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3次元PICシミュレーションを用いた大気吸入型イオンエンジン放電室内部におけるプラズマ生成解析
https://jaxa.repo.nii.ac.jp/records/3806
https://jaxa.repo.nii.ac.jp/records/38063552f5fe-259d-4383-8cc5-cb0e28aec34d
名前 / ファイル | ライセンス | アクション |
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AA1530019021.pdf (621.4 kB)
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Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2015-05-15 | |||||
タイトル | ||||||
タイトル | 3次元PICシミュレーションを用いた大気吸入型イオンエンジン放電室内部におけるプラズマ生成解析 | |||||
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 |
川口, 伸一郎
× 川口, 伸一郎× 臼井, 英之× 三宅, 洋平× 安河内, 翼× 福田, 雅人× 横田, 久美子× 田川, 雅人× Kawaguchi, Shinichiro× Usui, Hideyuki× Miyake, Yohei× Tsubasa, Yasukochi× Fukuda, Masato× Yokota, Kumiko× Tagawa, Masahito |
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著者所属 | ||||||
神戸大学 | ||||||
著者所属 | ||||||
神戸大学 | ||||||
著者所属 | ||||||
神戸大学 | ||||||
著者所属 | ||||||
神戸大学 | ||||||
著者所属 | ||||||
神戸大学 | ||||||
著者所属 | ||||||
神戸大学 | ||||||
著者所属 | ||||||
神戸大学 | ||||||
著者所属(英) | ||||||
en | ||||||
Kobe University | ||||||
著者所属(英) | ||||||
en | ||||||
Kobe University | ||||||
著者所属(英) | ||||||
en | ||||||
Kobe University | ||||||
著者所属(英) | ||||||
en | ||||||
Kobe University | ||||||
著者所属(英) | ||||||
en | ||||||
Kobe University | ||||||
著者所属(英) | ||||||
en | ||||||
Kobe University | ||||||
著者所属(英) | ||||||
en | ||||||
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11回宇宙環境シンポジウム講演論文集 en : JAXA Special Publication: Proceedings of the 11th Spacecraft Environment Symposium 巻 JAXA-SP-14-012, p. 143-147, 発行日 2015-03-20 |
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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11回宇宙環境シンポジウム (2014年12月10日-11日. 大阪府立大学 I-siteなんば), 大阪 | |||||
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 | 11th Spacecraft Environment Symposium (December 10-11, 2014. I-site Namba, Osaka Prefecture University), Osaka, 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 for the development. 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), particularly focused 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 | |||||
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: AA1530019021 | |||||
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-14-012 |