{"created":"2023-06-20T14:39:31.484779+00:00","id":6263,"links":{},"metadata":{"_buckets":{"deposit":"af419439-aa25-4dc4-b402-25a0c60cff61"},"_deposit":{"created_by":1,"id":"6263","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"6263"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00006263","sets":["1887:1893","9:789:1031:1060"]},"author_link":["31531","31532","31530","31533","31529","31534"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Coupled load analysis and testing method for evaluating design of satellite/rocket"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2006-01-20","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"36","bibliographicPageStart":"31","bibliographicVolumeNumber":"JAXA-SP-05-008","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構特別資料: 平成16年度総合技術研究本部宇宙領域宇宙科学研究本部合同研究成果報告書:人工衛星系基盤技術"},{"bibliographic_title":"JAXA Special Publication: FY2004 Report of Joint Research Achievements of the Space Division of Institute of Aerospace Technology and Institute of Space and Astronautical Science: Basic Technologies of Satellite Systems","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"This paper describes the results of an investigation into the current status of a satellite-rocket coupled load analysis technique and a vibration test technique used to validate analytical results in Europe and the USA. Their analytical techniques are at the same level as in Japan. They consider vibration testing to be important for validating analysis results but believe that it is difficult to validate results by testing with a three-axis, six-DOF test machine. A Japanese manufacturer has a good technology for performing such tests. We concluded that Japan has the potential to lead other countries in this technical area by realizing a three-axis, six-DOF test machine for analyzing and improving coupled load methods.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0049054007","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: JAXA-SP-05-008","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Japan Aerospace Exploration Agency (JAXA)"}]},"item_3_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"1349-113X","subitem_source_identifier_type":"ISSN"}]},"item_3_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_3_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":"宇宙航空研究開発機構 総合技術研究本部"}]},"item_3_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 Space Technology and Aeronautics"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"下田, 孝幸"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"内田, 英樹"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"幸節, 雄二"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Shimoda, Takayuki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Uchida, Hideki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kosetsu, Yuji","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":"2020-01-16"}],"displaytype":"detail","filename":"49054007.pdf","filesize":[{"value":"2.1 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"49054007.pdf","url":"https://jaxa.repo.nii.ac.jp/record/6263/files/49054007.pdf"},"version_id":"f46b085e-df48-4e43-b73c-b8751adfc155"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"衛星設計","subitem_subject_scheme":"Other"},{"subitem_subject":"ロケットエンジン設計","subitem_subject_scheme":"Other"},{"subitem_subject":"振動荷重","subitem_subject_scheme":"Other"},{"subitem_subject":"結合振動荷重解析","subitem_subject_scheme":"Other"},{"subitem_subject":"数学モデル","subitem_subject_scheme":"Other"},{"subitem_subject":"計算機プログラム","subitem_subject_scheme":"Other"},{"subitem_subject":"構造設計","subitem_subject_scheme":"Other"},{"subitem_subject":"振動試験","subitem_subject_scheme":"Other"},{"subitem_subject":"satellite design","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"rocket engine design","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"vibratory load","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"coupled load analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"mathematical model","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"computer program","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"structural design","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"vibration test","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":"technical report","resourceuri":"http://purl.org/coar/resource_type/c_18gh"}]},"item_title":"衛星/ロケット設計評価のための振動解析手法と実験的手法に関する調査・研究","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"衛星/ロケット設計評価のための振動解析手法と実験的手法に関する調査・研究"}]},"item_type_id":"3","owner":"1","path":["1060","1893"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"6263","relation_version_is_last":true,"title":["衛星/ロケット設計評価のための振動解析手法と実験的手法に関する調査・研究"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:58:57.101154+00:00"}