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Effects of LEO environment on mechanical properties of polyimide films under tensile stress
https://jaxa.repo.nii.ac.jp/records/5227
https://jaxa.repo.nii.ac.jp/records/522768bf7007-f613-4c6d-adfd-d613e4417782
| 名前 / ファイル | ライセンス | アクション |
|---|---|---|
64307011.pdf (546.7 kB)
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| Item type | 会議発表論文 / Conference Paper(1) | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|
| 公開日 | 2015-03-26 | |||||||||
| タイトル | ||||||||||
| タイトル | Effects of LEO environment on mechanical properties of polyimide films under tensile stress | |||||||||
| 言語 | en | |||||||||
| 言語 | ||||||||||
| 言語 | eng | |||||||||
| キーワード | ||||||||||
| 言語 | en | |||||||||
| 主題Scheme | Other | |||||||||
| 主題 | MPAC&SEED, Polyimide film, Mechanical property, Atomic oxygen, Surface roughness | |||||||||
| 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 |
島村, 宏之
× 島村, 宏之
× 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（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. 81-90, 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 | Mechanical properties of polyimide films after exposure to a low earth orbit (LEO) environment were investigated using tensile tests. Polyimide films were placed in a tensile stress state during space exposure to evaluate the effects of tensile stress state on degradation of mechanical properties. Atomic oxygen (AO), ultraviolet (UV), and electron beam (EB) irradiation tests were also conducted for polyimide films to enable comparison to the degradation behavior of the flight samples. Results show that the tensile strength and elongation were decreased by space exposure. The reduction of the mechanical properties became marked as the exposure period increased. The AO irradiation was considered to be the main degrading factor; both UV and EB had only slight effects on the mechanical properties. The tensile strength and elongation of the AO irradiated samples decreased with increased AO fluence. Moreover, the surface roughness of the AO irradiated samples developed dependently on the increased AO fluence. Consequently, surface roughness is one of the leading causes of degradation of mechanical properties. Excessive stress might concentrate at a concave region on the rough surface, leading to formation of surface cracks and initiation points of destruction. No obvious difference attributable to the tensile stress state (below 7 MPa) was apparent in the degradation of mechanical properties. | |||||||||
| 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: AA0064307011 | |||||||||
| 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 | |||||||||
