{"created":"2023-06-20T14:36:25.584225+00:00","id":2738,"links":{},"metadata":{"_buckets":{"deposit":"c8c2b251-a6eb-4872-8c56-fcf03a7dba13"},"_deposit":{"created_by":1,"id":"2738","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"2738"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00002738","sets":["1887:1893","9:1090:1311:1325"]},"author_link":["8714","8711","8712","8708","8706","8705","8709","8710","8713","8707"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Numerical analysis to support the development of H-2A launch vehicle and LNG propulsion system"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2004-10-29","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"36","bibliographicPageStart":"31","bibliographicVolumeNumber":"JAXA-RM-04-009","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構研究開発資料: 平成15年度総合技術研究本部宇宙領域研究成果報告書:輸送系"},{"bibliographic_title":"JAXA Research and Development Memorandum: FY15 Annual Report of Research & Development on Space Technology in the Institute of Space Technology and Aeronautics: Space Transportation System","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Numerical simulation has been carried out to support the development of the H-2A launch vehicle and the LNG propulsion system. Numerical results reveal the mixed flow field with hot hydrogen and cold hydrogen in a liquid rocket engine of the H-2A. The local erosion results from the change of the heat flux to the concavity and convexity of the fin in the solid rocket booster (SRB-A). In the LNG propulsion system, it is indicated from the numerical evaluation that the increase of the pressure in the combustion chamber and the decrease in the chemical non-equilibrium loss are required in order to improve the engine performance. The effect of the film cooling inside the igniter is shown and the flame temperature was estimated. The consumption of helium gas at the flight is evaluated by the numerical analysis.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0047944007","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: JAXA-RM-04-009","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Japan Aerospace Exploration Agency (JAXA)"}]},"item_3_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"1349-1121","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":"AA11983593","subitem_source_identifier_type":"NCID"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"宇宙航空研究開発機構 総合技術研究本部"},{"subitem_text_value":"宇宙航空研究開発機構 総合技術研究本部"},{"subitem_text_value":"宇宙航空研究開発機構 総合技術研究本部"},{"subitem_text_value":"宇宙航空研究開発機構 総合技術研究本部"},{"subitem_text_value":"宇宙航空研究開発機構 総合技術研究本部"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"清水, 和弥"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"伊藤, 隆"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"根岸, 秀世"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"清水, 太郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"山西, 伸宏"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Shimizu, Kazuya","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ito, Takashi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Negishi, Hideyo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Shimizu, Taro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yamanishi, Nobuhiro","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":"2020-01-15"}],"displaytype":"detail","filename":"47944007.pdf","filesize":[{"value":"2.0 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"47944007.pdf","url":"https://jaxa.repo.nii.ac.jp/record/2738/files/47944007.pdf"},"version_id":"ac5522d7-c7e2-42b4-bd02-b35ed44e9143"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"数値解析","subitem_subject_scheme":"Other"},{"subitem_subject":"H-2Aロケット","subitem_subject_scheme":"Other"},{"subitem_subject":"固体ロケットブースター","subitem_subject_scheme":"Other"},{"subitem_subject":"LNG","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD","subitem_subject_scheme":"Other"},{"subitem_subject":"燃焼器","subitem_subject_scheme":"Other"},{"subitem_subject":"火炎温度","subitem_subject_scheme":"Other"},{"subitem_subject":"エンジン性能","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"H-2A rocket","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"solid rocket booster","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"LNG","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"combustion chamber","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flame temperature","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"engine performance","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":"technical report","resourceuri":"http://purl.org/coar/resource_type/c_18gh"}]},"item_title":"H-2AロケットおよびLNG推進系の開発を支援するCFD解析","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"H-2AロケットおよびLNG推進系の開発を支援するCFD解析"}]},"item_type_id":"3","owner":"1","path":["1325","1893"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"2738","relation_version_is_last":true,"title":["H-2AロケットおよびLNG推進系の開発を支援するCFD解析"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T09:16:51.381023+00:00"}