{"created":"2023-06-20T14:54:21.913377+00:00","id":22699,"links":{},"metadata":{"_buckets":{"deposit":"b8da7575-f8b3-4edc-84da-ec01160e8f37"},"_deposit":{"created_by":1,"id":"22699","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"22699"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00022699","sets":["1887:1888"]},"author_link":["212988","212989","212987","212992","212990","212991"],"item_7_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Damage mechanics based creep fatigue analysis of combustion chamber for satellite's bipropellant thruster"}]},"item_7_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2016-03-15","bibliographicIssueDateType":"Issued"},"bibliographicIssueNumber":"835","bibliographicPageStart":"15-00667","bibliographicVolumeNumber":"82","bibliographic_titles":[{"bibliographic_title":"日本機械学会論文集"},{"bibliographic_title":"Transactions of the JSME (in Japanese)","bibliographic_titleLang":"en"}]}]},"item_7_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Creep - fatigue analyses based on the concept of continuum damage mechanics were conducted for the combustion chamber used in a satellite’s bipropellant thruster. The previously identified models and material parameters for the niobium alloy (C103) which is used as the combustion chamber’s material were extended to deal with the prediction of the creep - fatigue behavior and the chamber life of a bipropellant thruster. The thrust force of 22 N thruster was selected for FEM analyses and post damage calculations. The analyses in different injection modes of continuation and pulse were conducted to evaluate their influence on the chamber’s life. The maximum temperatures on a chamber surface were also changed for two patterns of 1250 C and 1500 C. The combustion chamber life was evaluated for the different surface temperature. The analysis results show that the calculated chamber’s life of continuous injection at 1500 C was shorter than that at 1250 C because of plasticity damage. The analysis results also show that the major damage mode was creep and fatigue damage was very little in pulse injection. From the results, it is expected that the used models and determined material parameters can predict the mechanical features and creep - fatigue life for the combustion chamber of a bipropellant thruster.","subitem_description_type":"Other"}]},"item_7_description_18":{"attribute_name":"内容記述","attribute_value_mlt":[{"subitem_description":"形態: カラー図版あり","subitem_description_type":"Other"}]},"item_7_description_19":{"attribute_name":"内容記述（英）","attribute_value_mlt":[{"subitem_description":"Physical characteristics: Original contains color illustrations","subitem_description_type":"Other"}]},"item_7_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: PA1610089000","subitem_description_type":"Other"}]},"item_7_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"日本機械学会"}]},"item_7_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"The Japan Society of Mechanical Engineers"}]},"item_7_relation_25":{"attribute_name":"DOI","attribute_value_mlt":[{"subitem_relation_name":[{"subitem_relation_name_text":"info:doi/10.1299/transjsme.15-00667"}],"subitem_relation_type_id":{"subitem_relation_type_id_text":"http://dx.doi.org/10.1299/transjsme.15-00667","subitem_relation_type_select":"DOI"}}]},"item_7_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"2187-9761","subitem_source_identifier_type":"ISSN"}]},"item_7_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"東京大学大学院工学系研究科"},{"subitem_text_value":"東京大学生産技術研究所"},{"subitem_text_value":"宇宙航空研究開発機構研究開発部門(JAXA)"}]},"item_7_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"School of Engineering, University of Tokyo"},{"subitem_text_language":"en","subitem_text_value":"Institute of Industrial Science, University of Tokyo"},{"subitem_text_language":"en","subitem_text_value":"Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA)"}]},"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":"升岡, 正"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"都井, 裕"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"池田, 博英"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Masuoka, Tadashi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Toi, Yutaka","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ikeda, Hirohide","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"Damage mechanics","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Bipropellant thruster","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Niobium alloy","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"High temperature","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Creep","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Fatigue","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":"journal article","resourceuri":"http://purl.org/coar/resource_type/c_6501"}]},"item_title":"損傷力学に基づく人工衛星用二液式スラスタ燃焼器のクリープ疲労解析","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"損傷力学に基づく人工衛星用二液式スラスタ燃焼器のクリープ疲労解析"}]},"item_type_id":"7","owner":"1","path":["1888"],"pubdate":{"attribute_name":"公開日","attribute_value":"2016-06-24"},"publish_date":"2016-06-24","publish_status":"0","recid":"22699","relation_version_is_last":true,"title":["損傷力学に基づく人工衛星用二液式スラスタ燃焼器のクリープ疲労解析"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T03:16:47.522194+00:00"}