{"created":"2023-06-20T15:13:51.352653+00:00","id":43826,"links":{},"metadata":{"_buckets":{"deposit":"04dd8911-97d0-4d46-a6dc-4c626e6c35b4"},"_deposit":{"created_by":1,"id":"43826","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"43826"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00043826","sets":["1887:1893","1896:1898:1913:1916"]},"author_link":["465813","465812","465810","465808","465809","465811"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Dynamic Characteristics of Gimbal System of 300kg Thrust Liquid Propellant Rocket Engine (II) (Torques of gimbal bearing and feed pipes)"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1973-06","bibliographicIssueDateType":"Issued"},"bibliographicPageStart":"12","bibliographicVolumeNumber":"243","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所資料"},{"bibliographic_title":"Technical Memorandum of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The load torques of the gimbaI bearing and feed pipes of a liquid propellant gimbal rocket engine have an effect on the characteristics of swiveling of the engine. In order to analize swiveling motion of an engine and to design the gimbal system, it is need to find out the characteristics of each torques respectively. . The major purposes of this experiments are to obtain (1) the characteristics of torque due to the friction of gimbal bearings under thrust loads at slow swiveling angular velocity, (2) the characteristics of the torque due to the high pressure and momentum of mass flow in the propellant feed pipes.  The data obtained were presented in graphical forms, and an empirical equation on the characteristics of torque of a gimbal bearing was obtained.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALTM0243000","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 TM-243","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":"0452-2982","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":"AN00314334","subitem_source_identifier_type":"NCID"}]},"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"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"楢崎, 哲二"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"野溝, 国夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"荻原, 裟千夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"吉原, 正一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"NARASAKI, Tetsuji","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kunio, Nomizo","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":"2020-01-28"}],"displaytype":"detail","filename":"naltm00243.pdf","filesize":[{"value":"1.3 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltm00243.pdf","url":"https://jaxa.repo.nii.ac.jp/record/43826/files/naltm00243.pdf"},"version_id":"36c2a043-aef8-4049-a280-707c45eea40e"}]},"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300kgジンバル液体ロケットエンジンの揺動特性(Ⅱ)","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"推力300kgジンバル液体ロケットエンジンの揺動特性(Ⅱ)"}]},"item_type_id":"3","owner":"1","path":["1893","1916"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"43826","relation_version_is_last":true,"title":["推力300kgジンバル液体ロケットエンジンの揺動特性(Ⅱ)"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:07:14.698284+00:00"}