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Evaluation of MoS2 Bonded Film degradation on ISS SM-SEED experiment
https://jaxa.repo.nii.ac.jp/records/5230
https://jaxa.repo.nii.ac.jp/records/5230007ecdf1-914a-4cb5-9b23-9edab18a4a85
名前 / ファイル | ライセンス | アクション |
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64307014.pdf (1.1 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 | Evaluation of MoS2 Bonded Film degradation on ISS SM-SEED experiment | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | MPAC&SEED, ISS Service Module, JEM, ELM-ES, PAM, HMB-34 | |||||
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 |
田川, 雅人
× 田川, 雅人× 松本, 康司× 岸, 克宏× 秋山, 正雄× Tagawa, Masahito× Matsumoto, Koji× Kishi, Katsuhiro× Akiyama, Masao |
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著者所属 | ||||||
神戸大学工学部機械工学科 | ||||||
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 | ||||||
超高温材料研究センター | ||||||
著者所属 | ||||||
IHIエアロスペース宇宙技術部 | ||||||
著者所属(英) | ||||||
en | ||||||
Department of Mechanical Engineering, Faculty of Engineering, Kobe University | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Aerospace Technology, Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Ultra-high Temperature Materials Research Institute | ||||||
著者所属(英) | ||||||
en | ||||||
Space Systems Department, IHI Aerospace | ||||||
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. 127-129, 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 | This paper describes upon the on orbit degradation of the MoS2 Bonded Film which are applied to external mechanism of Japanese Experiment Module (JEM) of International Space Station (ISS). The test articles were launched and kept on orbit for 1 year, 2 year and 3 year. Evaluation are performed by measuring adhesive property, friction property and surface properties of the MoS2 bonded film, HMB-34. Also ground environment exposure test were conducted to compare the degradation against on orbit exposed environment effect. | |||||
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: AA0064307014 | |||||
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 |