{"created":"2023-06-20T15:09:05.982543+00:00","id":38607,"links":{},"metadata":{"_buckets":{"deposit":"86db0a22-e8f4-4a56-ada7-3787f6adf9ad"},"_deposit":{"created_by":1,"id":"38607","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"38607"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00038607","sets":["1887:1891"]},"author_link":["434892","434895","434893","434891","434894","434890","434897","434896"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Research Activity on a RBCC Engine System"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2013-10","bibliographicIssueDateType":"Issued"},"bibliographic_titles":[{"bibliographic_title":"第57回宇宙科学技術連合講演会講演集"},{"bibliographic_title":"Proceedings of 57th Space Sciences and Technology Conference","bibliographic_titleLang":"en"}]}]},"item_5_description_14":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）","attribute_value_mlt":[{"subitem_description":"第57回宇宙科学技術連合講演会（2013年10月9日-11日. 米子コンベンションセンター（BiG SHiP）), 米子市, 鳥取県","subitem_description_type":"Other"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Feasibility study on future transportation vehicle (termed as reference system) is undergoing at Japan AerospaceExploration Agency, setting the target on reusable, manned launch vehicles. Two-staged vehicle to low earth orbit is thefinal target of the current study, with hydrocarbon fuel (namely ethanol) in scope for easy and low-cost operation, andfiner system packaging due to high density. To compensate the Isp loss associated with usage of hydrocarbon fuel,airbreathing technology is fitted to the booster stage of the vehicle, i.e., application of a RBCC (Rocket Based CombinedCycle) engine. This engine is to embed rocket engines within a ramjet-duct, with various operation modes according toflight speed. Research activity has been conducted at JAXA to establish design methodology of this engine system withan emphasis on aerodynamic design with hydrogen as its fuel. Status of the research activity is herein reported.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AC1400023000","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: JSASS-2013-4276","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"日本航空宇宙学会(JSASS)"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"The Japan Society for Aeronautical and Space Sciences(JSASS)"}]},"item_5_rights_28":{"attribute_name":"権利","attribute_value_mlt":[{"subitem_rights":"(C)2013 一般社団法人 日本航空宇宙学会"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"宇宙航空研究開発機構(JAXA)"},{"subitem_text_value":"宇宙航空研究開発機構(JAXA)"},{"subitem_text_value":"宇宙航空研究開発機構(JAXA)"},{"subitem_text_value":"宇宙航空研究開発機構(JAXA)"}]},"item_5_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)"}]},"item_5_version_type_30":{"attribute_name":"著者版フラグ","attribute_value_mlt":[{"subitem_version_resource":"http://purl.org/coar/version/c_970fb48d4fbd8a85","subitem_version_type":"VoR"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"植田, 修一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"加藤, 周徳"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"長谷川, 進"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"平岩, 徹夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ueda, Shuuichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kato, Kanenori","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hasegawa, Susumu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hiraiwa, Tetsuo","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":"2020-01-24"}],"displaytype":"detail","filename":"AC1400023.pdf","filesize":[{"value":"2.4 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"AC1400023.pdf","url":"https://jaxa.repo.nii.ac.jp/record/38607/files/AC1400023.pdf"},"version_id":"083f3c69-8dfb-485d-8955-a0df90bcc448"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"Space Transportation; Rocket-Based Combined Cycle Engine","subitem_subject_language":"en","subitem_subject_scheme":"Other"}]},"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":"conference paper","resourceuri":"http://purl.org/coar/resource_type/c_5794"}]},"item_title":"ロケット複合エンジンシステムにかかる技術研究状況について","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"ロケット複合エンジンシステムにかかる技術研究状況について"}]},"item_type_id":"5","owner":"1","path":["1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"38607","relation_version_is_last":true,"title":["ロケット複合エンジンシステムにかかる技術研究状況について"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:38:32.298071+00:00"}