WEKO3
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軽量構体パネルの研究
https://jaxa.repo.nii.ac.jp/records/2716
https://jaxa.repo.nii.ac.jp/records/2716494c4540-6cf4-432a-854d-cf51ca0a5804
名前 / ファイル | ライセンス | アクション |
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48057025.pdf (1.9 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 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | サンドウィッチパネル | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 軽量 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ハニカムコア | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | CFRP | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 構造安定性 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 振動試験 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 低コスト | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | spacecraft structure | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | sandwich panel | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | low weight | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | honeycomb core | |||||
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 | structural stability | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | vibration test | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | low cost | |||||
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 |
石澤, 淳一郎
× 石澤, 淳一郎× 今川, 吉郎× 南, 伸太朗× 馬場, 尚子× 森, 一之× Ishizawa, Junichiro× Imagawa, Kichiro× Minami, Shintaro× Baba, Naoko× Mori, Kazuyuki |
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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研究開発資料: 平成15年度総合技術研究本部宇宙領域研究成果報告書:衛星系 en : JAXA Research and Development Memorandum: FY15 Annual Report of Research & Development on Space Technology in the Institute of Space Technology and Aeronautics: Satellite System 巻 JAXA-RM-04-010, p. 121-124, 発行日 2004-10-29 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Since spacecraft structures constitute a high proportion of total satellite mass, sandwich panels are commonly used which consist of a honeycomb core and either a CFRP or aluminum skin. Sandwich panels have a high specific rigidity, but are expensive to manufacture. JAXA has developed light weight sandwich panels using integral molding of CFRP-prepreg and light weight plastic foam. This material has good workability, design flexibility and a low cost of manufacture. Research on the material's applicability to space structures is almost completed. In this paper, reported are the results of vibration testing of a 50-kg class satellite assembly using these light weight sandwich panels. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1349-1121 | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA11983593 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0048057025 | |||||
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-RM-04-010 |