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A HG-IFE-PIC model for ion thruster plume interactions
https://jaxa.repo.nii.ac.jp/records/6372
https://jaxa.repo.nii.ac.jp/records/63727e2f6ceb-40d4-48ac-a216-1384bae5e3cd
名前 / ファイル | ライセンス | アクション |
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49206057.pdf (2.0 MB)
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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 | ||||||
言語 | en | |||||
タイトル | A HG-IFE-PIC model for ion thruster plume interactions | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | イオンスラスタ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | アルゴリズム | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 計算機プログラム | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 数値シミュレーション | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 宇宙機-プラズマ相互作用 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 高速プラズマ流 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | particle-in-cell法 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 不均一プラズマ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 境界条件 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | ion thruster | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | algorithm | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | computer program | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | numerical simulation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | spacecraft-plasma interaction | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | high speed plasma flow | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | particle-in-cell method | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | nonuniform plasma | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | boundary condition | |||||
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 | |||||
著者 |
Wang, J.
× Wang, J.× Kafafy, R. |
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著者所属 | ||||||
Virginia Polytech. Inst. and State Univ. | ||||||
著者所属 | ||||||
Virginia Polytech. Inst. and State Univ. | ||||||
著者所属(英) | ||||||
en | ||||||
Virginia Polytechnic Institute and State University | ||||||
著者所属(英) | ||||||
en | ||||||
Virginia Polytechnic Institute and State University | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構 | |||||
出版者(英) | ||||||
出版者 | Japan Aerospace Exploration Agency (JAXA) | |||||
書誌情報 |
宇宙航空研究開発機構特別資料 en : JAXA Special Publication: 9th Spacecraft Charging Technology Conference 巻 JAXA-SP-05-001E, p. 520-528, 発行日 2005-08-01 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | This paper presents a new algorithm, the hybrid-grid immersed-finite-element particle-in-cell, for modeling electric propulsion plume spacecraft interactions. This algorithm is designed to handle the complex boundary condition of a real spacecraft accurately while maintaining the computational speed of a standard PIC code. Simulations are performed to study multiple-ion thruster plume spacecraft interactions. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1349-113X | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA11984031 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0049206057 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: JAXA-SP-05-001E |