{"created":"2023-06-20T14:39:00.485763+00:00","id":5672,"links":{},"metadata":{"_buckets":{"deposit":"3236280f-2db7-4a21-b92b-663a36adac8c"},"_deposit":{"created_by":1,"id":"5672","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"5672"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00005672","sets":["1887:1891","9:789:972:991"]},"author_link":["27807","27806","27804","27805"],"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2008-02-29","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"174","bibliographicPageStart":"168","bibliographicVolumeNumber":"JAXA-SP-07-008E","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構特別資料"},{"bibliographic_title":"JAXA Special Publication: Proceedings of Lectures and Workshop International: Recent Advances in Multidisciplinary Technology and Modeling","bibliographic_titleLang":"en"}]}]},"item_5_description_17":{"attribute_name":"抄録(英)","attribute_value_mlt":[{"subitem_description":"A theoretical model describing the chemical ablation of a solid rocket motor nozzle ablator by the alumina-carbon reaction is presented. An application of it to a typical solid rocket motor with a graphite nozzle ablator indicates a large influence of the reaction on the nozzle surface recession.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0063824017","subitem_description_type":"Other"}]},"item_5_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: JAXA-SP-07-008E","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"}]},"item_5_publisher_9":{"attribute_name":"出版者(英)","attribute_value_mlt":[{"subitem_publisher":"Japan Aerospace Exploration Agency 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裕"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Matsukawa, Yutaka","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sato, Yutaka","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":"63824017.pdf","filesize":[{"value":"629.9 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"63824017.pdf","url":"https://jaxa.repo.nii.ac.jp/record/5672/files/63824017.pdf"},"version_id":"345eac06-a614-4328-a8f7-ff67201cdabd"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"ノズル流","subitem_subject_scheme":"Other"},{"subitem_subject":"ロケットノズル","subitem_subject_scheme":"Other"},{"subitem_subject":"固体燃料ロケットエンジン","subitem_subject_scheme":"Other"},{"subitem_subject":"推進薬燃焼","subitem_subject_scheme":"Other"},{"subitem_subject":"ノズル形状","subitem_subject_scheme":"Other"},{"subitem_subject":"ノズル壁","subitem_subject_scheme":"Other"},{"subitem_subject":"アブレーション材料","subitem_subject_scheme":"Other"},{"subitem_subject":"後退","subitem_subject_scheme":"Other"},{"subitem_subject":"黒鉛","subitem_subject_scheme":"Other"},{"subitem_subject":"酸化アルミニウム","subitem_subject_scheme":"Other"},{"subitem_subject":"化学アブレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"nozzle flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"rocket nozzle","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"solid propellant rocket engine","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"propellant combustion","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"nozzle geometry","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"nozzle wall","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"ablative material","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"recession","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"graphite","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aluminum oxide","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"chemical ablation","subitem_subject_language":"en","subitem_subject_scheme":"Other"}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"eng"}]},"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":"Analytical evaluation of the solid rocket motor nozzle surface recession by the alumina-carbon reaction","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Analytical evaluation of the solid rocket motor nozzle surface recession by the alumina-carbon reaction","subitem_title_language":"en"}]},"item_type_id":"5","owner":"1","path":["991","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"5672","relation_version_is_last":true,"title":["Analytical evaluation of the solid rocket motor nozzle surface recession by the alumina-carbon reaction"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T08:09:35.734038+00:00"}