{"created":"2023-06-20T14:49:30.409329+00:00","id":17369,"links":{},"metadata":{"_buckets":{"deposit":"23e1c595-b12c-4e91-9706-7339ed638b36"},"_deposit":{"created_by":1,"id":"17369","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"17369"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00017369","sets":["1543:1693:1710","1887:1891"]},"author_link":["157624","157623","157620","157625","157622","157621"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Development of accurate optimization method of the TSTO spaceplane: New aerodynamics model using CFD method"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2003-04","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"136","bibliographicPageStart":"133","bibliographic_titles":[{"bibliographic_title":"宇宙輸送シンポジウム　平成14年度"},{"bibliographic_title":"Proceedings of Space Transportation Symposium FY2002","bibliographic_titleLang":"en"}]}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"A new aerodynamics model is developed using the data obtained by accurate CFD simulations, as one of the components for the total optimization of TSTO systems. The developed component is integrated into the optimization program, and the influence of the new component is evaluated. Strong aerodynamic interaction occurs between the Booster and the Orbiter in the CFD simulations, and it indicates the importance of the accurate aerodynamics model. The optimization using the new aerodynamics model results in the heavier gross take-off weight compared to the result using the conventional aerodynamics model.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0045426033","subitem_description_type":"Other"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"東京大学 大学院工学系研究科"},{"subitem_text_value":"宇宙科学研究所"},{"subitem_text_value":"宇宙科学研究所"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"University of Tokyo Graduate School of Engineering"},{"subitem_text_language":"en","subitem_text_value":"Institute of Space and Astronautical Science"},{"subitem_text_language":"en","subitem_text_value":"Institute of Space and Astronautical Science"}]},"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":"下山, 幸治"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"藤井, 孝藏"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"小林, 弘明"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Shimoyama, Koji","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Fujii, Kozo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kobayashi, Hiroaki","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"TSTOスペースプレーン","subitem_subject_scheme":"Other"},{"subitem_subject":"空力係数","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD","subitem_subject_scheme":"Other"},{"subitem_subject":"Baldwin-Lomax乱流モデル","subitem_subject_scheme":"Other"},{"subitem_subject":"軌道制御","subitem_subject_scheme":"Other"},{"subitem_subject":"ブースターロケット","subitem_subject_scheme":"Other"},{"subitem_subject":"軌道機","subitem_subject_scheme":"Other"},{"subitem_subject":"研究開発","subitem_subject_scheme":"Other"},{"subitem_subject":"TSTO spaceplane","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic coefficient","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Baldwin-Lomax turbulence model","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"trajectory control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"booster rocket","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"orbiter","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"research and development","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":"TSTO統合最適設計の高度化:CFD解析によるTSTO空力評価モデルの構築","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"TSTO統合最適設計の高度化:CFD解析によるTSTO空力評価モデルの構築"}]},"item_type_id":"5","owner":"1","path":["1710","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"17369","relation_version_is_last":true,"title":["TSTO統合最適設計の高度化:CFD解析によるTSTO空力評価モデルの構築"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T04:39:13.004549+00:00"}