{"created":"2023-06-20T15:07:23.180479+00:00","id":36753,"links":{},"metadata":{"_buckets":{"deposit":"0bb0de95-ae68-43d9-81b5-83cdf73e929c"},"_deposit":{"created_by":1,"id":"36753","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"36753"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00036753","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["477441","477442","477443","477444"],"item_5_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"OREXの空力および空力加熱解析結果"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1996-01","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"26","bibliographicPageStart":"17","bibliographicVolumeNumber":"29","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":"航空宇宙技術研究所 8 Jun. 1995 東京 日本","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":"National Aerospace Laboratory 8 Jun. 1995 Tokyo Japan","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"HOPE(H-2ロケット打上型有翼回収機)開発に先立って3つの実験を行った。1994年2月4日にH-2のTF#1の機会にOREX(軌道再突入実験)を行い、再突入時の空気熱力学および空気力学の基礎データを取得しOREXの主目的のひとつの結果を報告した。空力熱力学については、飛行実験前に風洞実験値とFay&Riddell法から導いた推定値との比較を評価した。実験後、以前に確認したFay&Riddell法を使い飛行軌道から誘導した加熱率を推定した。そして熱解析モデルを使い澱み点の温度を計算し、飛行データの値と比較した。空気力学に関しては、推定値と飛行圧力データとを比較した。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Three experiments are performed preceding to the development of HOPE (H-2 Orbiting Plane). OREX (Orbital Reentry Experiment) was performed taking the opportunity of H-2 TF (Test Flight) No. 1 on Feb. 4, 1994. A result of one of the main purpose of OREX, acquisition of fundamental data of aerothermo- and aerodynamics during reentry is reported. As to aerothermodynamics, comparison between wind tunnel test data and values estimated from Fay & Riddell method was evaluated before a flight experiment. After the experiment, heating rate induced from flight orbit using Fay & Riddell method validated before was evaluated. And a temperature at the stagnation point was calculated using thermal-analysis model, then the value was compared with flight data. As to aerodynamics, flight pressure data was compared with estimated value.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0000110003","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-29","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":"宇宙開発事業団"},{"subitem_text_value":"航空宇宙技術研究所"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Space Development Agency of Japan"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"下田, 孝幸"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"松崎, 貴至"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Shimoda, Takayuki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Matsuzaki, Takashi","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":"nalsp0029003.pdf","filesize":[{"value":"769.3 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0029003.pdf","url":"https://jaxa.repo.nii.ac.jp/record/36753/files/nalsp0029003.pdf"},"version_id":"605959ef-e704-4700-9030-27050e69b130"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"OREX","subitem_subject_scheme":"Other"},{"subitem_subject":"軌道再突入実験","subitem_subject_scheme":"Other"},{"subitem_subject":"空気熱力学","subitem_subject_scheme":"Other"},{"subitem_subject":"空気力学","subitem_subject_scheme":"Other"},{"subitem_subject":"HOPE","subitem_subject_scheme":"Other"},{"subitem_subject":"H-2ロケット打上型有翼回収機","subitem_subject_scheme":"Other"},{"subitem_subject":"風洞","subitem_subject_scheme":"Other"},{"subitem_subject":"熱解析モデル","subitem_subject_scheme":"Other"},{"subitem_subject":"澱み点","subitem_subject_scheme":"Other"},{"subitem_subject":"飛行圧力データ","subitem_subject_scheme":"Other"},{"subitem_subject":"高エンタルピー流れ","subitem_subject_scheme":"Other"},{"subitem_subject":"OREX","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"orbital reentry experiments","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerothermodynamics","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamics","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":"wind tunnel","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"thermal analysis model","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"stagnation point","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flight pressure data","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"high enthalpy flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"eng"}]},"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":"The result of an analysis of aerothermo and aerodynamics of OREX","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"The result of an analysis of aerothermo and aerodynamics of OREX","subitem_title_language":"en"}]},"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":"36753","relation_version_is_last":true,"title":["The result of an analysis of aerothermo and aerodynamics of OREX"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:32:27.434003+00:00"}