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タイトルTechnique for fabrication by resistance heating and tensile properties of CFRP cables
その他のタイトルCFRPケーブルの抵抗加熱製造法と張力特性
著者(日)本山 泰之; 守屋 一政; 太田 俊昭
著者(英)Motoyama, Hiroyuki; Moriya, Kazumasa; Ota, Toshiaki
著者所属(日)防衛大学校 システム工学群 航空宇宙工学科; 防衛大学校 システム工学群 航空宇宙工学科; 九州大学 大学院工学研究院
著者所属(英)National Defense Academy Department of Aerospace Engineering, School of Systems Engineering; National Defense Academy Department of Aerospace Engineering, School of Systems Engineering; Kyushu University Graduate School of Engineering
発行日2002-06-26
刊行物名Memoirs of the Faculty of Engineering, Kyushu University
九州大学工学紀要
62
2
開始ページ97
終了ページ111
刊行年月日2002-06-26
言語eng
抄録This study is to propose the on-orbit fabrication of CFRP cable net structures by using the method of electrical resistance heating in order to construct large space structures in the near future. The on-orbit fabrication of cable net structures is accomplished by transporting coiled stock of prepreg of CFRP cable from the earth to the orbit and curing it by means of the resistance heating whose operating power is supplied by the solar electric power system. Laboratory tests indicate that CFRP cables can be cured uniformly and precisely with the specified cure cycle by controlling the low voltage current. Tensile tests for CFRP cables cured by the resistance heating as well as those of uncured ones have also been performed and the results show that the cured cables exhibit the high tensile strength and stiffness which are about two times higher than those of the uncured ones. In preparing for the tensile specimens of uncured cables, it has been found that any part of CFRP cables can be left uncured by the present method without changing the curing process. At these uncured portions, they can be bent for folding and be connected to other structural members with knots without using mechanical hinges or joints.
キーワードcomposite material; CFRP; cable network; on orbit fabrication; resistance heating; tensile test; stiffness; large space structure; research and development; 複合材; CFRP; ケーブルネットワーク; 軌道上製造; 抵抗加熱; 張力試験; 硬さ; 大型宇宙構造体; 研究開発
資料種別Technical Report
ISSN1345-868X
SHI-NOAA0033106001
URIhttps://repository.exst.jaxa.jp/dspace/handle/a-is/27597


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