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炭素繊維強化形状記憶ポリマの宇宙適用性評価
https://jaxa.repo.nii.ac.jp/records/5994
https://jaxa.repo.nii.ac.jp/records/59941f40a081-3a38-4cab-ac88-b87c24ba1245
名前 / ファイル | ライセンス | アクション |
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49500010.pdf (1.1 MB)
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Item type | テクニカルレポート / Technical Report(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 炭素繊維強化形状記憶ポリマの宇宙適用性評価 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 形状記憶ポリマ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 炭素繊維強化樹脂 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 展開式構造 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 大型宇宙構造物 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 航空宇宙環境 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 複合材料 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ガラス転移温度 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | プリプレグ | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | shape memory polymer | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | carbon fiber reinforced plastic | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | deployable structure | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | large space structure | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | aerospace environment | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | composite material | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | glass transition temperature | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | prepreg | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_18gh | |||||
資源タイプ | technical report | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Space applicability study on carbon reinforced shape memory polymer | |||||
著者 |
石澤, 淳一郎
× 石澤, 淳一郎× 南, 伸太朗× 島村, 宏之× Ishizawa, Junichiro× Minami, Shintaro× 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 | ||||||
Japan Aerospace Exploration Agency Institute of Aerospace Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Aerospace Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Aerospace Technology | ||||||
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: 平成18年度 宇宙航空研究開発機構 総合技術研究本部 宇宙科学研究本部 研究成果報告書 en : JAXA Special Publication: Report on Research Achievements for FY2006 Institute of Space and Astronautical Science, Institute of Aerospace Technology, Japan Aerospace Exploration Agency 巻 JAXA-SP-06-006, p. 53-56, 発行日 2006-11-01 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Carbon fiber reinforced shape memory polymer (FR-SMP) has been developed for space deployable structures as solar paddles, antennas, etc. This material is lightweight, low-cost, and has high workability. We have experimentally proved enough tolerance against space environment for its mechanical and shapes recover property. Deploying test using flat plate models has been revealed that unidirectional reinforced configuration has good shape memory property due to well-balanced rigidity and flexibility. Hemisphere model has been produced through newly-developed FR-SMP dry prepreg. | |||||
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: AA0049500010 | |||||
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-06-006 |