{"created":"2023-06-20T14:54:13.324605+00:00","id":22508,"links":{},"metadata":{"_buckets":{"deposit":"eca2299c-5fba-492e-8cca-16cc4f0a9d33"},"_deposit":{"created_by":1,"id":"22508","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"22508"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00022508","sets":["1887:1888"]},"author_link":["211046","211047","211042","211044","211043","211045"],"item_7_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2014-12-26","bibliographicIssueDateType":"Issued"},"bibliographicIssueNumber":"ists29","bibliographicPageEnd":"Pa_99","bibliographicPageStart":"Pa_91","bibliographicVolumeNumber":"12","bibliographic_titles":[{},{"bibliographic_title":"Transactions of the Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan","bibliographic_titleLang":"en"}]}]},"item_7_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Engine system analysis upon a Rocket-Based Combined Cycle (RBCC) engine for the booster stage of a TSTO launch vehicle was conducted, to evaluate the benefits of hypersonic air-breathing technology upon the performance of the launch vehicle. Hydrocarbon fuel (namely ethanol) and LOx was selected as the propellant of the vehicle to enable easy handling and good packaging of high-density fuel into the airplane-like vehicle shape. First, parametric study on the ramjet-duct portion of the RBCC engine was conducted for fixed embedded rocket engine parameters. Then the rocket engine parameters were varied for the fixed ramjet-duct parameters to attain best performance with a fixed ramjet-duct projected area. The analysis method and primary results are herein reported.","subitem_description_type":"Other"}]},"item_7_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: PA1510007000","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(JSASS)"}]},"item_7_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"The Japan Society for Aeronautical and Space Sciences (JSASS)"}]},"item_7_relation_25":{"attribute_name":"DOI","attribute_value_mlt":[{"subitem_relation_name":[{"subitem_relation_name_text":"info:doi/10.2322/tastj.12.Pa_91"}],"subitem_relation_type_id":{"subitem_relation_type_id_text":"http://dx.doi.org/10.2322/tastj.12.Pa_91","subitem_relation_type_select":"DOI"}}]},"item_7_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"1884-0485","subitem_source_identifier_type":"ISSN"}]},"item_7_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency(JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency(JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency(JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency(JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency(JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency(JAXA)"}]},"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":"Tomioka, Sadatake","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hiraiwa, Tetso","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Saito, Toshihito","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kato, Kanenori","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kodera, Masatoshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tani, Koichiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"RBCC Engines","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"TSTO Launch Vehicle","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"System Analysis","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":"journal article","resourceuri":"http://purl.org/coar/resource_type/c_6501"}]},"item_title":"System Analysis of a Hydrocarbon-Fueled RBCC Engine Applied to a TSTO Launch Vehicle","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"System Analysis of a Hydrocarbon-Fueled RBCC Engine Applied to a TSTO Launch Vehicle","subitem_title_language":"en"}]},"item_type_id":"7","owner":"1","path":["1888"],"pubdate":{"attribute_name":"公開日","attribute_value":"2020-01-22"},"publish_date":"2020-01-22","publish_status":"0","recid":"22508","relation_version_is_last":true,"title":["System Analysis of a Hydrocarbon-Fueled RBCC Engine Applied to a TSTO Launch Vehicle"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T03:19:59.391771+00:00"}