{"created":"2023-06-20T15:13:54.400907+00:00","id":43878,"links":{},"metadata":{"_buckets":{"deposit":"ea8bef9f-7f7a-4d2a-8e67-a3cb8feadf57"},"_deposit":{"created_by":1,"id":"43878","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"43878"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00043878","sets":["1887:1893","1896:1898:1913:1916"]},"author_link":["466087","466086","466090","466089","466085","466088"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Graphs Showing Characteristic of Liquid Rocket Propellants Performance"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1975-03","bibliographicIssueDateType":"Issued"},"bibliographicPageStart":"64","bibliographicVolumeNumber":"295","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所資料"},{"bibliographic_title":"Technical Memorandum of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Graphs showing characteristic curves of rocket propellants performance (Isp,C*,T,etc.),are available to assist the design or investigation of rocket engines.As the most practical or most used liquid rocket propellants,four propellants(LOX-LH2,N204-A・50,LOX-RP・1,LOX-C2H5OH)were selected,and the extent of practical usage performance of the propellants were computed(ε,Pc,O/F).The results are shown in the respective graphs.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALTM0295000","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: NAL TM-295","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"航空宇宙技術研究所"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"National Aerospace Laboratory(NAL)"}]},"item_3_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0452-2982","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":"AN00314334","subitem_source_identifier_type":"NCID"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"航空宇宙技術研究所宇宙研究グループ"},{"subitem_text_value":"航空宇宙技術研究所宇宙研究グループ"},{"subitem_text_value":"航空宇宙技術研究所宇宙研究グループ"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"楢崎, 哲二"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"荻原, 裟千男"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"吉原, 正一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"NARASAKI, Tetsuji","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"OGIWARA, Sachio","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"YOSHIWARA, Shoichi","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":"2020-01-28"}],"displaytype":"detail","filename":"naltm00295.pdf","filesize":[{"value":"1.9 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltm00295.pdf","url":"https://jaxa.repo.nii.ac.jp/record/43878/files/naltm00295.pdf"},"version_id":"757693f9-8960-42af-abab-653b9e91a410"}]},"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":"液体ロケット推進薬の性能特性図","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"液体ロケット推進薬の性能特性図"}]},"item_type_id":"3","owner":"1","path":["1893","1916"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"43878","relation_version_is_last":true,"title":["液体ロケット推進薬の性能特性図"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:06:20.009325+00:00"}