{"created":"2023-06-20T15:13:54.267403+00:00","id":43876,"links":{},"metadata":{"_buckets":{"deposit":"2ade9754-825e-496b-809c-69c179ea6e4f"},"_deposit":{"created_by":1,"id":"43876","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"43876"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00043876","sets":["1887:1893","1896:1898:1913:1916"]},"author_link":["466079","466078","466080","466077"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Polynomial Approximation of Theoretical Performance Parameters of Liquid Propellant Combinations"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1976-03","bibliographicIssueDateType":"Issued"},"bibliographicPageStart":"129","bibliographicVolumeNumber":"293","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":"Polynomial approximations in three variables are presented for the calculation of theoretical performance parameters of the liquid rocket propellant combinations of liquid oxygen/liquid hydrogen,liquid oxygen/liquid methane,liquid oxygen/RP-1.liquid fluorine/liquid hydrogen,and nitrogen tetroxide/A-50.The parameters included are the adiabatic flame temperature,characteristic velocity,specific impulse,thrust coefficient,and specific heat ratios for both equilibrium and frozen compositions during expansion.The approximations are valid for wide ranges of mixture ratios,pressures from 10 to 80 atm,and nozzle area expansion ratios,from 10 to 100,or from 50 to 200.Maximum deviation between the approximated and exact theoretical values are shown.Performance parameters given by the polynomial approximations are graphically displayed.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALTM0293000","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-293","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角田支所"},{"subitem_text_value":"航空宇宙技術研究所角田支所"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"毛呂, 明夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"鈴木, 和雄"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"MORO, Akio","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"SUZUKI, Kazuo","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":"naltm00293.pdf","filesize":[{"value":"5.0 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltm00293.pdf","url":"https://jaxa.repo.nii.ac.jp/record/43876/files/naltm00293.pdf"},"version_id":"6642d2b9-883a-46f2-a6ae-10dff4c0a286"}]},"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":"ロケットプロペラントの理論性能: 多項近似式による表示","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"ロケットプロペラントの理論性能: 多項近似式による表示"}]},"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":"43876","relation_version_is_last":true,"title":["ロケットプロペラントの理論性能: 多項近似式による表示"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:06:22.467092+00:00"}