構造技術の研究:GXロケットLNG推進系複合材タンク開発支援のための評価試験

Material type: 文書・図像類

Author: He, Jianmei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)：: Adhesively-bonded structure between CFRP composites and Aluminum metal (Al) plays an important role in the development of a light-weight Aluminum-line...

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Material Type: 文書・図像類
Title: 構造技術の研究:GXロケットLNG推進系複合材タンク開発支援のための評価試験
Author/Editor: He, Jianmei
下田, 孝幸
幸節, 雄二
Shimoda, Takayuki
Kosetsu, Yuji
Author Heading: He, Jianmei
下田, 孝幸
幸節, 雄二
Shimoda, Takayuki
Kosetsu, Yuji
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: Researches on space structural technology: Cryogenic mechanical performance assessments for LNG composite tank development of the GX rocket
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:輸送系 = JAXA Research and Development Memorandum: FY15 Annual Report of Research & Development on Space Technology in the Institute of Space Technology and Aeronautics: Space Transportation System
No. or year of volume/issue: JAXA-RM-04-009
Volume: JAXA-RM-04-009
Pages: 37-42
ISSN (Periodical Title): ISSN : 1349-1121
Text Language Code: jpn
Subject Heading: CFRP
複合材料
アルミニウム
燃料タンク
宇宙構造体
熱応力
熱膨張
破壊強度
composite material
aluminum
propellant tank
space structure
thermal stress
thermal expansion
fracture strength
Target Audience: 一般
Note (General): Adhesively-bonded structure between CFRP composites and Aluminum metal (Al) plays an important role in the development of a light-weight Aluminum-lined CFRP cryogenic propellant tank in terms of design safety and durability. Large thermal stresses and strains produced by the difference of thermal expansion ratios among an adhesive material, CFRP composite and aluminum liner will lead to the potential of fracture strength deterioration for CFRP-Adhesive-Al bond structures at cryogenic temperatures below - 150 C. In this study, experimentally investigated was some temperature-dependent mechanical performance of the adhesive film AF163-2K itself and CFRP-AF163-2K-Al bond structures.
資料番号: AA0047944008
レポート番号: JAXA-RM-04-009
Source: https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=2739&item_no=1&attribute_id=31&file_no=1
https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=2739&item_no=1&attribute_id=31&file_no=1
Access Restrictions: 限定公開
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