{"created":"2023-06-20T14:46:51.604715+00:00","id":14461,"links":{},"metadata":{"_buckets":{"deposit":"11c8e301-588a-407d-b823-8f97f1635991"},"_deposit":{"created_by":1,"id":"14461","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"14461"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00014461","sets":["1543:1656:1664","1887:1891"]},"author_link":["132364","132375","132376","132369","132367","132365","132374","132368","132377","132373","132370","132372","132366","132371"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"A Study on Aerodynamic Characteristics of Reusable Launch Vehicles for Sub-Orbital Flight"}]},"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":"An experimental study on the aerodynamic characteristics of reusable launch vehicles (RLVs) has been conducted. Experimental models were wing-body types which cross sectional configuration of the fuselages were an isosceles right triangle and a square. They have been used in previous experiments and their results show that cross sectional configuration has great impact on longitudinal and lateral aerodynamic characteristics, especially in subsonic and transonic regions with high angle of attacks. For an analysis flight trajectory, many aerodynamic data with various attitudes of the air craft are required. With consideration of reentry by space shuttle, roll angle is one of the most important parameters. So in present study, aerodynamic characteristics with roll angles are acuired and compared. By the results, cross sectional configuration of the fuselage also has effects on them.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0064729038","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"},{"subitem_text_value":"九州大学"},{"subitem_text_value":"宇宙航空研究開発機構宇宙科学研究本部"},{"subitem_text_value":"宇宙航空研究開発機構"}]},"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"},{"subitem_text_language":"en","subitem_text_value":"Kyushu University"},{"subitem_text_language":"en","subitem_text_value":"Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency (JAXA)"}]},"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":"石田, 拓郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"麻生, 茂"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"谷, 泰寛"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"森下, 和彦"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"植松, 太郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"稲谷, 芳文"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"入門, 朋子"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ishida, Takuro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Aso, Shigeru","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tani, Yasuhiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Morishita, Kazuhiko","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Uematsu, Taro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Inatani, Yoshifumi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Irikado, Tomoko","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"Wing body","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"cross sectional configuration","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic characteristics","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Roll angle","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":"弾道飛行に向けた往還機形状の空力特性に関する研究","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"弾道飛行に向けた往還機形状の空力特性に関する研究"}]},"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":"14461","relation_version_is_last":true,"title":["弾道飛行に向けた往還機形状の空力特性に関する研究"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T05:34:11.882235+00:00"}