{"created":"2023-06-20T14:38:57.205659+00:00","id":5601,"links":{},"metadata":{"_buckets":{"deposit":"77ae6176-eaa7-459b-afac-c75d299436ab"},"_deposit":{"created_by":1,"id":"5601","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"5601"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00005601","sets":["1887:1891","9:789:972:983"]},"author_link":["27415","27411","27414","27412","27413","27416"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Development of a hyper-velocity shock tube for improvement of reentry flight environment assessment technologies"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2008-02-29","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"26","bibliographicPageStart":"23","bibliographicVolumeNumber":"JAXA-SP-07-019","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構特別資料: 第79回風洞研究会議論文集"},{"bibliographic_title":"JAXA Special Publication: Proceedings of the Wind Tunnel Technology Association 79th Meeting","bibliographic_titleLang":"en"}]}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"JAXA総合技術研究本部では、将来の再使用輸送系、有人飛行、惑星プローブ開発に関わる基盤技術の向上を目指し、観測部が70×70mm、全長約23mの中規模で、最大衝撃波速度12km/sを達成可能な中型高速衝撃波管を開発し、その運用を開始した。本報告では、衝撃波管の概要と性能について紹介するとともに、超高速短時間計測システム開発の現状を紹介し、今後の研究開発の方向について議論する。","subitem_description_type":"Abstract"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0063897004","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: JAXA-SP-07-019","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Japan Aerospace Exploration Agency (JAXA)"}]},"item_5_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"1349-113X","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":"AA11984031","subitem_source_identifier_type":"NCID"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"宇宙航空研究開発機構 総合技術研究本部"},{"subitem_text_value":"宇宙航空研究開発機構 総合技術研究本部"},{"subitem_text_value":"東京大学 大学院新領域創成科学研究科"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Institute of Aerospace 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