{"created":"2023-06-20T14:36:25.290879+00:00","id":2733,"links":{},"metadata":{"_buckets":{"deposit":"77f0b486-c0b4-4327-9c4d-78188fcb53e8"},"_deposit":{"created_by":1,"id":"2733","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"2733"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00002733","sets":["1887:1893","9:1090:1311:1325"]},"author_link":["8653","8661","8654","8657","8651","8658","8666","8659","8660","8662","8663","8655","8664","8652","8665","8656","8649","8650"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル(英)","attribute_value_mlt":[{"subitem_alternative_title":"Research on system analysis: Development of concept study program, investigation on design criteria and research on aerodynamic technologies"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2004-10-29","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"8","bibliographicPageStart":"5","bibliographicVolumeNumber":"JAXA-RM-04-009","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構研究開発資料: 平成15年度総合技術研究本部宇宙領域研究成果報告書:輸送系"},{"bibliographic_title":"JAXA Research and Development Memorandum: FY15 Annual Report of Research & Development on Space Technology in the Institute of Space Technology and Aeronautics: Space Transportation System","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録(英)","attribute_value_mlt":[{"subitem_description":"In this research, optimal design, evaluation, and aerodynamic problems for future space transportation systems are conducted. An optimal design program is developed in the research of optimal design and evaluation. The design criteria are also investigated and several types of the concept for the future space transportation systems are designed optically and are evaluated. In the last physical year, a developmental plan of prototype of the design program was established and a part of the prototype was developed. The catalysis and the real gas effect are dealt as aerodynamic problems for the future space transportation systems. In the last physical year, precious data were obtained by the high enthalpy wind tunnel.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0047944002","subitem_description_type":"Other"}]},"item_3_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: JAXA-RM-04-009","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構"}]},"item_3_publisher_9":{"attribute_name":"出版者(英)","attribute_value_mlt":[{"subitem_publisher":"Japan Aerospace Exploration Agency (JAXA)"}]},"item_3_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"1349-1121","subitem_source_identifier_type":"ISSN"}]},"item_3_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AA11983593","subitem_source_identifier_type":"NCID"}]},"item_3_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"},{"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_3_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"},{"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":"鈴木, 広一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"高嵜, 浩一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"南, 吉紀"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"甲斐, 高志"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"佐藤, 哲也"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"小林, 弘明"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"藤田, 和央"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"伊藤, 健"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"黒滝, 卓司"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Suzuki, Hirokazu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Takasaki, Koichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Minami, Yoshinori","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kai, Takashi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sato, Tetsuya","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kobayashi, Hiroaki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Fujita, Kazuhisa","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ito, Takeshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kurotaki, Takuji","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":"2020-01-15"}],"displaytype":"detail","filename":"47944002.pdf","filesize":[{"value":"506.6 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"47944002.pdf","url":"https://jaxa.repo.nii.ac.jp/record/2733/files/47944002.pdf"},"version_id":"056d9c89-adfa-418c-8f24-4b75b617c3d9"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"システム解析","subitem_subject_scheme":"Other"},{"subitem_subject":"宇宙輸送システム","subitem_subject_scheme":"Other"},{"subitem_subject":"空力特性","subitem_subject_scheme":"Other"},{"subitem_subject":"評価","subitem_subject_scheme":"Other"},{"subitem_subject":"高エンタルピ風洞","subitem_subject_scheme":"Other"},{"subitem_subject":"最適設計","subitem_subject_scheme":"Other"},{"subitem_subject":"設計条件","subitem_subject_scheme":"Other"},{"subitem_subject":"再使用宇宙機","subitem_subject_scheme":"Other"},{"subitem_subject":"system analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"space transportation system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic characteristic","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"evaluation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"high enthalpy wind tunnel","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"optimal design","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"design criterion","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"reusable spacecraft","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":"technical report","resourceuri":"http://purl.org/coar/resource_type/c_18gh"}]},"item_title":"システム解析の研究:コンセプトスタディプログラムの開発と設計基準の検討および空力技術に関する研究","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"システム解析の研究:コンセプトスタディプログラムの開発と設計基準の検討および空力技術に関する研究"}]},"item_type_id":"3","owner":"1","path":["1325","1893"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"2733","relation_version_is_last":true,"title":["システム解析の研究:コンセプトスタディプログラムの開発と設計基準の検討および空力技術に関する研究"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T09:16:56.972382+00:00"}