{"created":"2023-06-20T14:46:51.471896+00:00","id":14459,"links":{},"metadata":{"_buckets":{"deposit":"34b65eb5-bdca-47c1-a6f3-f95ffc9c7deb"},"_deposit":{"created_by":1,"id":"14459","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"14459"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00014459","sets":["1543:1656:1664","1887:1891"]},"author_link":["132354","132355","132348","132352","132350","132349","132353","132351"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Research on reducing aerodynamic interference at the separation of TSTO type reusable launch vehicle in the air"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2009-12","bibliographicIssueDateType":"Issued"},"bibliographicVolumeNumber":"平成20年度","bibliographic_titles":[{"bibliographic_title":"宇宙航行の力学シンポジウム"},{"bibliographic_title":"Symposium on Flight Mechanics and Astrodynamics","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":"宇宙航行の力学シンポジウム(平成20年度)(2008年12月4～5日、宇宙航空研究開発機構宇宙科学研究本部)","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":"Symposium on Flight Mechanics and Astrodynamics 2008 (December 4-5, 2008. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)), Sagamihara, Kanagawa Japan","subitem_description_type":"Other"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"In this paper, we focused on reduction of reflected shock wave generated between two bodies in hypersonic flow field. To investigate reflected shock wave, we conducted wind tunnel experiments using TSTO models; the one has a rounded nosed circular cylinder configuration, the other has slender body.The slender body has three cross section configuration types(circle, triangle and square). From the results, the slender body having triangle cross section configuration can have weakest reflected shock wave in three TSTO models.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0064729036","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本部"}]},"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)"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"九州大学"},{"subitem_text_value":"九州大学"},{"subitem_text_value":"九州大学"},{"subitem_text_value":"九州大学"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Kyushu University"},{"subitem_text_language":"en","subitem_text_value":"Kyushu University"},{"subitem_text_language":"en","subitem_text_value":"Kyushu University"},{"subitem_text_language":"en","subitem_text_value":"Kyushu University"}]},"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":"植松, 太郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"石田, 拓郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"麻生, 茂"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"谷, 泰寛"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Uematsu, Taro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ishida, Takuro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Aso, Shigeru","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tani, Yasuhiro","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":"TSTO型宇宙往還機の空中分離における空力干渉の低減","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"TSTO型宇宙往還機の空中分離における空力干渉の低減"}]},"item_type_id":"5","owner":"1","path":["1664","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"14459","relation_version_is_last":true,"title":["TSTO型宇宙往還機の空中分離における空力干渉の低減"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T05:34:12.774171+00:00"}