drift radius to plasma region length, AC frequency, and ratio of electron cyclotron frequency to AC frequency. High plasma density reduces electric field penetration and then lower the azimuthal current. | |||||
内容記述 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 形態: カラー図版あり | |||||
内容記述 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 形態: PDF | |||||
内容記述(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Physical characteristics: Original contains color illustrations | |||||
内容記述(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Physical characteristics: PDF | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0061856141 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: STEP-2012-058 |