{"created":"2023-06-20T14:39:39.976009+00:00","id":6425,"links":{},"metadata":{"_buckets":{"deposit":"9cfb9d52-624d-43c9-98ec-6f6100511232"},"_deposit":{"created_by":1,"id":"6425","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"6425"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00006425","sets":["1887:1891","9:789:1067:1071"]},"author_link":["32628","32627"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Hypersonic aerothermodynamic and scramjet research using high enthalpy shock tunnel HIEST"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2005-03-30","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"8","bibliographicPageStart":"1","bibliographicVolumeNumber":"JAXA-SP-04-014","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構特別資料: 第73回風洞研究会議論文集"},{"bibliographic_title":"JAXA Special Publication: Proceedings of the Wind Tunnel Technology Association 73rd Meeting","bibliographic_titleLang":"en"}]}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"HOPE研究が盛んであった1990年代初期、大気圏再突入時の流れを地上で再現して実在気体熱空力特性を観測することを目的として大型高温衝撃風洞の建設計画が進められ、スクラムジェットエンジン試験への利用にも積極的であったJAXA宇宙推進技術共同センターにおいて1997年度末にHIESTが完成した。以来、HOPEその他の熱空力試験および超高速域スクラムジェットエンジン試験など現在まで1,000回を超える試験を行ってきた。ここではこれまでHIESTにおいて行ってきた試験の主要な成果について述べる。","subitem_description_type":"Abstract"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0048471001","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: 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tunnel","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"atmospheric reentry","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"shock tube test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic heating","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"hypersonic flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"scramjet engine","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wall catalysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"temperature dependence","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wind tunnel 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