{"created":"2023-06-20T15:14:46.972855+00:00","id":44784,"links":{},"metadata":{"_buckets":{"deposit":"ab055fa5-f9c3-4a7c-9c26-88039e024f0b"},"_deposit":{"created_by":1,"id":"44784","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"44784"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00044784","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["471232","471230","471233","471229","471231","471227","471228","471226"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Spinning Combustion Tests of 200mm-dia. Solid Propellant Rocket Motor"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1978-03","bibliographicIssueDateType":"Issued"},"bibliographicPageStart":"13","bibliographicVolumeNumber":"530","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所報告"},{"bibliographic_title":"Technical Report of National Aerospace Laboratory TR-530","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Spinning combustion tests for a 200mm-dia. class solid propellant rocket were conducted and compared with numerical results. The combustion surface obtained by the extinction test shows that the acceleration-produced burning effect is limited to the region having the angle 85.5 deg to 90 deg between the combustion surface and the acceleration vector. This angle extent was independent of the burning time and the grain configuration. The aspects of the combustion surface, together with the transient burning-rate augmentation data given by the strand experiment, were included in a model for computer programming of the predicted pressure-time diagram. The predicted pressure history and the variation of grain configuration with time show a qualitatively good comparison.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALTR0530000","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-530","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角田支所"},{"subitem_text_value":"航空宇宙技術研究所角田支所"},{"subitem_text_value":"航空宇宙技術研究所角田支所"},{"subitem_text_value":"航空宇宙技術研究所角田支所"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Kakuda Branch Office, National Aerospace Laboratory(NAL)"},{"subitem_text_language":"en","subitem_text_value":"Kakuda Branch Office, National Aerospace Laboratory(NAL)"},{"subitem_text_language":"en","subitem_text_value":"Kakuda Branch Office, National Aerospace Laboratory(NAL)"},{"subitem_text_language":"en","subitem_text_value":"Kakuda Branch Office, National Aerospace Laboratory(NAL)"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"泉川, 宗男"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"高橋, 守"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"三谷, 徹"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"新岡, 嵩"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"IZUMIKAWA, Muneo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"TAKAHASHI, Mamoru","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"MITANI, Tohru","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"NIIOKA, Takashi","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":"naltr00530.pdf","filesize":[{"value":"1.4 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr00530.pdf","url":"https://jaxa.repo.nii.ac.jp/record/44784/files/naltr00530.pdf"},"version_id":"7ea7f5ba-7414-41fa-94b7-cb0c12146c1a"}]},"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":"200mm径固体ロケットのスピン燃焼実験","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"200mm径固体ロケットのスピン燃焼実験"}]},"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":"44784","relation_version_is_last":true,"title":["200mm径固体ロケットのスピン燃焼実験"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:50:57.858626+00:00"}