{"created":"2023-06-20T15:10:39.544723+00:00","id":40237,"links":{},"metadata":{"_buckets":{"deposit":"5fdf2ee4-2578-4d77-8463-c3991c4bc6f9"},"_deposit":{"created_by":1,"id":"40237","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"40237"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00040237","sets":["1887:1893","1896:1898:1913:1916"]},"author_link":["446959","446958"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Reconstructed below Mach 2 flight of Hypersonic Flight Experiment vehicle (HYFLEX)"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1998-07","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"12","bibliographicPageStart":"1","bibliographicVolumeNumber":"726","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所資料"},{"bibliographic_title":"Technical Memorandum of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"本稿では、1996年2月12日に打ち上げられた極超音速飛行実験機(以下HYFLEX)のマッハ2以下の飛行について述べる。飛行実験では機体の回収には失敗したものの、テレメトリデータ、レーダトラッキングデータが良好に取得された。本稿ではこれら取得されたデータに基づき、マッハ2以下の飛行について再現を試みた。得られた結果から、HYFLEXがスピン状態で降下していく様子が概ね把握できた。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"This paper describes the actual flight trajectory under Mach 2 of the Hypersonic Flight Experiment vehicle (HYFLEX). Although the recovery of the vehicle failed, radar tracking and telemetry data were obtained. In this paper, these data are analyzed and the flight trajectory under Mach 2 is reconstructed. It was found that the vehicle flew in a random spin and not according to the preflight plan. The reason for the failed maneuver was proved by postflight simulation.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0001567000","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 TM-726","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":"0452-2982","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":"AN00314334","subitem_source_identifier_type":"NCID"}]},"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 新型航空機研究グループ"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Advanced Aircraft Research Group"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"鈴木, 広一"}],"nameIdentifiers":[{"nameIdentifier":"446958","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Suzuki, Hirokazu","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"446959","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":"naltm0000726.pdf","filesize":[{"value":"1.1 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltm0000726.pdf","url":"https://jaxa.repo.nii.ac.jp/record/40237/files/naltm0000726.pdf"},"version_id":"7b12af3b-d2e8-42b1-b4cb-413a4296dad0"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"HYFLEX","subitem_subject_scheme":"Other"},{"subitem_subject":"極超音速飛行実験","subitem_subject_scheme":"Other"},{"subitem_subject":"慣性航法データ","subitem_subject_scheme":"Other"},{"subitem_subject":"飛行実験","subitem_subject_scheme":"Other"},{"subitem_subject":"大仰角飛行","subitem_subject_scheme":"Other"},{"subitem_subject":"飛行経路","subitem_subject_scheme":"Other"},{"subitem_subject":"飛行姿勢","subitem_subject_scheme":"Other"},{"subitem_subject":"飛行シミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"迎え角","subitem_subject_scheme":"Other"},{"subitem_subject":"再突入経路","subitem_subject_scheme":"Other"},{"subitem_subject":"HYFLEX","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Hypersonic Flight Experiment","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"inertial navigation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flight test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"high angle of attack flight","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flight path","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flight attitude","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flight simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"angle of attack","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"reentry trajectory","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":"極超音速飛行実験(HYFLEX)機のマッハ2以下の実飛行経路について","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"極超音速飛行実験(HYFLEX)機のマッハ2以下の実飛行経路について"}]},"item_type_id":"3","owner":"1","path":["1893","1916"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"40237","relation_version_is_last":true,"title":["極超音速飛行実験(HYFLEX)機のマッハ2以下の実飛行経路について"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T19:16:37.625561+00:00"}