{"created":"2023-06-20T14:39:31.093247+00:00","id":6257,"links":{},"metadata":{"_buckets":{"deposit":"755ab701-f95f-43e8-9b03-77ae5fce9bd5"},"_deposit":{"created_by":1,"id":"6257","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"6257"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00006257","sets":["1887:1893","9:789:1031:1060"]},"author_link":["31494","31492","31493","31491"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Temperature-dependent fracture performance for multiphase bond structures: Research on space structural technology"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2006-01-20","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"6","bibliographicPageStart":"3","bibliographicVolumeNumber":"JAXA-SP-05-008","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構特別資料: 平成16年度総合技術研究本部宇宙領域宇宙科学研究本部合同研究成果報告書:人工衛星系基盤技術"},{"bibliographic_title":"JAXA Special Publication: FY2004 Report of Joint Research Achievements of the Space Division of Institute of Aerospace Technology and Institute of Space and Astronautical Science: Basic Technologies of Satellite Systems","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Adhesively-bonded structure between advanced CFRP composites and aluminum metal (A1) plays an important role in the development of a lightweight space structure. Accurately understanding the temperature-dependent fracture behaviors of such multiphase bond structures is very important from design safety and durability viewpoints. Substantial thermal stress-strain, which is caused by the mismatch of thermal expansion ratios between adhesives, CFRP composites and aluminum metal could lead to the strength deterioration of such multiphase bond structures over a wide temperature range. In this study, temperature-dependent Mode-2 fracture performance of adhesively-bonded joints between CFRP and A1 was experimentally investigated using a candidate structure adhesive film named AF 163-2K.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0049054001","subitem_description_type":"Other"}]},"item_3_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: JAXA-SP-05-008","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Japan Aerospace Exploration Agency (JAXA)"}]},"item_3_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"1349-113X","subitem_source_identifier_type":"ISSN"}]},"item_3_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AA11984031","subitem_source_identifier_type":"NCID"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"宇宙航空研究開発機構 総合技術研究本部"},{"subitem_text_value":"宇宙航空研究開発機構 総合技術研究本部"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"He, Jianmei"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"下田, 孝幸"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"He, Jianmei","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Shimoda, Takayuki","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":"2020-01-16"}],"displaytype":"detail","filename":"49054001.pdf","filesize":[{"value":"1.5 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"49054001.pdf","url":"https://jaxa.repo.nii.ac.jp/record/6257/files/49054001.pdf"},"version_id":"c0326722-66d3-482a-b792-540273b07953"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"宇宙機構造材料","subitem_subject_scheme":"Other"},{"subitem_subject":"軽量宇宙構造物","subitem_subject_scheme":"Other"},{"subitem_subject":"複合材料","subitem_subject_scheme":"Other"},{"subitem_subject":"CFRP","subitem_subject_scheme":"Other"},{"subitem_subject":"熱応力","subitem_subject_scheme":"Other"},{"subitem_subject":"応力-歪関係","subitem_subject_scheme":"Other"},{"subitem_subject":"熱膨張","subitem_subject_scheme":"Other"},{"subitem_subject":"接着結合ジョイント","subitem_subject_scheme":"Other"},{"subitem_subject":"アルミニウム","subitem_subject_scheme":"Other"},{"subitem_subject":"極低温","subitem_subject_scheme":"Other"},{"subitem_subject":"spacecraft construction material","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"light-weight space structure","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"composite material","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"CFRP","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"thermal stress","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"stress-strain relationship","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"thermal expansion","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"adhesively bonded joint","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aluminum","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"cryogenic temperature","subitem_subject_language":"en","subitem_subject_scheme":"Other"}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"jpn"}]},"item_resource_type":{"attribute_name":"資源タイプ","attribute_value_mlt":[{"resourcetype":"technical report","resourceuri":"http://purl.org/coar/resource_type/c_18gh"}]},"item_title":"複合接着構造の破壊力学特性の温度依存性評価:宇宙機構造技術の研究","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"複合接着構造の破壊力学特性の温度依存性評価:宇宙機構造技術の研究"}]},"item_type_id":"3","owner":"1","path":["1060","1893"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"6257","relation_version_is_last":true,"title":["複合接着構造の破壊力学特性の温度依存性評価:宇宙機構造技術の研究"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:59:03.793814+00:00"}