{"created":"2023-06-20T14:38:38.396352+00:00","id":5225,"links":{},"metadata":{"_buckets":{"deposit":"a02af9f5-8244-4386-8d80-90f5fdcf2f82"},"_deposit":{"created_by":1,"id":"5225","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"5225"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00005225","sets":["1887:1891","9:789:956:958"]},"author_link":["25127","25128"],"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2009-03-31","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"71","bibliographicPageStart":"67","bibliographicVolumeNumber":"JAXA-SP-08-015E","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構特別資料"},{"bibliographic_title":"JAXA Special Publication: Proceedings of International Symposium on \"SM/MPAC & SEED Experiment\"","bibliographic_titleLang":"en"}]}]},"item_5_description_15":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）（英）","attribute_value_mlt":[{"subitem_description":"International Symposium on \"SM/MPAC & SEED Experiment\" (International Congress Center EPOCHAL TSUKUBA, 10-11 March 2008)","subitem_description_type":"Other"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Polymer matrix composites such as carbon fiber reinforced plastic (CFRP) are lightweight materials which have good mechanical properties and are applied widely as basic structural materials for spacecraft, especially reusable launch vehicle. However the degradation data of the CFRP after exposed in space environment for long period was not obtained in ground experiment. Therefore understanding the process of degradation for CFRP is very important to maintain structural reliability. In this study we evaluate the two heat resistant CFRP which are candidates for the reusable launch vehicle.","subitem_description_type":"Other"}]},"item_5_description_19":{"attribute_name":"内容記述（英）","attribute_value_mlt":[{"subitem_description":"Physical characteristics: Original contains color illustrations","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0064307009","subitem_description_type":"Other"}]},"item_5_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: JAXA-SP-08-015E","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Japan Aerospace Exploration Agency (JAXA)"}]},"item_5_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"1349-113X","subitem_source_identifier_type":"ISSN"}]},"item_5_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_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"富士重工航空宇宙カンパニー"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Aerospace Company, Fuji Heavy Industries"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"荒川, 陽司"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Arakawa, Yoji","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":"64307009.pdf","filesize":[{"value":"929.4 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"64307009.pdf","url":"https://jaxa.repo.nii.ac.jp/record/5225/files/64307009.pdf"},"version_id":"5457be3c-fe39-404e-9807-212775f8d5b0"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"CFRP, Polycyanate, Polyimide, Delamination, Micro crack","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":"conference paper","resourceuri":"http://purl.org/coar/resource_type/c_5794"}]},"item_title":"Influence on polymer matrix composite exposed to space environment","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Influence on polymer matrix composite exposed to space environment","subitem_title_language":"en"}]},"item_type_id":"5","owner":"1","path":["958","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"5225","relation_version_is_last":true,"title":["Influence on polymer matrix composite exposed to space environment"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T08:20:46.728345+00:00"}