{"created":"2023-06-20T14:58:15.243636+00:00","id":27078,"links":{},"metadata":{"_buckets":{"deposit":"d353eda7-464c-4718-b3fd-0f2d0ce9c887"},"_deposit":{"created_by":1,"id":"27078","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"27078"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00027078","sets":["1887:1888"]},"author_link":["319880","319882","319879","319881"],"item_7_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Combustion Characteristics of a Swirling LOX Type Hybrid Rocket Engine"}]},"item_7_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2006","bibliographicIssueDateType":"Issued"},"bibliographicIssueNumber":"629","bibliographicPageEnd":"249","bibliographicPageStart":"242","bibliographicVolumeNumber":"54","bibliographic_titles":[{"bibliographic_title":"日本航空宇宙学会論文集"},{"bibliographic_title":"Journal of the Japan Society for Aeronautical and Space Sciences","bibliographic_titleLang":"en"}]}]},"item_7_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: SA1003782000","subitem_description_type":"Other"}]},"item_7_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"日本航空宇宙学会"}]},"item_7_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"The Japan Society for Aeronautical and Space Sciences"}]},"item_7_relation_25":{"attribute_name":"DOI","attribute_value_mlt":[{"subitem_relation_name":[{"subitem_relation_name_text":"info:doi/10.2322/jjsass.54.242"}],"subitem_relation_type_id":{"subitem_relation_type_id_text":"http://dx.doi.org/10.2322/jjsass.54.242","subitem_relation_type_select":"DOI"}}]},"item_7_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"1344-6460","subitem_source_identifier_type":"ISSN"}]},"item_7_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"東京都立科学技術大学大学院工学研究科"},{"subitem_text_value":"東京都立科学技術大学大学院工学研究科"}]},"item_7_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Tokyo Metropoliran Institute of Technology"},{"subitem_text_language":"en","subitem_text_value":"Tokyo Metropoliran Institute of Technology"}]},"item_access_right":{"attribute_name":"アクセス権","attribute_value_mlt":[{"subitem_access_right":"metadata only access","subitem_access_right_uri":"http://purl.org/coar/access_right/c_14cb"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"北川, 幸樹"}],"nameIdentifiers":[{"nameIdentifier":"319879","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"湯浅, 三郎"}],"nameIdentifiers":[{"nameIdentifier":"319880","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Kitagawa, Koki","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"319881","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Yuasa, Saburo","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"319882","nameIdentifierScheme":"WEKO"}]}]},"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":"journal article","resourceuri":"http://purl.org/coar/resource_type/c_6501"}]},"item_title":"液体酸素旋回型ハイブリッドロケットエンジンの燃焼特性","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"液体酸素旋回型ハイブリッドロケットエンジンの燃焼特性"}]},"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":"27078","relation_version_is_last":true,"title":["液体酸素旋回型ハイブリッドロケットエンジンの燃焼特性"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T02:10:00.862844+00:00"}