{"created":"2023-06-20T14:54:11.424002+00:00","id":22467,"links":{},"metadata":{"_buckets":{"deposit":"d7103476-98a7-4cbd-b7bc-b591e2d4ffaa"},"_deposit":{"created_by":1,"id":"22467","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"22467"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00022467","sets":["1887:1888"]},"author_link":["210740","210732","210738","210734","210741","210739","210733","210742","210735","210737","210743","210736"],"item_7_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2014-03","bibliographicIssueDateType":"Issued"},"bibliographicIssueNumber":"2","bibliographicPageEnd":"149","bibliographicPageStart":"129","bibliographicVolumeNumber":"23","bibliographic_titles":[{},{"bibliographic_title":"Advanced Composite Materials","bibliographic_titleLang":"en"}]}]},"item_7_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"This paper presents the mechanical and gas barrier properties of titanium alloy foil-inserted carbon fiber/epoxy composites (CFRPs) undertaken to improve gas barrier properties for cryogenic propellant tank applications. A newly developed β-titanium alloy (GumMetal, GM) was applied. A sheet of titanium foil (α-Ti or GM, 0.05 or 0.1 mm) was inserted between cross-plied composite laminates ([0 degree 2/90 degree 2]S) without adhesive. Epoxy resin in the prepreg contributes to bonding between the Ti-foil and CFRP. The Ti-alloy foil insert did not strongly affect the tensile or compressive strength. Transverse cracks in the 90 degree layer never penetrated into the Ti-alloy foil layer before the final failure under tensile loading. Nonlinear stress-strain behaviors attributable to the pseudo-elastic behaviors of both unidirectional CFRP and β-Ti alloy (GM) were estimated using high-order stiffness and classical lamina theory. The numerical results agreed with the experimentally obtained results. Helium gas leakage under tensile stress was not observed before the final failure of the composites (1.4% of tensile strain). The excellent mechanical and gas barrier properties were successfully demonstrated.","subitem_description_type":"Other"}]},"item_7_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: PA1420014000","subitem_description_type":"Other"}]},"item_7_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Taylor & Francis"}]},"item_7_relation_25":{"attribute_name":"DOI","attribute_value_mlt":[{"subitem_relation_name":[{"subitem_relation_name_text":"info:doi/10.1080/09243046.2013.844756"}],"subitem_relation_type":"isVersionOf","subitem_relation_type_id":{"subitem_relation_type_id_text":"http://dx.doi.org/10.1080/09243046.2013.844756","subitem_relation_type_select":"DOI"}}]},"item_7_rights_28":{"attribute_name":"権利","attribute_value_mlt":[{"subitem_rights":"This is an Accepted Manuscript of an article published by Taylor & Francis in Advanced Composite Materials on 05/11/2013, available online: http://www.tandfonline.com/doi/abs/10.1080/09243046.2013.844756."}]},"item_7_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0924-3046","subitem_source_identifier_type":"ISSN"}]},"item_7_source_id_22":{"attribute_name":"ISSNONLINE","attribute_value_mlt":[{"subitem_source_identifier":"1568-5519","subitem_source_identifier_type":"ISSN"}]},"item_7_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AA10744021","subitem_source_identifier_type":"NCID"}]},"item_7_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"宇宙航空研究開発機構航空本部(JAXA)"},{"subitem_text_value":"青山学院大学"},{"subitem_text_value":"青山学院大学"},{"subitem_text_value":"青山学院大学"},{"subitem_text_value":"東京大学"},{"subitem_text_value":"宇宙航空研究開発機構航空本部(JAXA)"}]},"item_7_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Institute of Aeronautical Technology, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Aoyama-Gakuin University"},{"subitem_text_language":"en","subitem_text_value":"Aoyama-Gakuin University"},{"subitem_text_language":"en","subitem_text_value":"Aoyama-Gakuin University"},{"subitem_text_language":"en","subitem_text_value":"The University of Tokyo"},{"subitem_text_language":"en","subitem_text_value":"Institute of Aeronautical Technology, Japan Aerospace Exploration Agency (JAXA)"}]},"item_7_version_type_30":{"attribute_name":"著者版フラグ","attribute_value_mlt":[{"subitem_version_resource":"http://purl.org/coar/version/c_ab4af688f83e57aa","subitem_version_type":"AM"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"小笠原, 俊夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"荒井, 紀男"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"福本, 亮一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"小川, 武史"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"横関, 智弘"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"吉村, 彰記"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ogasawara, Toshio","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Arai, Norio","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Fukumoto, Ryoichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ogawa, Takeshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yokozeki, Tomohiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yoshimura, Akinori","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_files":{"attribute_name":"ファイル情報","attribute_type":"file","attribute_value_mlt":[{"accessrole":"open_date","date":[{"dateType":"Available","dateValue":"2020-01-22"}],"displaytype":"detail","filename":"PA1420014.pdf","filesize":[{"value":"1.8 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"PA1420014.pdf","url":"https://jaxa.repo.nii.ac.jp/record/22467/files/PA1420014.pdf"},"version_id":"dda4c04a-1e7a-4f47-b245-23c8b83efca4"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"carbon fiber composites","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"titanium alloy foil","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"cryogenic propellant tank","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"matrix crack","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"stress-strain behavior","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"gas leakage","subitem_subject_language":"en","subitem_subject_scheme":"Other"}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"eng"}]},"item_resource_type":{"attribute_name":"資源タイプ","attribute_value_mlt":[{"resourcetype":"journal article","resourceuri":"http://purl.org/coar/resource_type/c_6501"}]},"item_title":"Titanium alloy foil-inserted carbon fiber/epoxy composites for cryogenic propellant tank application","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Titanium alloy foil-inserted carbon fiber/epoxy composites for cryogenic propellant tank application","subitem_title_language":"en"}]},"item_type_id":"7","owner":"1","path":["1888"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"22467","relation_version_is_last":true,"title":["Titanium alloy foil-inserted carbon fiber/epoxy composites for cryogenic propellant tank application"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T03:20:40.643460+00:00"}