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Evaluation of F-OSR exposed to space on SM/SEED experiment
https://jaxa.repo.nii.ac.jp/records/5234
https://jaxa.repo.nii.ac.jp/records/5234f05ed286-9b97-4d68-ac55-771cfef92ba9
名前 / ファイル | ライセンス | アクション |
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64307018.pdf (476.5 kB)
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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 | Evaluation of F-OSR exposed to space on SM/SEED experiment | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | optical solar reflector, polyetherimide | |||||
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 |
宮崎, 英治
× 宮崎, 英治× 石澤, 淳一郎× 島村, 宏之× Miyazaki, Eiji× Ishizawa, Junichiro× Shimamura, Hiroyuki |
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著者所属 | ||||||
宇宙航空研究開発機構総合技術研究本部 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構総合技術研究本部 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構総合技術研究本部 | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Aerospace Technology, Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Aerospace Technology, Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Aerospace Technology, Japan Aerospace Exploration Agency (JAXA) | ||||||
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: Proceedings of International Symposium on "SM/MPAC & SEED Experiment" 巻 JAXA-SP-08-015E, p. 149-154, 発行日 2009-03-31 |
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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 | International Symposium on "SM/MPAC & SEED Experiment" (International Congress Center EPOCHAL TSUKUBA, 10-11 March 2008) | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | A Flexible Optical Solar Reflector (F-OSR) is a thermal control film for spacecraft. It provides low solar absorptance (alpha(sub s)) and high infrared emittance (epsilon) with flexibility. The F-OSR, which has a conductive layer and a mirror layer coated onto a polyetherimide base film, is a thermal control film material for spacecraft. Results indicate a mass increase: atomic oxygen does not erode F-OSR in low earth orbit. Thermo-optical properties show no marked change. In fact, F-OSR is verified as retaining its initial properties after exposure on ISS orbit for 46 months. Transmission electron microscopy (TEM) observation of cross-sections, including those of the exposed surface, showed that a new layer had formed over the flight sample. Qualitative analysis of the new layer indicates that the layer mainly comprises silicon and oxygen. The layer is chemically produced by deposited silicon contamination and atomic oxygen, which would be SiO2. This experiment also provides actual quantitative contamination data on ISS, contributing to improvement of contamination control on ISS in the future. | |||||
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: AA0064307018 | |||||
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-08-015E |