WEKO3
アイテム
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Preliminary study on sustained arc due to plasma excited by debris impact on the solar array coupon
https://jaxa.repo.nii.ac.jp/records/6393
https://jaxa.repo.nii.ac.jp/records/63938e82ff79-1f11-4c36-8af2-615db54d08b6
名前 / ファイル | ライセンス | アクション |
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49206078.pdf (1.8 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 | Preliminary study on sustained arc due to plasma excited by debris impact on the solar array coupon | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 持続的アーク | |||||
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 | プラズマ相互作用 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 宇宙デブリ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 衝撃損傷 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ソーラーアレイクーポン | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 超高速衝突 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 絶縁破壊 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 短絡 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | sustained arc | |||||
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 | plasma interaction | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | space debris | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | impact damage | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | solar array coupon | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | hypervelocity impact | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | dielectric breakdown | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | short circuit | |||||
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 |
赤星, 保浩
× 赤星, 保浩× 原野, 孝幸× 町田, 裕× 福重, 進也× 高良, 隆男× 細田, 聡史× Cho, Mengu× Akahoshi, Yasuhiro× Harano, Takayuki× Machida, Yu× Fukushige, Shinya× Kora, Takao× Hosoda, Satoshi× Cho, Mengu |
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著者所属 | ||||||
九州工業大学 大学院工学研究科 | ||||||
著者所属 | ||||||
九州工業大学 大学院工学研究科 | ||||||
著者所属 | ||||||
九州工業大学 大学院工学研究科 | ||||||
著者所属 | ||||||
九州工業大学 大学院工学研究科 | ||||||
著者所属 | ||||||
九州工業大学 大学院工学研究科 | ||||||
著者所属 | ||||||
九州工業大学 大学院工学研究科 | ||||||
著者所属 | ||||||
九州工業大学 大学院工学研究科 | ||||||
著者所属(英) | ||||||
en | ||||||
Kyushu Institute of Technology Graduate School of Engineering | ||||||
著者所属(英) | ||||||
en | ||||||
Kyushu Institute of Technology Graduate School of Engineering | ||||||
著者所属(英) | ||||||
en | ||||||
Kyushu Institute of Technology Graduate School of Engineering | ||||||
著者所属(英) | ||||||
en | ||||||
Kyushu Institute of Technology Graduate School of Engineering | ||||||
著者所属(英) | ||||||
en | ||||||
Kyushu Institute of Technology Graduate School of Engineering | ||||||
著者所属(英) | ||||||
en | ||||||
Kyushu Institute of Technology Graduate School of Engineering | ||||||
著者所属(英) | ||||||
en | ||||||
Kyushu Institute of Technology Graduate School of Engineering | ||||||
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. 697-702, 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 | Recently solar array has become higher in potential and larger in capacitance. Therefore, possibility of collision between space debris and enlarged solar array has been pointed out. Actually, a lot of debris and dust impacts were confirmed on fuselage of retrieved satellite SFU and solar array paddle of satellite Eureca. If space debris collides with solar array of an orbit satellite, it causes generation of high-density plasma by debris impact induced dielectric breakdown of satellite component and the phenomenon called discharge. This discharge short circuit and current does not flow into a load of the satellite. And the very worst event by this discharge is operational end of the satellite. However, any events of discharge phenomenon by debris impact cannot be yet confirmed. But we cannot ignore such possibility of discharge by debris impact. The purpose of the present paper is to investigate discharge condition due to debris impact which yields us reduction of electric power of solar array, and to reduce influence of the impact on satellite missions. In this study, a solar array coupon was tested under hypervelocity impact in which a projectile was launched by a two-stage light gas gun installed in KIT. As a result, we verified discharge event in the hypervelocity impact ground test. | |||||
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: AA0049206078 | |||||
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 |