{"created":"2023-06-20T14:39:25.304524+00:00","id":6169,"links":{},"metadata":{"_buckets":{"deposit":"92a5f401-3040-4cba-b548-e45b0da4c136"},"_deposit":{"created_by":1,"id":"6169","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"6169"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00006169","sets":["1887:1891","9:789:1031:1052"]},"author_link":["30903","30908","30906","30909","30904","30910","30905","30902","30901","30907"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"The application of CFD in rocket engine development"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2006-02-28","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"220","bibliographicPageStart":"215","bibliographicVolumeNumber":"JAXA-SP-05-017","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構特別資料: 航空宇宙数値シミュレーション技術シンポジウム2005論文集"},{"bibliographic_title":"JAXA Special Publication: Proceedings of Aerospace Numerical Simulation Symposium 2005","bibliographic_titleLang":"en"}]}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The numerical simulations carried out for the rocket engine development at the Japan Aerospace Exploration Agency is presented. Although numerical simulations played a major role in the return to flight of the H-2A launch vehicle, the basic design of the rocket was initiated more than a decade ago. Back then, CFD was gradually spreading from the academia to the industrial society, but not to a revel where CFD was actively used as a design tool. Now, the remarkable progress in the performance of high-end computers and the advances in the simulation techniques have made CFD an indispensable tool for designing. In this paper, the research activities of developing numerical simulators of rocket engines and some numerical analysis carried out for the return to flight program of the H-2A launch vehicle are presented. Results show that CFD is beginning to expand its role as a tool for developing rocket engines.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0049212036","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: JAXA-SP-05-017","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"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Japan Aerospace Exploration Agency (JAXA)"}]},"item_5_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"1349-113X","subitem_source_identifier_type":"ISSN"}]},"item_5_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AA11984031","subitem_source_identifier_type":"NCID"}]},"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 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_5_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":"山西, 伸宏"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"清水, 太郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"根岸, 秀世"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"清水, 和弥"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"谷, 直樹"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yamanishi, Nobuhiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Shimizu, Taro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Negishi, Hideyo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Shimizu, Kazuya","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tani, Naoki","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":"2020-01-16"}],"displaytype":"detail","filename":"49212036.pdf","filesize":[{"value":"3.0 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"49212036.pdf","url":"https://jaxa.repo.nii.ac.jp/record/6169/files/49212036.pdf"},"version_id":"aed74590-32b1-4cb2-95af-4fdddc3798d8"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"計算流体力学","subitem_subject_scheme":"Other"},{"subitem_subject":"ロケットエンジン","subitem_subject_scheme":"Other"},{"subitem_subject":"日本の宇宙プログラム","subitem_subject_scheme":"Other"},{"subitem_subject":"研究開発","subitem_subject_scheme":"Other"},{"subitem_subject":"ロケットエンジン設計","subitem_subject_scheme":"Other"},{"subitem_subject":"設計ツール","subitem_subject_scheme":"Other"},{"subitem_subject":"H-2Aロケットエンジン","subitem_subject_scheme":"Other"},{"subitem_subject":"シミュレータ","subitem_subject_scheme":"Other"},{"subitem_subject":"ロケットエンジンシステム","subitem_subject_scheme":"Other"},{"subitem_subject":"ロケットエンジン供給システム","subitem_subject_scheme":"Other"},{"subitem_subject":"燃焼システム","subitem_subject_scheme":"Other"},{"subitem_subject":"computational fluid dynamics","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"rocket engine","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Japanese space program","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"research and development","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"rocket engine design","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"design tool","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"H-2A rocket engine","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"simulator","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"rocket engine system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"rocket engine feeding system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"combustion system","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":"ロケットエンジン開発におけるCFD","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"ロケットエンジン開発におけるCFD"}]},"item_type_id":"5","owner":"1","path":["1052","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"6169","relation_version_is_last":true,"title":["ロケットエンジン開発におけるCFD"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T08:00:52.327847+00:00"}