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アイテム
Electrostatic Discharge Ground Test of a Polar Orbit Satellite Solar Panel
http://hdl.handle.net/10228/00006972
http://hdl.handle.net/10228/00006972fc989526-9933-48f5-8e8a-42d4974e88d0
| 名前 / ファイル | ライセンス | アクション |
|---|---|---|
LaSEINE-2006_02.pdf (2.1 MB)
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| アイテムタイプ | 学術雑誌論文 = Journal Article(1) | |||||
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| 公開日 | 2018-11-20 | |||||
| 資源タイプ | ||||||
| 資源タイプ識別子 | http://purl.org/coar/resource_type/c_6501 | |||||
| 資源タイプ | journal article | |||||
| タイトル | ||||||
| タイトル | Electrostatic Discharge Ground Test of a Polar Orbit Satellite Solar Panel | |||||
| 言語 | en | |||||
| 言語 | ||||||
| 言語 | eng | |||||
| 著者 |
趙, 孟佑
× 趙, 孟佑× Kim, Jeong-ho× Hosoda, Satoshi× Nozaki, Yukishige× Miura, Takeshi× Iwata, Takanori |
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| 抄録 | ||||||
| 内容記述タイプ | Abstract | |||||
| 内容記述 | The Advanced Land Observing Satellite that was launched by the Japan Aerospace Exploration Agency in 2006 carries a large solar-array paddle of 22 times 3 m in polar orbit. The wake side of the solar paddle can be charged to a negative value exceeding -1000 V. Numerical simulations and laboratory experiments are carried out to investigate charging and arcing phenomena on the backside of the solar paddle that has exposed bypass diode boards and silver-Teflon thermal film. Possibility of secondary arc and surge voltage between hot and return ends of power circuit has been investigated. The authors irradiate solar-panel coupons with an electron beam to simulate charging situation near the North Pole. Surface flashover is observed once the insulator potential exceeds -7000 V. The authors have also tested charging situation near the South Pole where carbon fiber-reinforced plastics surface facing dense ionospheric plasma may arc easily once a satellite potential drops to -80 or -90 V. The solar-paddle design has been modified to increase the safety margin against arcing, and tests have been carried out to identify the strength limit under extremely harsh test environment. | |||||
| 言語 | en | |||||
| 書誌情報 |
en : IEEE Transactions on Plasma Science 巻 34, 号 5, p. 2011-2030, 発行日 2006-10-16 |
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| 出版社 | ||||||
| 出版者 | IEEE | |||||
| DOI | ||||||
| 関連タイプ | isVersionOf | |||||
| 識別子タイプ | DOI | |||||
| 関連識別子 | https://doi.org/10.1109/TPS.2006.881935 | |||||
| NCID | ||||||
| 収録物識別子タイプ | NCID | |||||
| 収録物識別子 | AA0066803X | |||||
| ISSN | ||||||
| 収録物識別子タイプ | EISSN | |||||
| 収録物識別子 | 1939-9375 | |||||
| ISSN | ||||||
| 収録物識別子タイプ | PISSN | |||||
| 収録物識別子 | 0093-3813 | |||||
| 著作権関連情報 | ||||||
| 権利情報 | Copyright (c) 2006 IEEE. Personal use of this material is permitted. Permission from IEEE must be obtained for all other uses, in any current or future media, including reprinting/republishing this material for advertising or promotional purposes, creating new collective works, for resale or redistribution to servers or lists, or reuse of any copyrighted component of this work in other works. | |||||
| キーワード | ||||||
| 主題Scheme | Other | |||||
| 主題 | Aurora | |||||
| キーワード | ||||||
| 主題Scheme | Other | |||||
| 主題 | Earth Observation Satellite (EOS) | |||||
| キーワード | ||||||
| 主題Scheme | Other | |||||
| 主題 | ground test | |||||
| キーワード | ||||||
| 主題Scheme | Other | |||||
| 主題 | particle simulation | |||||
| キーワード | ||||||
| 主題Scheme | Other | |||||
| 主題 | polar orbit | |||||
| キーワード | ||||||
| 主題Scheme | Other | |||||
| 主題 | solar array | |||||
| キーワード | ||||||
| 主題Scheme | Other | |||||
| 主題 | spacecraft charging | |||||
| キーワード | ||||||
| 主題Scheme | Other | |||||
| 主題 | thermal film | |||||
| 出版タイプ | ||||||
| 出版タイプ | AM | |||||
| 出版タイプResource | http://purl.org/coar/version/c_ab4af688f83e57aa | |||||
| 査読の有無 | ||||||
| 値 | yes | |||||
| 研究者情報 | ||||||
| URL | https://hyokadb02.jimu.kyutech.ac.jp/html/168_ja.html | |||||
| 論文ID（連携） | ||||||
| 値 | 10017525 | |||||
| 連携ID | ||||||
| 値 | 248 | |||||
