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Robust design of satellite systems against spacecraft charging
https://jaxa.repo.nii.ac.jp/records/6350
https://jaxa.repo.nii.ac.jp/records/63506b0b4fcd-1fc8-4b67-82c5-1d73806b6b98
名前 / ファイル | ライセンス | アクション |
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49206035.pdf (2.4 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 | Robust design of satellite systems against spacecraft charging | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 衛星設計 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 静電放電 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 宇宙機帯電 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 航空宇宙環境 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 宇宙プラズマ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 電磁干渉 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 宇宙機電子機器 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 設計指針 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 電磁適合性 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | satellite design | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | electrostatic discharge | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | spacecraft charging | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | aerospace environment | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | space plasma | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | electromagnetic interference | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | spacecraft electronic equipment | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | design guideline | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | electromagnetic compatibility | |||||
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 |
小野寺, 範義
× 小野寺, 範義× 村上, 洋一× 小圷, 秀明× Onodera, Noriyoshi× Murakami, Yoichi× Koakutsu, Hideaki |
|||||
著者所属 | ||||||
三菱電機 鎌倉製作所 宇宙システム部 | ||||||
著者所属 | ||||||
三菱電機 鎌倉製作所 宇宙システム部 | ||||||
著者所属 | ||||||
三菱電機 鎌倉製作所 相模工場 | ||||||
著者所属(英) | ||||||
en | ||||||
Mitsubishi Electric Corporation Space Systems Department, Kamakura Works | ||||||
著者所属(英) | ||||||
en | ||||||
Mitsubishi Electric Corporation Space Systems Department, Kamakura Works | ||||||
著者所属(英) | ||||||
en | ||||||
Mitsubishi Electric Corporation Sagami Factory, Kamakura Works | ||||||
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. 272-279, 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 | Space plasma can build up high differential potentials on satellite surfaces resulting in Electrostatic Discharges (ESD), sometimes causing anomalous behavior of satellite systems. As these phenomena give rise to possible risks affecting the performance of satellite, the charging is one of major concerns for satellite manufacturers. It has been investigated the influence of charging phenomena on satellite systems and its mitigation techniques. Our activities include not only investigation of influences on power systems but also that of other risks such as Electromagnetic Compatibility (EMC) or immediate surge to electronic device. In this paper, some of our assessments and the concerned problems are reported. It is obvious that international standardized guidelines for designing satellite systems against ESD will be established in the near future. It would be desirable if the requirements shall be appropriate and practical for satellite systems design, manufacturing and testing. | |||||
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: AA0049206035 | |||||
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 |