{"created":"2023-06-20T15:07:30.024391+00:00","id":36868,"links":{},"metadata":{"_buckets":{"deposit":"febd300d-012b-46e3-b87b-73e8e2c0fdd0"},"_deposit":{"created_by":1,"id":"36868","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"36868"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00036868","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["477928","477926","477930","477927","477925","477929"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"On flight data of HYFLEX"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1997-01","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"48","bibliographicPageStart":"43","bibliographicVolumeNumber":"34","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 6-7 JUN. 1996 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 6-7 JUN. 1996 Tokyo Japan","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"日本のHOPE(H-2ロケット打上げ型有翼回収機)の開発のために計画した、HYFLEX(極超音速飛行実験)を1996年2月12日に成功裏に実施した。実験に使用した飛行体は全長4.4mの細長いボディ形状をしており、全備重量は1,073kgである。飛行実験を通して空気力学、熱防護システム、誘導・制御に関する種々の極超音速揚力飛行データを取得した。極超音速航空力学に関連する以下の飛行データ、すなわち空力特性、空力加熱、ADS(大気データセンサ)とRCS(ガスジェット姿勢制御システム)ガスジェット相互作用実験のための圧力測定、および機体周りの電子密度などを簡単に概観した。予測法の有効性を検討するため、飛行データを風洞試験結果およびCFD(数値流体力学)計算に基づく飛行前予測データと比較した。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"HYFLEX (Hypersonic Flight Experiment) which was planned for the development of the Japanese unmanned orbiting plane, HOPE (H-2 Orbiting Plane), was successfully conducted on Feb. 12, 1996. The vehicle used in the experiment has a 4.4 m-long slender body configuration whose gross weight is 1,073 kg. Various hypersonic lifting flight data on aerodynamics, thermal protection system, and guidance & control were acquired during the flight. In this paper, the following flight data in respect to hypersonic aerodynamics are briefly reviewed: aerodynamic characteristics, aerodynamic heating, pressure measurements for ADS (Air Data Sensor) and RCS (Reaction Control Subsystem) gas-jet interaction experiment, and electron density around the vehicle. The data are compared with the preflight predictions based on wind tunnel test results and CFD (Computational Fluid Dynamics) calculations in order to investigate validity of the prediction methods.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0000685009","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-34","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"},{"subitem_text_value":"航空宇宙技術研究所"},{"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"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"},{"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":"渡辺, 重哉"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"白水, 正男"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"山本, 昌孝"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Watanabe, Shigeya","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Shirouzu, Masao","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yamamoto, Masataka","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":"nalsp0034009.pdf","filesize":[{"value":"520.4 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0034009.pdf","url":"https://jaxa.repo.nii.ac.jp/record/36868/files/nalsp0034009.pdf"},"version_id":"aa4566ce-c7d8-438e-a43e-741d674dc9db"}]},"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":"HOPE","subitem_subject_scheme":"Other"},{"subitem_subject":"H-2ロケット打ち上げ型有翼回収機","subitem_subject_scheme":"Other"},{"subitem_subject":"熱防護システム","subitem_subject_scheme":"Other"},{"subitem_subject":"空力特性","subitem_subject_scheme":"Other"},{"subitem_subject":"空力加熱","subitem_subject_scheme":"Other"},{"subitem_subject":"電子密度","subitem_subject_scheme":"Other"},{"subitem_subject":"航空機計算空気力学","subitem_subject_scheme":"Other"},{"subitem_subject":"大気データセンサ","subitem_subject_scheme":"Other"},{"subitem_subject":"ガスジェット相互作用","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD","subitem_subject_scheme":"Other"},{"subitem_subject":"数値流体力学","subitem_subject_scheme":"Other"},{"subitem_subject":"極超音速揚力飛行","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":"thermal protection system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic characteristic","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic heating","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"electron density","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aircraft computational aerodynamics","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"air data sensor","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"gas jet interaction","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"computational fluid dynamics","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"hypersonic lifting flight","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":"極超音速飛行実験(HYFLEX)の飛行データについて","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"極超音速飛行実験(HYFLEX)の飛行データについて"}]},"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":"36868","relation_version_is_last":true,"title":["極超音速飛行実験(HYFLEX)の飛行データについて"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:30:16.111940+00:00"}