{"created":"2023-06-20T14:36:13.410930+00:00","id":2534,"links":{},"metadata":{"_buckets":{"deposit":"068fc257-89f5-4c0d-81a5-3401f09b4ad7"},"_deposit":{"created_by":1,"id":"2534","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"2534"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00002534","sets":["1887:1893","9:1090:1186:1189"]},"author_link":["7049","7058","7057","7056","7053","7051","7052","7054","7050","7055"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Identification of Important Design Parameters for Rocket Turbopump Turbine by Using QFD"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2012-03-30","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"9","bibliographicPageStart":"1","bibliographicVolumeNumber":"JAXA-RM-11-021","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構研究開発資料"},{"bibliographic_title":"JAXA Research and Development Memorandum","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"An application of QFD (Quality Function Deployment) method for the design of rocket turbopump turbines is presented in this paper. Generally rocket turbopump turbines are designed as supersonic impulse turbines, and because of its special specifications, improvements on turbine efficiency and robustness is difficult. Further improvement on turbine design techniques is needed, because turbine performance directly affects engine performance and reliability in a liquid rocket propulsion system. The purpose of present work is to improve turbine design techniques by applying QFD method to the rocket turbopump turbines. In this presentation,  the QFD results for the identification of important design parameters and for the visualization of the market needs which was obtained from rocket engine stakeholders are discussed.","subitem_description_type":"Other"}]},"item_3_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_3_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_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0065218000","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-RM-11-021","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":"1349-1121","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":"AA11983593","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宇宙輸送ミッション本部宇宙輸送系推進技術研究開発センターエンジン研究開発グループ (JAXA)"},{"subitem_text_value":"テラ・コンサルティング"},{"subitem_text_value":"岩手大学工学部"},{"subitem_text_value":"宇宙航空研究開発機構宇宙輸送ミッション本部宇宙輸送系推進技術研究開発センターエンジン研究開発グループ (JAXA)"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Engine System Research and Development Group, Space Transportation Propulsion Research and Development Center, Space Transportation Mission Directorate, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Terra-Consulting"},{"subitem_text_language":"en","subitem_text_value":"Faculty of Engineering, Iwate University"},{"subitem_text_language":"en","subitem_text_value":"Engine System Research and Development Group, Space Transportation Propulsion Research and Development Center, Space Transportation Mission Directorate, Japan Aerospace Exploration Agency (JAXA)"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"瀧田, 純也"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"福岡, 勝"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"國枝, 麿"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"船崎, 健一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"内海, 政春"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Takida, Junya","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Fukuoka, Masaru","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kunieda, Maro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Funazaki, Kenichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Uchimi, Masaharu","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":"2020-01-15"}],"displaytype":"detail","filename":"65218000.pdf","filesize":[{"value":"1.0 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"65218000.pdf","url":"https://jaxa.repo.nii.ac.jp/record/2534/files/65218000.pdf"},"version_id":"7ed1cb89-1c0d-4e89-9662-3becab1b0507"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"Quality Function Deployment","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Market needs","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Important Design Parameter","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Supersonic Impulse Turbine","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":"QFD を用いたロケットターボポンプ用タービンの重要設計パラメータの抽出","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"QFD を用いたロケットターボポンプ用タービンの重要設計パラメータの抽出"}]},"item_type_id":"3","owner":"1","path":["1189","1893"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"2534","relation_version_is_last":true,"title":["QFD を用いたロケットターボポンプ用タービンの重要設計パラメータの抽出"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T09:20:39.225308+00:00"}