{"created":"2023-06-20T15:14:05.244185+00:00","id":44059,"links":{},"metadata":{"_buckets":{"deposit":"d13521d9-7aa7-4b19-9854-1eb9c6c75e1c"},"_deposit":{"created_by":1,"id":"44059","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"44059"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00044059","sets":["1887:1893","1896:1898:1913:1916"]},"author_link":["467346","467353","467349","467348","467345","467344","467350","467352","467351","467347"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Measurements of Static Stability of Capsule-Type Re-Entry Bodies"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1982-10","bibliographicIssueDateType":"Issued"},"bibliographicPageStart":"53","bibliographicVolumeNumber":"476","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所資料"},{"bibliographic_title":"Technical Memorandum of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Hypersonic wind tunnel tests were made to determine the aerodynamic characteristics of some capsule type re-entry bodies at Mach number 7.1 and at angles of attack from 0°to 20°.The Reynolds number based on maximum body diameter varied from 4.5 × 105 to 18×105.Tests were made to determine the appropriate nose and shoulder radii of these capsules necessary to obtain optimum configurations for the aerodynamic requirements.The nose radius R1 is changed from 2 to 4 and shoulder radius R2 from 0 to 0.1,which are nondimensionalized by the maximum radius R3 of the sharp shoulder capsules,respectively.Results of the tests indicate that higher lift to drag ratio L/D and lower trim angles δ can be obtained by increasing the nose radius.The same trends are shown when decreasing the shoulder radius.The Reynolds number shows a slight effect on the lift and drag coefficients CL,CD,but no remarkable differences can be seen in other aerodynamic coefficients.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALTM0476000","subitem_description_type":"Other"}]},"item_3_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: NAL TM-476","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"航空宇宙技術研究所"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"National Aerospace 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弘一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"小山, 忠勇"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"YAMAMOTO, Yukimitsu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"WATANABE, Mitsunori","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"NOMURA, Shigeaki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"HOZUMI, Koichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"KOYAMA, Tadao","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":"2020-01-28"}],"displaytype":"detail","filename":"naltm00476.pdf","filesize":[{"value":"2.4 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