{"created":"2023-06-20T15:07:49.375831+00:00","id":37185,"links":{},"metadata":{"_buckets":{"deposit":"d696927f-5185-4901-923a-1a559ebd095b"},"_deposit":{"created_by":1,"id":"37185","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"37185"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00037185","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["479378","479382","479384","479376","479380","479385","479383","479379","479381","479377"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Aerodynamic heating experiments on a HYFLEX model in high-enthalpy shock tunnel"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1998-01","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"24","bibliographicPageStart":"17","bibliographicVolumeNumber":"38","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所特別資料"},{"bibliographic_title":"Special Publication of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_5_description_14":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）","attribute_value_mlt":[{"subitem_description":"22-23 May 1997 (58th). 27-28 Nov. 1997 (59th)","subitem_description_type":"Other"}]},"item_5_description_15":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）（英）","attribute_value_mlt":[{"subitem_description":"22-23 May 1997 (58th). 27-28 Nov. 1997 (59th)","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"日本の無人宇宙往還機HOPE(H-2ロケット打上げ型有翼回収機)の開発のための小型実験機の1つとして、HYFLEX(超音速飛行実験)を計画した。C/C(カーボン繊維カーボン樹脂複合材料)高温構造部およびセラミックタイル部の空力加熱を飛行中に測定した。本論文では、HYFLEX実験機の空力加熱測定用モデルについて述べた。HYFLEX実験機モデルは、角田宇宙推進技術研究センターの中型の自由ピストン衝撃風洞HEK(中型高温衝撃風洞)で試験した。試験条件は、HYFLEXの飛行経路から選び、この実験から得られた結果を飛行データと比較した。HEKノズルの気流検定結果についても述べた。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The HYFLEX (Hypersonic Flight Experiment) project was planned as one of a series of small-scale experimental vehicles for the development of the Japanese unmanned orbiting plane, HOPE (H-2 Orbiting Plane). The aerodynamic heating to the region of C/C (Carbon/Carbon composite) hot structure and ceramic tile were measured during flight. In this paper, aerodynamic heating experiments on a HYFLEX model are presented. The HYFLEX model was tested in the HEK (High Enthalpy Kakuda), a medium size free-piston shock tunnel at the Kakuda Research Center. Test conditions were selected along the HYFLEX flight trajectory and results obtained in these experiments are compared with flight data. Flow calibration results of the HEK nozzle are also presented.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0001434003","subitem_description_type":"Other"}]},"item_5_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: NAL SP-38","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"航空宇宙技術研究所"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"National Aerospace Laboratory (NAL)"}]},"item_5_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0289-260X","subitem_source_identifier_type":"ISSN"}]},"item_5_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AN10097345","subitem_source_identifier_type":"NCID"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"航空宇宙技術研究所 角田宇宙推進技術研究センター"},{"subitem_text_value":"航空宇宙技術研究所 角田宇宙推進技術研究センター"},{"subitem_text_value":"航空宇宙技術研究所 角田宇宙推進技術研究センター"},{"subitem_text_value":"航空宇宙技術研究所 角田宇宙推進技術研究センター"},{"subitem_text_value":"航空宇宙技術研究所 角田宇宙推進技術研究センター"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Kakuda Research Center"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Kakuda Research Center"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Kakuda Research Center"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Kakuda Research Center"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Kakuda Research Center"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"植田, 修一"}],"nameIdentifiers":[{"nameIdentifier":"479376","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"佐藤, 和雄"}],"nameIdentifiers":[{"nameIdentifier":"479377","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"小室, 智幸"}],"nameIdentifiers":[{"nameIdentifier":"479378","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"高橋, 政浩"}],"nameIdentifiers":[{"nameIdentifier":"479379","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"伊藤, 勝宏"}],"nameIdentifiers":[{"nameIdentifier":"479380","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Ueda, Shuichi","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"479381","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Sato, Kazuo","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"479382","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Komuro, Tomoyuki","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"479383","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Takahashi, Masahiro","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"479384","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Ito, Katsuhiro","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"479385","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":"2020-02-10"}],"displaytype":"detail","filename":"nalsp0038003.pdf","filesize":[{"value":"721.9 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0038003.pdf","url":"https://jaxa.repo.nii.ac.jp/record/37185/files/nalsp0038003.pdf"},"version_id":"6f74782c-bd23-4487-b074-40ddbdf6dbef"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"HYFLEX","subitem_subject_scheme":"Other"},{"subitem_subject":"超音速飛行実験","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":"空力加熱","subitem_subject_scheme":"Other"},{"subitem_subject":"自由ピストン衝撃風洞","subitem_subject_scheme":"Other"},{"subitem_subject":"HEK","subitem_subject_scheme":"Other"},{"subitem_subject":"中型高温衝撃風洞","subitem_subject_scheme":"Other"},{"subitem_subject":"熱流速","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":"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":"aerodynamic heating","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"free piston shock tunnel","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"HEK","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"High Enthalpy Kakuda","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"heat flux","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":"conference paper","resourceuri":"http://purl.org/coar/resource_type/c_5794"}]},"item_title":"高温衝撃風洞におけるHYFLEXの空力加熱試験","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"高温衝撃風洞におけるHYFLEXの空力加熱試験"}]},"item_type_id":"5","owner":"1","path":["1891","1915"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"37185","relation_version_is_last":true,"title":["高温衝撃風洞におけるHYFLEXの空力加熱試験"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:23:55.372577+00:00"}