{"created":"2023-06-20T15:08:00.133334+00:00","id":37387,"links":{},"metadata":{"_buckets":{"deposit":"ebec3385-4f52-4e91-9d18-a8aa42eb1638"},"_deposit":{"created_by":1,"id":"37387","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"37387"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00037387","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["480513","480505","480499","480503","480496","480510","480502","480508","480506","480500","480504","480509","480511","480498","480497","480507","480501","480512"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Aerodynamic heating experiment on a HOPE-X model in the high enthalpy shock tunnel"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1999-05","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"60","bibliographicPageStart":"57","bibliographicVolumeNumber":"42","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":"21-22 May 1998 (60th). 26-27 Nov. 1998 (61st)","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":"21-22 May 1998 (60th). 26-27 Nov. 1998 (61st)","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"HOPE-X(宇宙往還技術試験機)模型の空力加熱試験を航空宇宙技術研究所角田研究センターの自由ピストン型衝撃風洞(HIEST)で実施した。70個の同軸型熱電対を模型の風上側に装備した。模型は実物の1/40スケールである。気流条件は、同じ自由ピストンドライバー条件の下で、ノズルスロート径を変えることにより変化させた。この条件の下で測定された模型の周りの熱流束分布を報告した。模型の翼前縁の熱流束の変動についても言及した。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Aerodynamic heating experiment on a HOPE-X (H-2 Orbiting Plane Experimental) reentry vehicle model was carried out in the free piston shock tunnel HIEST (High Enthalpy Shock Tunnel) at National Aerospace Laboratory Kakuda Research Center. Seventy coaxial thermocouples were instrumented on the windward of the model, which is 1/40 scale of the actual vehicle. Flow condition was varied with different diameter nozzle throats under same free piston driver condition. Measured heat flux distribution around the model under the condition was reported. Heat flux fluctuation on the leading edge of the model was also mentioned.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0001959007","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-42","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"},{"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":"航空宇宙技術振興財団"},{"subitem_text_value":"航空宇宙技術振興財団"},{"subitem_text_value":"宇宙開発事業団"}]},"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"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Kakuda Research Center"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Technology Foundation"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Technology Foundation"},{"subitem_text_language":"en","subitem_text_value":"National Space Development Agency of Japan"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"丹野, 英幸"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"小室, 智幸"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"佐藤, 和雄"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"伊藤, 勝宏"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"高橋, 政浩"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"植田, 修一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"前原, 卓哉"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"成田, 智昭"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"水藤, 貴靖"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tanno, Hideyuki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Komuro, Tomoyuki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sato, Kazuo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ito, Katsuhiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Takahashi, Masahiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ueda, Shuichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Maehara, Takuya","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Narita, Tomoaki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Suito, Takanobu","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":"2020-02-10"}],"displaytype":"detail","filename":"nalsp0042007.pdf","filesize":[{"value":"379.7 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0042007.pdf","url":"https://jaxa.repo.nii.ac.jp/record/37387/files/nalsp0042007.pdf"},"version_id":"4daaae25-c60a-40ec-bcf9-ac75763d9d88"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"空力加熱","subitem_subject_scheme":"Other"},{"subitem_subject":"HOPE-X","subitem_subject_scheme":"Other"},{"subitem_subject":"宇宙往還技術試験機","subitem_subject_scheme":"Other"},{"subitem_subject":"高温衝撃風洞","subitem_subject_scheme":"Other"},{"subitem_subject":"自由ピストン型衝撃風洞","subitem_subject_scheme":"Other"},{"subitem_subject":"熱流束分布","subitem_subject_scheme":"Other"},{"subitem_subject":"翼前縁","subitem_subject_scheme":"Other"},{"subitem_subject":"熱流束の変動","subitem_subject_scheme":"Other"},{"subitem_subject":"同軸型熱電対","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic heating","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"HOPE X","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"H 2 Orbiting Plane Experimental","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"high enthalpy shock tunnel","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"free piston shock tunnel","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"heat flux distribution","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"leading edge","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"heat flux fluctuation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"coaxial thermocouple","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":"高温衝撃風洞によるHOPE-X模型の空力加熱試験","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"高温衝撃風洞によるHOPE-X模型の空力加熱試験"}]},"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":"37387","relation_version_is_last":true,"title":["高温衝撃風洞によるHOPE-X模型の空力加熱試験"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:20:14.333021+00:00"}