{"created":"2023-06-20T15:10:13.610437+00:00","id":39820,"links":{},"metadata":{"_buckets":{"deposit":"6a0ab38e-b57e-42f2-bde1-0701225d52b1"},"_deposit":{"created_by":1,"id":"39820","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"39820"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00039820","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["444658","444661","444656","444659","444660","444657"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Suspending wind-tunnel test for the ALFLEX vehicle"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1996-09","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"25","bibliographicPageStart":"1","bibliographicVolumeNumber":"1306","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":"無人有翼宇宙往還機(HOPE)の研究の一環として進めている小型自動着陸実験(ALFLEX)の懸吊風洞実験を実施した。これはALFLEX実験機の40％縮尺模型を用いて実験機の懸吊飛行状態を風洞の中で模擬するものであり、制御系を含む懸吊飛行システムの設計確認と、制御系設計のための空力特性の推定を目的として実施したものである。試験の結果、一部の構成要素の問題点が明らかになり、改修が行われることになったが、システムとしてはほぼ設計通りの機能を発揮すること、推定された空力特性は設計に使用した空力モデルと大きな差がないことが確認された。これらの結果を反映して実飛行試験の計画策定が行われることとなった。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"A suspending wind-tunnel test for the Automatic Landing Flight Experiment (ALFLEX) was conducted as a part of the research on an unmanned winged reentry vehicle (HOPE). The suspending flight was simulated in the wind-tunnel using a 40 percent scaled model of the ALFLEX vehicle to validate the design of the suspending system and to identify the aerodynamic characteristics of the vehicle for designing a control system. As a result, problems of some elements of the system are identified and a counterplan is considered. It is concluded that the system works well except for these problems, and that there is not much difference between the actual aerodynamic characteristics and the predicted ones used in designing the vehicle. The flight test plan of ALFLEX is then fixed based on these results.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0000683000","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-1306","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 動的風洞試験グループ"},{"subitem_text_value":"航空宇宙技術研究所 ALFLEXサブグループ"},{"subitem_text_value":"宇宙開発事業団 ALFLEX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":"Dynamic Wind-Tunnel Test Group"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory ALFLEX Sub Group"},{"subitem_text_language":"en","subitem_text_value":"National Space Development Agency of Japan ALFLEX Sub Group"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"動的風洞試験グループ"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"NAL/NASDA HOPE研究共同チーム"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"NAL/NASDA HOPE研究共同チーム"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Dynamic Wind-Tunnel Test Group","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"NAL/NASDA HOPE Joint Team","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"NAL/NASDA HOPE Joint 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":"2020-01-27"}],"displaytype":"detail","filename":"naltr01306.pdf","filesize":[{"value":"2.6 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr01306.pdf","url":"https://jaxa.repo.nii.ac.jp/record/39820/files/naltr01306.pdf"},"version_id":"866e2250-73cf-4cd7-b6f7-af98c4a44112"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"ALFLEX","subitem_subject_scheme":"Other"},{"subitem_subject":"小型自動着陸実験","subitem_subject_scheme":"Other"},{"subitem_subject":"HOPE","subitem_subject_scheme":"Other"},{"subitem_subject":"H-2 ロケット打上げ型有翼回収機","subitem_subject_scheme":"Other"},{"subitem_subject":"動的風洞実験","subitem_subject_scheme":"Other"},{"subitem_subject":"空力モデルの同定","subitem_subject_scheme":"Other"},{"subitem_subject":"懸吊システム","subitem_subject_scheme":"Other"},{"subitem_subject":"ADS","subitem_subject_scheme":"Other"},{"subitem_subject":"エアデータセンサ","subitem_subject_scheme":"Other"},{"subitem_subject":"ALFLEX","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"automatic landing flight experiment","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"HOPE","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"H 2 orbiting plane","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"dynamic wind tunnel test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"identification of aerodynamic model","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"suspending system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"ADS","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"air data sensor","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":"ALFLEX実験機の懸吊風洞試験","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"ALFLEX実験機の懸吊風洞試験"}]},"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":"39820","relation_version_is_last":true,"title":["ALFLEX実験機の懸吊風洞試験"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T19:18:45.023367+00:00"}