{"created":"2023-06-20T15:14:34.593891+00:00","id":44561,"links":{},"metadata":{"_buckets":{"deposit":"5dda2850-de4b-4d75-a52f-c0ddff986239"},"_deposit":{"created_by":1,"id":"44561","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"44561"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00044561","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["470076","470082","470081","470085","470084","470086","470083","470078","470079","470087","470080","470077"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Relation between the compositional variables and the pressure exponent of controllable solid rocket propellants"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1973-04","bibliographicIssueDateType":"Issued"},"bibliographicPageStart":"19","bibliographicVolumeNumber":"316","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所報告"},{"bibliographic_title":"Technical Report of National Aerospace Laboratory TR-316","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Experimental investigation of the pressure exponent in burning rate rule was conducted in order to find desirable propellants for controllable solid rockets. In strand and motor firings, partial replacement of ammonium perchlorate with potassium perchlorate, unimodal size distribution and finer particle size of oxidizers, lower loading fraction of binder, polybutadiene binder, and limited addition of aluminium were effective in obtaining higher pressure exponent of the composite propellants. The compositional effect on pressure exponent was explained by combustion mechanism considerations and granular diffusion flame theory.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALTR0316000","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: NAL TR-316","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"航空宇宙技術研究所"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"National Aerospace Laboratory(NAL)"}]},"item_3_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0389-4010","subitem_source_identifier_type":"ISSN"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"航空宇宙技術研究所宇宙研究グループ"},{"subitem_text_value":"航空宇宙技術研究所宇宙研究グループ"},{"subitem_text_value":"航空宇宙技術研究所宇宙研究グループ"},{"subitem_text_value":"航空宇宙技術研究所宇宙研究グループ"},{"subitem_text_value":"航空宇宙技術研究所宇宙研究グループ"},{"subitem_text_value":"航空宇宙技術研究所宇宙研究グループ"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Space Technology Research Group, National Aerospace Laboratory(NAL)"},{"subitem_text_language":"en","subitem_text_value":"Space Technology Research Group, National Aerospace Laboratory(NAL)"},{"subitem_text_language":"en","subitem_text_value":"Space Technology Research Group, National Aerospace Laboratory(NAL)"},{"subitem_text_language":"en","subitem_text_value":"Space Technology Research Group, National Aerospace Laboratory(NAL)"},{"subitem_text_language":"en","subitem_text_value":"Space Technology Research Group, National Aerospace Laboratory(NAL)"},{"subitem_text_language":"en","subitem_text_value":"Space Technology Research Group, National Aerospace Laboratory(NAL)"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"五代, 富文"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"清水, 盛生"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"伊藤, 克弥"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"西村, 久男"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"種村, 利春"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"藤原, 勉"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"GODAI, Tomifumi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"SHIMIZU, Morio","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"ITO, Katsuya","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"NISHIMURA, Hisao","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"TANEMURA, Toshiharu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"FUJIWARA, Tsutomu","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":"2020-01-29"}],"displaytype":"detail","filename":"naltr00316.pdf","filesize":[{"value":"3.4 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr00316.pdf","url":"https://jaxa.repo.nii.ac.jp/record/44561/files/naltr00316.pdf"},"version_id":"6cbe45b5-8487-4c87-bfb8-f0c755ca776c"}]},"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":"推力中断型固体ロケット用プロペラントの組成と圧力指数の関係","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"推力中断型固体ロケット用プロペラントの組成と圧力指数の関係"}]},"item_type_id":"3","owner":"1","path":["1893","1917"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"44561","relation_version_is_last":true,"title":["推力中断型固体ロケット用プロペラントの組成と圧力指数の関係"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:54:57.329455+00:00"}