{"created":"2023-06-20T14:36:03.510264+00:00","id":2358,"links":{},"metadata":{"_buckets":{"deposit":"e2cbfd80-98e5-4470-b059-d95acb9d4c54"},"_deposit":{"created_by":1,"id":"2358","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"2358"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00002358","sets":["1887:1893","9:10:309:341"]},"author_link":["5620","5621"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"High Speed Flight Demonstration (HSFD) phase 2"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2005-03-07","bibliographicIssueDateType":"Issued"},"bibliographicVolumeNumber":"JAXA-RR-04-026","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":"高速飛行実証は当機構が再使用型有翼宇宙輸送系研究開発の一環として実施している一連の飛行実験の1つである。計画はフェーズ1とフェーズ2の2つのフェーズから構成される。フェーズ2の主目的は有翼型宇宙輸送システム形状実証機の遷音速空力特性を高精度で取得し、風洞試験および数値流体力学(CFD)の推定精度向上に資することである。フェーズ2の第1回飛行実験は2003年7月にスウェーデンのエスレンジ実験場においてフランス国立宇宙研究センター(CNES)と共同で実施された。飛行はほぼ順調に行われ、マッハ0.8における空力特性データが良好に取得され、また遷音速領域の誘導制御系設計技術の確認が行われたが、最終段階で回収系パラシュートの作動不良が発生し、実証機が破損したため、飛行実験は1回で中断されている。取得されたデータは、将来の再使用型有翼宇宙輸送系の開発に対して大きな貢献をすることが期待されている。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The High-Speed Flight Demonstration (HSFD) project is the latest in a series of flight experiments in a research program into reusable space transportation systems being conducted by JAXA. The project consists of two phases which use sub-scale demonstrators based on the HOPE-X (H-2 Orbiting Plane, Experimental) winged re-entry vehicle configuration. Phase 2 was a drop test from a stratospheric balloon to clarify the transonic aerodynamic characteristics of the HOPE-X configuration and to obtain data to validate wind tunnel tests and Computational Fluid Dynamics (CFD) predictions. The first Phase 2 flight was conducted at the Esrange test site in Sweden in July 2003 in collaboration with Centre National d'Etudes Spatiales of France (CNES). Although the experiment had to be discontinued after an anomaly of the recovery system resulted in damage to the vehicle, flight test data were obtained at Mach 0.8, and fully autonomous flight control technologies for the transonic speed region were demonstrated. The data obtained from the HSFD project are expected to provide essential information for development of future reusable space transportation systems.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0048700000","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-04-026","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":"NAL/NASDA HOPE研究共同チーム HOPE-Xグループ　高速飛行実証班"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"NAL/NASDA HOPE Team High Speed Flight Demonstration Subgroup, HOPE-X Group"}]},"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 Team","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":"48700000.pdf","filesize":[{"value":"17.8 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"48700000.pdf","url":"https://jaxa.repo.nii.ac.jp/record/2358/files/48700000.pdf"},"version_id":"b2d57438-1c41-4b5b-8bfa-2e6fbab013e4"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"再使用型宇宙輸送系","subitem_subject_scheme":"Other"},{"subitem_subject":"有翼再突入機","subitem_subject_scheme":"Other"},{"subitem_subject":"高速飛行実証","subitem_subject_scheme":"Other"},{"subitem_subject":"計算流体力学","subitem_subject_scheme":"Other"},{"subitem_subject":"飛行試験","subitem_subject_scheme":"Other"},{"subitem_subject":"遷音速空力学","subitem_subject_scheme":"Other"},{"subitem_subject":"空力特性","subitem_subject_scheme":"Other"},{"subitem_subject":"風洞試験","subitem_subject_scheme":"Other"},{"subitem_subject":"reusable space transportation system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"winged reentry vehicle","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"High Speed Flight Demonstration","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"computational fluid dynamics","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flight test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"transonic aerodynamics","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic characteristic","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wind tunnel 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":"高速飛行実証フェーズ2","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"高速飛行実証フェーズ2"}]},"item_type_id":"3","owner":"1","path":["341","1893"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"2358","relation_version_is_last":true,"title":["高速飛行実証フェーズ2"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T20:03:00.406656+00:00"}