{"created":"2023-06-20T14:36:02.889082+00:00","id":2345,"links":{},"metadata":{"_buckets":{"deposit":"afc769cf-6d31-4f0d-b3d6-d9f48f6d9ca5"},"_deposit":{"created_by":1,"id":"2345","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"2345"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00002345","sets":["1887:1893","9:10:309:334"]},"author_link":["5522","5523"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Ground-to-stratosphere flight test report: Ascent simulation of the test vehicle"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2005-09-07","bibliographicIssueDateType":"Issued"},"bibliographicVolumeNumber":"JAXA-RR-04-033","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構研究開発報告"},{"bibliographic_title":"JAXA Research and Development Report","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"成層圏滞空飛行試験では、飛行船の浮力による上昇飛行を予測するためのシミュレーションモデルを開発し、これを試験機の設計・運用方法の検講と、飛行試験における浮力設定および飛行経路予測に供した。木稿では、浮力によって上昇する飛行船の基本的な特性を示すとともに、シミュレーションモデルの概略を述べ、飛行試験結果とシミュレーションとの比較を行う。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"In the Ground-To-Stratosphere flight test program, a simulation model was developed to calculate the ascend flight of an airship and utilized for buoyancy management and flight path estimation as well as for the vehicle design. This paper presents fundamental characteristics of an airship ascending by buoyancy, outline of the simulation model, and a comparison between the flight data and the simulation.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0048701000","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-RR-04-033","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":"1349-1113","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":"AA1192675X","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 航空利用技術開発センター"}]},"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 Aeronautics Application Technology Center"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"原田, 賢哉"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Harada, Kenya","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":"48701000.pdf","filesize":[{"value":"3.3 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"48701000.pdf","url":"https://jaxa.repo.nii.ac.jp/record/2345/files/48701000.pdf"},"version_id":"38adcebb-0615-4445-9f06-1aa59297b354"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"飛行船","subitem_subject_scheme":"Other"},{"subitem_subject":"成層圏プラットフォーム","subitem_subject_scheme":"Other"},{"subitem_subject":"成層圏","subitem_subject_scheme":"Other"},{"subitem_subject":"飛行シミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"数値シミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"浮力","subitem_subject_scheme":"Other"},{"subitem_subject":"温度分布","subitem_subject_scheme":"Other"},{"subitem_subject":"上昇速度","subitem_subject_scheme":"Other"},{"subitem_subject":"airship","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"stratospheric platform","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"stratosphere","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flight simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"buoyancy","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"temperature distribution","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"ascent velocity","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":"成層圏滞空飛行試験成果報告書:試験機の上昇シミュレーション","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"成層圏滞空飛行試験成果報告書:試験機の上昇シミュレーション"}]},"item_type_id":"3","owner":"1","path":["334","1893"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"2345","relation_version_is_last":true,"title":["成層圏滞空飛行試験成果報告書:試験機の上昇シミュレーション"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T09:24:11.132708+00:00"}