{"created":"2023-06-20T15:11:31.745125+00:00","id":41208,"links":{},"metadata":{"_buckets":{"deposit":"163be9a9-cdde-4ea3-8da7-d0c485252b5a"},"_deposit":{"created_by":1,"id":"41208","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"41208"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00041208","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["451176","451177"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"A quiet STOL research aircraft development program"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1994-01","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"135","bibliographicPageStart":"1","bibliographicVolumeNumber":"1223","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所報告"},{"bibliographic_title":"Technical Report of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"この報告書は航空宇宙技術研究所が開発設計したSTOL実験機「飛鳥」の研究開発計画の全容について概説する。飛鳥は1985年10月28日に初飛行を行った。1977-1985の8年間におよぶ開発経過報告には航空機機体、システムと多数の開発試験が含まれる。飛鳥は航空自衛隊の中型貨物輸送機シリーズであるC-1機の改良機で川崎重工が開発試作した。機体は新しく設計され、C-1機の双発エンジンはSTOL運用のパワードリフトを確保できる上面吹き出し(USB)方式を採用するため、4発のFJR710/600Sファンジェットエンジンに取り替えられた。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"This report presents a general account of a program undertaken by the National Aerospace Laboratory to develop a STOL reserach aircraft, designated ASKA. The ASKA made its first flight on October 28, 1985. Descriptions of the development over the 8 years from 1977 to 1985 are included along with descriptions of the aircraft and its systems, and various development tests. The ASKA is a modified C-1 medium-sized troop and freight transport, manufactured by Kawasaki Heavy Industries for the Air Self-Defence Force. The airframe was made anew and the two engines of C-1 were replaced with four FJR710/600S fan-jet engines arranged as in upper surface blowing system to provide powered lift for STOL operations.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0004238000","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 TR-1223","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":"0389-4010","subitem_source_identifier_type":"ISSN"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"航空宇宙技術研究所"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"STOLプロジェクト推進本部機体技術開発室"}],"nameIdentifiers":[{"nameIdentifier":"451176","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Aircraft, D. S.  STOL Aircraft Proj. G.","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"451177","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":"2020-01-27"}],"displaytype":"detail","filename":"naltr01223.pdf","filesize":[{"value":"9.9 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr01223.pdf","url":"https://jaxa.repo.nii.ac.jp/record/41208/files/naltr01223.pdf"},"version_id":"39be6a7c-4a8e-4b6a-8887-77afef7a121f"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"STOL機","subitem_subject_scheme":"Other"},{"subitem_subject":"航空機開発","subitem_subject_scheme":"Other"},{"subitem_subject":"実験機","subitem_subject_scheme":"Other"},{"subitem_subject":"高揚力装置","subitem_subject_scheme":"Other"},{"subitem_subject":"USBシステム","subitem_subject_scheme":"Other"},{"subitem_subject":"ファンジェットエンジン","subitem_subject_scheme":"Other"},{"subitem_subject":"四発航空機","subitem_subject_scheme":"Other"},{"subitem_subject":"ナセル","subitem_subject_scheme":"Other"},{"subitem_subject":"フラップ","subitem_subject_scheme":"Other"},{"subitem_subject":"境界層制御","subitem_subject_scheme":"Other"},{"subitem_subject":"騒音抑制","subitem_subject_scheme":"Other"},{"subitem_subject":"ノズル","subitem_subject_scheme":"Other"},{"subitem_subject":"操縦翼面","subitem_subject_scheme":"Other"},{"subitem_subject":"風洞試験","subitem_subject_scheme":"Other"},{"subitem_subject":"飛行シミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"STOL aircraft","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"technology development of aircraft","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"research aircraft","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"high lift device","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"USB system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"fan jet engine","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"four engines aircraft","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"nacelle","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flap","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"boundary layer control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"noise control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"USB nozzle","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"control surface","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wind tunnel test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flight simulation","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":"低騒音STOL実験機機体開発総合報告書","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"低騒音STOL実験機機体開発総合報告書"}]},"item_type_id":"3","owner":"1","path":["1893","1917"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"41208","relation_version_is_last":true,"title":["低騒音STOL実験機機体開発総合報告書"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T19:12:05.217863+00:00"}