{"created":"2023-06-20T14:36:10.224664+00:00","id":2482,"links":{},"metadata":{"_buckets":{"deposit":"13acc908-75a8-4125-9b13-232a6270a933"},"_deposit":{"created_by":1,"id":"2482","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"2482"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00002482","sets":["1887:1893","9:1090:1137:1145"]},"author_link":["6714","6716","6717","6719","6715","6718"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Required Specifications of an Electric Propulsion System Based on Flight Test Using a Motor Glider"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2015-03-13","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"7","bibliographicPageStart":"1","bibliographicVolumeNumber":"JAXA-RM-14-005","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構研究開発資料"},{"bibliographic_title":"JAXA Research and Development Memorandum","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The Japan Aerospace Exploration Agency (JAXA) is planning flight demonstration of an electric propulsion system which is equipped with new functions using a motor glider on 2014. The new electric propulsion system will be converted form the existing reciprocating engine of motor glider and be installed with motor glider. Prior to the development of the electric propulsion system, flight tests are conducted to acquire performance of JA07TTCECO with original propulsion system. Based on these flight test result, determined specifications of the electric propulsion system for replacing original system are as follows, 1)Take-off Power(max 150s):60kW, 2)Maximum Propeller Speed:2300rpm, 3)Maximum Ambient Temperature:40 C, 4)Maximum Continuous Power:32kW.","subitem_description_type":"Other"}]},"item_3_description_18":{"attribute_name":"内容記述","attribute_value_mlt":[{"subitem_description":"形態: カラー図版あり","subitem_description_type":"Other"}]},"item_3_description_19":{"attribute_name":"内容記述（英）","attribute_value_mlt":[{"subitem_description":"Physical characteristics: Original contains color illustrations","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA1530008000","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-14-005","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(JAXA)"}]},"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航空本部航空技術実証研究開発室（JAXA)"},{"subitem_text_value":"宇宙航空研究開発機構航空本部航空技術実証研究開発室（JAXA)"},{"subitem_text_value":"宇宙航空研究開発機構航空本部航空技術実証研究開発室（JAXA)"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Technology Demonstration Research Office, Institute of Aeronautical Technology, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Technology Demonstration Research Office, Institute of Aeronautical Technology, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Technology Demonstration Research Office, Institute of Aeronautical Technology, Japan Aerospace Exploration Agency (JAXA)"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"小林, 宙"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"飯島, 朋子"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"西沢, 啓"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kobayashi, Hiroshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Iijima, Tomoko","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nishizawa, Akira","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":"AA1530008000.pdf","filesize":[{"value":"1.3 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"AA1530008000.pdf","url":"https://jaxa.repo.nii.ac.jp/record/2482/files/AA1530008000.pdf"},"version_id":"39be9da2-2c70-460e-84a9-f5a7f538bb96"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"electric propulsion system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flight test","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":"原型機飛行試験による航空機用電動推進系の仕様検討","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"原型機飛行試験による航空機用電動推進系の仕様検討"}]},"item_type_id":"3","owner":"1","path":["1145","1893"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-04-09"},"publish_date":"2015-04-09","publish_status":"0","recid":"2482","relation_version_is_last":true,"title":["原型機飛行試験による航空機用電動推進系の仕様検討"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T09:21:50.414028+00:00"}