{"created":"2023-06-20T15:11:28.452567+00:00","id":41138,"links":{},"metadata":{"_buckets":{"deposit":"2a5cb69c-b066-4de0-b75d-4bc80ff44878"},"_deposit":{"created_by":1,"id":"41138","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"41138"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00041138","sets":["1887:1893","1896:1898:1913:1916"]},"author_link":["450726","450727"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Basic concept for the preliminary design of the hypersonic flight experiment, HYFLEX"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1995-01","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"28","bibliographicPageStart":"1","bibliographicVolumeNumber":"675","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所資料"},{"bibliographic_title":"Technical Memorandum of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"我が国初の揚力機の極超音速飛行実験として、HYFLEX(Hypersonic Flight Experiment)計画が、航技研と宇宙開発事業団の共同プロジェクトとして進められている。本資料は、概念設計/予備設計などの成果に基づいて設定した「基本設計初期構想」について概説したものである。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"A hypersonic flight experiment of a gliding vehicle called HYFLEX (Hypersonic Flight Experiment) is being prepared as a cooperative project by NAL (National Aerospace Laboratory) and The National Space Development Agency of Japan. The concept of the HYFLEX, defined as the base of preliminary design, is introduced in the present paper.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0004159000","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: NAL TM-675","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"航空宇宙技術研究所"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"National Aerospace Laboratory (NAL)"}]},"item_3_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0452-2982","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":"AN00314334","subitem_source_identifier_type":"NCID"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"NAL/NASDA HOPE研究共同チーム、HYFLEXサブグループ"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"HYFLEX Sub-Group, NAL/NASDA HOPE Joint Team"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"NAL/NASDA HOPE研究共同チーム"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"NAL/NASDA HOPE Joint 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MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltm00675.pdf","url":"https://jaxa.repo.nii.ac.jp/record/41138/files/naltm00675.pdf"},"version_id":"4a9db94d-7677-4255-b84e-ad7de3ee054c"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"極超音速飛行実験","subitem_subject_scheme":"Other"},{"subitem_subject":"HYFLEX","subitem_subject_scheme":"Other"},{"subitem_subject":"基本設計","subitem_subject_scheme":"Other"},{"subitem_subject":"初期構想","subitem_subject_scheme":"Other"},{"subitem_subject":"航空宇宙技術研究所","subitem_subject_scheme":"Other"},{"subitem_subject":"宇宙開発事業団","subitem_subject_scheme":"Other"},{"subitem_subject":"概念設計","subitem_subject_scheme":"Other"},{"subitem_subject":"予備設計","subitem_subject_scheme":"Other"},{"subitem_subject":"実験計画","subitem_subject_scheme":"Other"},{"subitem_subject":"実験機システム","subitem_subject_scheme":"Other"},{"subitem_subject":"飛行解析","subitem_subject_scheme":"Other"},{"subitem_subject":"空力設計","subitem_subject_scheme":"Other"},{"subitem_subject":"推進系設計","subitem_subject_scheme":"Other"},{"subitem_subject":"滑走車","subitem_subject_scheme":"Other"},{"subitem_subject":"hypersonic flight experiment","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"HYFLEX","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"basic design","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"initial concept","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"National Aerospace Laboratory","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"National Space Development Agency","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"conceptual design","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"preliminary design","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"experiment plan","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"experiment aircraft system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flight analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic design","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"propulsion system design","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"gliding vehicle","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 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