軽量構体パネルの研究

Material type: 文書・図像類

Author: 石澤, 淳一郎ほか

Publisher: 宇宙航空研究開発機構

Publication date: 2004-10-29

Material Format: Digital

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Note (General)：: Since spacecraft structures constitute a high proportion of total satellite mass, sandwich panels are commonly used which consist of a honeycomb core ...

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Material Type: 文書・図像類
Title: 軽量構体パネルの研究
Author/Editor: 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
Author Heading: 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
Publication, Distribution, etc.: 宇宙航空研究開発機構
Publication Date: 2004-10-29
Publication Date (W3CDTF): 2004-10-29
Alternative Title: Research on light weight sandwich panels
Periodical title: 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 = JAXA Research and Development Memorandum: FY15 Annual Report of Research & Development on Space Technology in the Institute of Space Technology and Aeronautics: Satellite System
No. or year of volume/issue: JAXA-RM-04-010
Volume: JAXA-RM-04-010
Pages: 121-124
ISSN (Periodical Title): ISSN : 1349-1121
Text Language Code: jpn
Subject Heading: 宇宙機構造
サンドウィッチパネル
軽量
ハニカムコア
CFRP
構造安定性
振動試験
低コスト
spacecraft structure
sandwich panel
low weight
honeycomb core
structural stability
vibration test
low cost
Target Audience: 一般
Note (General): 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.
資料番号: AA0048057025
レポート番号: JAXA-RM-04-010
Access Restrictions: 限定公開
Periodical Title (NCID): AA11983593
https://ci.nii.ac.jp/ncid/AA11983593
Data Provider (Database): 国立情報学研究所 : 学術機関リポジトリデータベース（IRDB）（機関リポジトリ）
https://irdb.nii.ac.jp
Original Data Provider (Database): 宇宙航空研究開発機構 : 宇宙航空研究開発機構リポジトリ