{"created":"2023-06-20T14:46:51.337377+00:00","id":14457,"links":{},"metadata":{"_buckets":{"deposit":"1e70053d-2fcb-473f-96cf-68660be10c50"},"_deposit":{"created_by":1,"id":"14457","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"14457"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00014457","sets":["1543:1656:1664","1887:1891"]},"author_link":["132328","132339","132326","132330","132335","132332","132329","132336","132327","132337","132331","132333","132334","132338"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Numerical Study of Drag Characteristics for Advanced Solid Rocket"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2009-12","bibliographicIssueDateType":"Issued"},"bibliographicVolumeNumber":"平成20年度","bibliographic_titles":[{"bibliographic_title":"宇宙航行の力学シンポジウム"},{"bibliographic_title":"Symposium on Flight Mechanics and Astrodynamics","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":"宇宙航行の力学シンポジウム(平成20年度)(2008年12月4～5日、宇宙航空研究開発機構宇宙科学研究本部)","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":"Symposium on Flight Mechanics and Astrodynamics 2008 (December 4-5, 2008. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)), Sagamihara, Kanagawa Japan","subitem_description_type":"Other"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Drag characteristics of Next-generation solid rocket motor is computationally studied for subsonic and super sonic conditions. Computed drag coefncients are compared with experiments. It is clarified that their difference is with in 10% of total, which is reasonable for conceptual aerodynamic analysis. Since difference of windward and base pressure is relatively small at subsonic condition, small change of base pressure can be result in large total drag change. For example, 1% change of base pressure based on free-stream static pressure corresponds to 20% change of total drag at Mach number 0.7. While, 5% change of base pressure corresponds to 4% change of total drag at Mach number 2.0. This result implies an importance of consideration of base pressure change induced by sting interference efect for the experimental data analysis.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0064729034","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宇宙科学研究本部"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)"}]},"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情報・計算工学センター"},{"subitem_text_value":"宇宙航空研究開発機構情報・計算工学センター"},{"subitem_text_value":"宇宙航空研究開発機構情報・計算工学センター"},{"subitem_text_value":"東京理科大学"},{"subitem_text_value":"東京理科大学"},{"subitem_text_value":"東京理科大学"},{"subitem_text_value":"東京大学"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"JAXA's Engineering Degital Innovation Center, Japan Aerospace Exploration Agency (JAXA)(JEDI)"},{"subitem_text_language":"en","subitem_text_value":"JAXA's Engineering Degital Innovation Center, Japan Aerospace Exploration Agency (JAXA)(JEDI)"},{"subitem_text_language":"en","subitem_text_value":"JAXA's Engineering Degital Innovation Center, Japan Aerospace Exploration Agency (JAXA)(JEDI)"},{"subitem_text_language":"en","subitem_text_value":"Science University of Tokyo"},{"subitem_text_language":"en","subitem_text_value":"Science University of Tokyo"},{"subitem_text_language":"en","subitem_text_value":"Science University of Tokyo"},{"subitem_text_language":"en","subitem_text_value":"University of Tokyo"}]},"item_access_right":{"attribute_name":"アクセス権","attribute_value_mlt":[{"subitem_access_right":"metadata only access","subitem_access_right_uri":"http://purl.org/coar/access_right/c_14cb"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"藤本, 圭一郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"北村, 圭一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"嶋, 英志"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"滑, 慶則"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"山崎, 祐希"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"山本, 誠"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"浅田, 健吾"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Fujimoto, Keiichiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kitamura, Keiichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Shima, Eiji","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Namera, Yoshinori","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yamasaki, Yuki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yamamoto, Makoto","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Asada, Kengo","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"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":"次期固体ロケットの抵抗特性解析: 抵抗予測精度についての一考察","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"次期固体ロケットの抵抗特性解析: 抵抗予測精度についての一考察"}]},"item_type_id":"5","owner":"1","path":["1664","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"14457","relation_version_is_last":true,"title":["次期固体ロケットの抵抗特性解析: 抵抗予測精度についての一考察"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T05:34:14.606553+00:00"}