{"created":"2023-06-20T14:48:37.754263+00:00","id":16453,"links":{},"metadata":{"_buckets":{"deposit":"de42539d-ec44-4665-8249-4cae34edc553"},"_deposit":{"created_by":1,"id":"16453","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"16453"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00016453","sets":["1543:1693:1702","1887:1891"]},"author_link":["149355","149354","149352","149350","149356","149353","149357","149351"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Nozzle Characteristic of a Rocket Based Combined Cycle Engine"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2011","bibliographicIssueDateType":"Issued"},"bibliographic_titles":[{"bibliographic_title":"平成22年度宇宙輸送シンポジウム: 講演集録"},{"bibliographic_title":"Proceedings of Space Transportation Symposium: FY2010","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":"平成22年度宇宙輸送シンポジウム(2011年1月20-21日. 宇宙航空研究開発機構宇宙科学研究所), 相模原市, 神奈川県","subitem_description_type":"Other"}]},"item_5_description_15":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）（英）","attribute_value_mlt":[{"subitem_description":"Space Transportation FY2010 (January 20-21, 2011. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency(JAXA)(ISAS)), Sagamihara, Kanagawa Japan","subitem_description_type":"Other"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Aerodynamic tests of small scale rocket combined cycle engine models were carried out to evaluate their performance and at rocket mode operation. In the experiment, thrust force of four models was measured on condition that environmental pressure was set up 4 kPa, rocket chamber pressure ranged up to 3MPa. Nitrogen gas was exhausted as the substitution for the actual rocket gas. As a result, thrust force of four models differentiated and thrust force of rocket combined cycle engine was lower than that of calculated value of conical rocket nozzle. Flow structures of rocket combined cycle engine nozzle were investigated to discuss the performance variation.","subitem_description_type":"Other"}]},"item_5_description_18":{"attribute_name":"内容記述","attribute_value_mlt":[{"subitem_description":"形態: カラー図版あり","subitem_description_type":"Other"},{"subitem_description":"形態: CD-ROM1枚","subitem_description_type":"Other"}]},"item_5_description_19":{"attribute_name":"内容記述（英）","attribute_value_mlt":[{"subitem_description":"Physical characteristics: Original contains color illustrations","subitem_description_type":"Other"},{"subitem_description":"Note: One CD-ROM","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0065073006","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構宇宙科学研究所"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)"}]},"item_5_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AN10324301","subitem_source_identifier_type":"NCID"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"東北大学"},{"subitem_text_value":"宇宙航空研究開発機構角田宇宙センター (JAXA)(KSPC)"},{"subitem_text_value":"宇宙航空研究開発機構角田宇宙センター (JAXA)(KSPC)"},{"subitem_text_value":"宇宙航空研究開発機構角田宇宙センター (JAXA)(KSPC)"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Tohoku University"},{"subitem_text_language":"en","subitem_text_value":"Kakuda Space Center, Japan Aerospace Exploration Agency (JAXA)(KSPC)"},{"subitem_text_language":"en","subitem_text_value":"Kakuda Space Center, Japan Aerospace Exploration Agency (JAXA)(KSPC)"},{"subitem_text_language":"en","subitem_text_value":"Kakuda Space Center, Japan Aerospace Exploration Agency (JAXA)(KSPC)"}]},"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":"久保, 貴裕"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"富岡, 定毅"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"谷, 香一郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"櫻中, 登"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kubo, Takahiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tomioka, Sadatake","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tani, Koichiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sakuranaka, Noboru","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"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":"RBCCエンジンのノズル特性について","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"RBCCエンジンのノズル特性について"}]},"item_type_id":"5","owner":"1","path":["1702","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"16453","relation_version_is_last":true,"title":["RBCCエンジンのノズル特性について"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T04:52:35.425535+00:00"}