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低地球軌道における高電圧太陽電池アレイを用いた放電実験
https://jaxa.repo.nii.ac.jp/records/3952
https://jaxa.repo.nii.ac.jp/records/39529471797a-c322-4ad0-ac28-b2ce1ae8407f
名前 / ファイル | ライセンス | アクション |
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62301007.pdf (1.3 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 | ||||||
タイトル | 低地球軌道における高電圧太陽電池アレイを用いた放電実験 | |||||
言語 | ||||||
言語 | jpn | |||||
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 | Electro-static discharge | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | On-Orbit | |||||
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 |
岩井, 俊輔
× 岩井, 俊輔× Likar, Justin J.× 奥村, 哲平× 増井, 博一× 豊田, 和弘× 趙, 孟佑× Iwai, Shunsuke× Likar, Justin J.× Okumura, Teppei× Masui, Hirokazu× Toyoda, Kazuhiro× Cho, Mengu |
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著者所属 | ||||||
九州工業大学 | ||||||
著者所属 | ||||||
Lockheed Martin Space Systems Company | ||||||
著者所属 | ||||||
宇宙航空研究開発機構研究開発本部未踏技術研究センター(JAXA) | ||||||
著者所属 | ||||||
九州工業大学 | ||||||
著者所属 | ||||||
九州工業大学 | ||||||
著者所属 | ||||||
九州工業大学 | ||||||
著者所属(英) | ||||||
en | ||||||
Kyushu Institute of Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Lockheed Martin Space Systems Company | ||||||
著者所属(英) | ||||||
en | ||||||
Innovative Technology Research Center, Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Kyushu Institute of Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Kyushu Institute of Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Kyushu Institute of Technology | ||||||
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. 47-56, 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 | Spacecraft payloads are multifunctional and provide a high degree of technicality. Because of these, the power consumption of spacecraft increases. Therefore, the bus voltage must be raised to mitigate the loss during transmission just as it is done for infrastructures on the Earth. Unlike on Earth, 100V is already considered as a high voltage in space, which can lead to arcing because of the interaction of the charged spacecraft with the ambient plasma. The arcing risk is particularly high on solar array. A way of solving problems related to the high voltage technology will be the key for the next generation space technologies such as larger space stations, space hotels, and so on. The authors performed two demonstration experiments in near earth orbit (low earth orbit and polar earth orbit) for testing solutions to the aforementioned problem. First, the data from HORYU-2, nano-satellite developed by Kyushu Institute of Technology, were analyzed. HORYU-2 mission consists in generating 300V without causing arcing, and contributing to the practical development of the next generation space systems. Second, a degradation test by arcs was performed on solar cells onboard the International Space Station by using PASCAL (Primary Arc effect Solar Cell At Leo), which was included MISSE-8 (Material on the International space station Experiment-8). In this paper, the high voltage and the arcing mitigation feasibility from data analysis results in near earth orbit are presented. | |||||
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: Demonstration of arching experiments using high voltage photovoltanic power generation onboard nao-satellite in low earth orbit (CEO) | |||||
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: AA0062301007 | |||||
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 |