{"created":"2023-06-20T15:14:53.734220+00:00","id":44910,"links":{},"metadata":{"_buckets":{"deposit":"2b69a8e5-901a-464b-9582-00eed2746f95"},"_deposit":{"created_by":1,"id":"44910","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"44910"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00044910","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["471901","471905","471912","471909","471898","471906","471913","471902","471914","471908","471900","471915","471903","471911","471897","471899","471916","471907","471910","471904"],"item_3_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"推力大きさ制御型固体ロケットモータの燃焼実験(第2報300φ球型内面燃焼方式)"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1981-02","bibliographicIssueDateType":"Issued"},"bibliographicPageStart":"34","bibliographicVolumeNumber":"654","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所報告"},{"bibliographic_title":"Technical Report of National Aerospace Laboratory TR-654","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"300-mm-diameter thrust controllable spherical solid rocket motors with 27kg weight propellant were successfully fired under the atmospheric condition for positive extinguishment. A modified rod-in-tube grain configuration was applied in an extended spherical rocket motor for getting a neutral burning and high propellant loading fraction. Ablative material with low emissivity and low ablative temperature was applied as an insulation liner because of its desirable properties for combustion extinction. Extinguishments occured at the end of the thrust pulses during the operation time of approximately 20 seconds when the control valve of the injectant was shut down. Post-fire examination of the hardware indicated that all components were in excellent condition.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALTR0654000","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-654","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"},{"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":"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":"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)"},{"subitem_text_language":"en","subitem_text_value":"Kakuda Branch Office, National Aerospace 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Motors","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Firing Tests of Thrust Controllable Solid Rocket Motors Part II:300-mm-Diameter Spherical Grain Motors","subitem_title_language":"en"}]},"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":"44910","relation_version_is_last":true,"title":["Firing Tests of Thrust Controllable Solid Rocket Motors Part II:300-mm-Diameter Spherical Grain Motors"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:48:41.738571+00:00"}