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大気吸入型イオンエンジン放電室内におけるプラズマ生成シミュレーション
https://jaxa.repo.nii.ac.jp/records/3954
https://jaxa.repo.nii.ac.jp/records/39543903f86c-01d2-4b37-843d-5bafa8b42530
名前 / ファイル | ライセンス | アクション |
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62301009.pdf (842.3 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 | 大気吸入型イオンエンジン放電室内におけるプラズマ生成シミュレーション | |||||
言語 | ||||||
言語 | jpn | |||||
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 |
本山, 貴仁
× 本山, 貴仁× 臼井, 英之× 三宅, 洋平× 川口, 伸一郎× 横田, 久美子× 田川, 雅人× Motoyama, Takahito× Usui, Hideyuki× Miyake, Yohei× Kawaguchi, Shinichiro× Yokota, Kumiko× Tagawa, Masahito |
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著者所属 | ||||||
神戸大学大学院工学研究科 | ||||||
著者所属 | ||||||
神戸大学大学院システム情報学研究科 | ||||||
著者所属 | ||||||
神戸大学大学院システム情報学研究科 | ||||||
著者所属 | ||||||
神戸大学大学院工学研究科 | ||||||
著者所属 | ||||||
神戸大学大学院工学研究科 | ||||||
著者所属 | ||||||
神戸大学大学院工学研究科 | ||||||
著者所属(英) | ||||||
en | ||||||
Graduate School of Engineering, Kobe University | ||||||
著者所属(英) | ||||||
en | ||||||
Graduate School of System Informatics, Kobe University | ||||||
著者所属(英) | ||||||
en | ||||||
Graduate School of System Informatics, Kobe University | ||||||
著者所属(英) | ||||||
en | ||||||
Graduate School of Engineering, Kobe University | ||||||
著者所属(英) | ||||||
en | ||||||
Graduate School of Engineering, Kobe University | ||||||
著者所属(英) | ||||||
en | ||||||
Graduate School of Engineering, Kobe University | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構(JAXA) | |||||
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: 第10回宇宙環境シンポジウム講演論文集 en : JAXA Special Publication: Proceedings of the 10th Spacecraft Environment Symposium 巻 JAXA-SP-13-016, p. 61-64, 発行日 2014-03-31 |
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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 | 第10回宇宙環境シンポジウム (2013年12月2日-3日. 科学技術館), 東京 | |||||
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 | 10th Spacecraft Environment Symposium (December 2-3, 2013, Science Museum), Tokyo Japan | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | In order to operate a satellite in sub-low earth orbit (sub-LEO), it is required to design an optimum ion engine to compensate the drag of the upper atmosphere. The air breathing ion engine (ABIE) is one of promising candidates for such an ion engine. However, the optimum design rule has not been established. Because ground experiments are difficult for ABIE, numerical simulation is a useful approach. In this study, in order to establish a useful guideline for designing ABIE, we perform particle simulations to examine plasma discharge in the ABE chamber by using the electromagnetic spacecraft environment simulator (EMSES). We particularly focus on electron acceleration process via electron cyclotron resonance. | |||||
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(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 | Translation title: Numerical Plasma Generation in the discharge chamber of sir breathing ion engine | |||||
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: AA0062301009 | |||||
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-13-016 |