WEKO3
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軽量構体パネルの研究
https://jaxa.repo.nii.ac.jp/records/6288
https://jaxa.repo.nii.ac.jp/records/62880dc776af-66c6-49ef-8fb1-f58db5c33fcd
名前 / ファイル | ライセンス | アクション |
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49054032.pdf (2.3 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 | 軽量構体パネルの研究 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 宇宙機構造材料 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | プレプレグ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 軽量化 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | プラスチックフォーム | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | CFRP | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | サンドイッチ構造 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 破壊試験 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 3点曲げ試験 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | spacecraft construction material | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | prepreg | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | weight reduction | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | plastic foam | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | CFRP | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | sandwich structure | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | fracture test | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | three-point bending test | |||||
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 | Research on light weight sandwich panels | |||||
著者 |
森, 一之
× 森, 一之× 島村, 宏之× 石澤, 淳一郎× 南, 伸太朗× 馬場, 尚子× Mori, Kazuyuki× Shimamura, Hiroyuki× Ishizawa, Junichiro× Minami, Shintaro× Baba, Naoko |
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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 | ||||||
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 Space Technology and Aeronautics | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics | ||||||
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16年度総合技術研究本部宇宙領域宇宙科学研究本部合同研究成果報告書:人工衛星系基盤技術 en : JAXA Special Publication: FY2004 Report of Joint Research Achievements of the Space Division of Institute of Aerospace Technology and Institute of Space and Astronautical Science: Basic Technologies of Satellite Systems 巻 JAXA-SP-05-008, p. 159-162, 発行日 2006-01-20 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Aluminum honeycomb sandwich panels are commonly used as spacecraft structures. The panels have a high specific rigidity, but are expensive. We have developed light-weight, low-cost sandwich panels using integral molding of CFRP-prepreg and light weight plastic foam. This panel has good workability, and thus higher design flexibility. In this paper, we report recent research results on the light weight sandwich panel, including simulation analysis and fracture tests. Analytical and experimental results show that further improvement in fracture strength of the panel will be expected. | |||||
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: AA0049054032 | |||||
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-05-008 |