{"created":"2023-06-20T15:04:02.658951+00:00","id":33254,"links":{},"metadata":{"_buckets":{"deposit":"fb17a4d1-a24f-4491-a2c6-03cda6376416"},"_deposit":{"created_by":1,"id":"33254","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"33254"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00033254","sets":["1887:1890","1896:1898:1899:1991"]},"author_link":["415823","415824"],"item_9_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2003-03","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"244","bibliographicPageStart":"233","bibliographicVolumeNumber":"17","bibliographic_titles":[{},{"bibliographic_title":"The Institute of Space and Astronautical Science report. S.P. : Aerodynamics, Thermophysics, Thermal Protection, Flight System Analysis and Design of Asteroid Sample Return Capsule","bibliographic_titleLang":"en"}]}]},"item_9_description_17":{"attribute_name":"抄録(英)","attribute_value_mlt":[{"subitem_description":"An integrated numerical method to obtain trajectory-based aerodynamic heating environment for entry probe vehicles with ablation is briefly described. In this method, a thermochemical nonequilibrium CFD code is loosely coupled with an ablation module along the entry trajectory. Radiative heating is estimated by the use of multi-band radiation module. The effect of earlier turbulent transition of the boundary layer due to ablation product gas is included. Calculated results for MUSES-C sample return capsule are shown and are compared with the results of existing analysis.","subitem_description_type":"Other"}]},"item_9_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: SA0200027000","subitem_description_type":"Other"}]},"item_9_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙科学研究所"}]},"item_9_publisher_9":{"attribute_name":"出版者(英)","attribute_value_mlt":[{"subitem_publisher":"Institute of Space and Astronautical Science"}]},"item_9_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0288-433X","subitem_source_identifier_type":"ISSN"}]},"item_9_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AA10455137","subitem_source_identifier_type":"NCID"}]},"item_9_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"東北大学大学院 工学研究科 航空宇宙工学専攻"}]},"item_9_text_7":{"attribute_name":"著者所属(英)","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Department of Aeronautics and Space Engineering, Tohoku University"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"澤田, 恵介"}],"nameIdentifiers":[{"nameIdentifier":"415823","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Sawada, Keisuke","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"415824","nameIdentifierScheme":"WEKO"}]}]},"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":"SA0200027.pdf","filesize":[{"value":"3.5 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"SA0200027.pdf","url":"https://jaxa.repo.nii.ac.jp/record/33254/files/SA0200027.pdf"},"version_id":"4f314e3f-e84b-4b69-a80d-28b56950cb5b"}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"eng"}]},"item_resource_type":{"attribute_name":"資源タイプ","attribute_value_mlt":[{"resourcetype":"departmental bulletin paper","resourceuri":"http://purl.org/coar/resource_type/c_6501"}]},"item_title":"An Integrated Numerical Method for Predicting Aerodynamic Heating Environment for MUSES-C Entry Capsule with Ablation","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"An Integrated Numerical Method for Predicting Aerodynamic Heating Environment for MUSES-C Entry Capsule with Ablation","subitem_title_language":"en"}]},"item_type_id":"9","owner":"1","path":["1890","1991"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"33254","relation_version_is_last":true,"title":["An Integrated Numerical Method for Predicting Aerodynamic Heating Environment for MUSES-C Entry Capsule with Ablation"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T00:11:54.588791+00:00"}