{"created":"2024-01-25T05:49:17.740314+00:00","id":2000210,"links":{},"metadata":{"_buckets":{"deposit":"2a908385-11fc-4718-b7a1-c7714183c900"},"_deposit":{"created_by":27,"id":"2000210","owners":[27],"pid":{"revision_id":0,"type":"depid","value":"2000210"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:02000210","sets":["1887:1893","9:1090:1695564675201:1706073209487"]},"author_link":[],"item_1692929429513":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":" 再使用ロケットの実用化において，エンジンコンポーネントの寿命予測技術の確立は急務である。燃焼器の熱疲労寿命の予測もその一つである。但し，燃焼器の熱疲労寿命に関するデータは皆無であることから，低コストで行える燃焼器熱疲労寿命試験方法を検討し，実際に試行した。低コスト化の範囲は，供試体製作から推進剤や冷却剤といった試験費の低減まで含む。また，予測には解析技術が必要となるが，FEM を用いた熱疲労寿命解析を行い，試験結果との比較を行ったのでそれらをまとめて報告する。","subitem_description_language":"ja","subitem_description_type":"Other"},{"subitem_description":" Reusable rocket engine technologies have been researched and developed in JAXA Kakuda Space Center. A regeneratively cooled combustion chamber is one of the critical components that determines rocket engine life. Therefore, the low-cost thermal fatigue life test method using a sub-scale annular combustion chamber was investigated and the test was conducted. The test method and the results are reported. ","subitem_description_language":"en","subitem_description_type":"Other"}]},"item_1692929640552":{"attribute_name":"内容記述","attribute_value_mlt":[{"subitem_description":"形態: カラー図版あり","subitem_description_language":"ja","subitem_description_type":"Other"},{"subitem_description":"Physical  characteristics: Original contains color illustrations","subitem_description_language":"en","subitem_description_type":"Other"}]},"item_1693474141533":{"attribute_name":"資料番号(Local)","attribute_value_mlt":[{"subitem_relation_type_id":{"subitem_relation_type_id_text":"資料番号: AA2330011000","subitem_relation_type_select":"Local"}}]},"item_1694684272217":{"attribute_name":"日付","attribute_value_mlt":[{"subitem_date_issued_datetime":"2023-11-27","subitem_date_issued_type":"Submitted"}]},"item_1695282775758":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_language":"ja","subitem_text_value":"宇宙航空研究開発機構研究開発部門第四研究ユニット  (JAXA)"},{"subitem_text_language":"ja","subitem_text_value":"宇宙航空研究開発機構研究開発部門第四研究ユニット  (JAXA)"},{"subitem_text_language":"ja","subitem_text_value":"宇宙航空研究開発機構研究開発部門第四研究ユニット  (JAXA)"},{"subitem_text_language":"ja","subitem_text_value":"株式会社日立ソリューションズ東日本"},{"subitem_text_language":"en","subitem_text_value":"Research Unit IV, Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Research Unit IV, Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Research Unit IV, Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Hitachi Solutions East Japan, LTD."}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2024-01-29","bibliographicIssueDateType":"Issued"},"bibliographicNumberOfPages":"14","bibliographicVolumeNumber":"JAXA-RM-23-005","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構研究開発資料","bibliographic_titleLang":"ja"},{"bibliographic_title":"JAXA Research and Development Memorandum","bibliographic_titleLang":"en"}]}]},"item_3_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: JAXA-RM-23-005","subitem_description_language":"ja","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 (JAXA)","subitem_publisher_language":"ja"},{"subitem_publisher":"Japan Aerospace Exploration Agency (JAXA)","subitem_publisher_language":"en"}]},"item_3_source_id_22":{"attribute_name":"ISSN ONLINE","attribute_value_mlt":[{"subitem_source_identifier":"2433-2224","subitem_source_identifier_type":"EISSN"}]},"item_3_version_type_30":{"attribute_name":"著者版フラグ","attribute_value_mlt":[{"subitem_version_resource":"http://purl.org/coar/version/c_970fb48d4fbd8a85","subitem_version_type":"VoR"}]},"item_access_right":{"attribute_name":"アクセス権","attribute_value_mlt":[{"subitem_access_right":"open access","subitem_access_right_uri":"http://purl.org/coar/access_right/c_abf2"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorAffiliations":[{"affiliationNames":[{"affiliationName":"宇宙航空研究開発機構 (JAXA)","affiliationNameLang":"ja"},{"affiliationName":"Japan Aerospace Exploration Agency (JAXA)","affiliationNameLang":"en"}]}],"creatorNames":[{"creatorName":"森谷, 信一","creatorNameLang":"ja"},{"creatorName":"MORIYA, Shinichi","creatorNameLang":"en"}]},{"creatorAffiliations":[{"affiliationNames":[{"affiliationName":"宇宙航空研究開発機構 (JAXA)","affiliationNameLang":"ja"},{"affiliationName":"Japan Aerospace Exploration Agency (JAXA)","affiliationNameLang":"en"}]}],"creatorNames":[{"creatorName":"齋藤, 俊仁","creatorNameLang":"ja"},{"creatorName":"SAITO, Toshihito","creatorNameLang":"en"}]},{"creatorAffiliations":[{"affiliationNames":[{"affiliationName":"宇宙航空研究開発機構 (JAXA)","affiliationNameLang":"ja"},{"affiliationName":"Japan Aerospace Exploration Agency (JAXA)","affiliationNameLang":"en"}]}],"creatorNames":[{"creatorName":"木村, 俊哉","creatorNameLang":"ja"},{"creatorName":"KIMURA, Toshiya","creatorNameLang":"en"}]},{"creatorAffiliations":[{"affiliationNames":[{"affiliationName":"株式会社日立ソリューションズ東日本","affiliationNameLang":"ja"},{"affiliationName":"Hitachi Solutions East Japan, LTD.","affiliationNameLang":"en"}]}],"creatorNames":[{"creatorName":"高橋, 正晴","creatorNameLang":"ja"},{"creatorName":"TAKAHASHI, Masaharu","creatorNameLang":"en"}]}]},"item_files":{"attribute_name":"ファイル情報","attribute_type":"file","attribute_value_mlt":[{"accessrole":"open_date","date":[{"dateType":"Available","dateValue":"2024-01-29"}],"filename":"AA2330011000.pdf","format":"application/pdf","mimetype":"application/pdf","url":{"url":"https://jaxa.repo.nii.ac.jp/record/2000210/files/AA2330011000.pdf"},"version_id":"3c375827-2cc0-4401-9c91-3c837d48362a"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"Rocket Engine","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Combustion Chamber","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Thermal Fatigue Life","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Linear Damage Rule","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":"円筒型サブスケールロケットエンジン燃焼室を用いた熱疲労寿命に関する実験的研究","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"円筒型サブスケールロケットエンジン燃焼室を用いた熱疲労寿命に関する実験的研究","subitem_title_language":"ja"},{"subitem_title":"Experimental study on thermal fatigue life of rocket engine combustion chamber by using annular type sub-scale chamber","subitem_title_language":"en"}]},"item_type_id":"40003","owner":"27","path":["1706073209487","1893"],"pubdate":{"attribute_name":"PubDate","attribute_value":"2024-01-29"},"publish_date":"2024-01-29","publish_status":"0","recid":"2000210","relation_version_is_last":true,"title":["円筒型サブスケールロケットエンジン燃焼室を用いた熱疲労寿命に関する実験的研究"],"weko_creator_id":"27","weko_shared_id":-1},"updated":"2024-01-25T05:49:22.011832+00:00"}