{"created":"2023-06-20T15:14:38.124840+00:00","id":44620,"links":{},"metadata":{"_buckets":{"deposit":"b38a5cfc-fcf2-40cd-bff2-7ef7293f2199"},"_deposit":{"created_by":1,"id":"44620","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"44620"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00044620","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["470385","470382","470381","470386","470383","470384"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Pressure Histories of Spinning Solid Propellant Rocket Motors"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1974-06","bibliographicIssueDateType":"Issued"},"bibliographicPageStart":"24","bibliographicVolumeNumber":"372","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所報告"},{"bibliographic_title":"Technical Report of National Aerospace Laboratory TR-372","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The burning pressure-time diagrams were predicted and measured for the spinning solid propellant rocket motors of internal burning star configuration. To predict pressure histories the acceleration-induced and orientation dependent burning-rate augmentation data of a solid propellant from slab motor tests were entered into a grain regression program. Spin tests were conducted using the 140φ motor of the CMDB and composite propellants at spin rates of 0～870 rpm. The spinning full-scale motors were also tested by means of“Spinning Solid Propellant Rocket High Altitude Test Facility”of National Aerospace Laboratory, Kakuda Branch. The measured pressure histories were compared with the computed ones. Futhermore, the grain surface profiles obtained by the extinction test of the 140φ motor were also compared with the calculated ones.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALTR0372000","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-372","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":"角田支所"},{"subitem_text_value":"角田支所"},{"subitem_text_value":"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)"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"新岡, 嵩"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"石井, 進一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"三谷, 徹"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"NIIOKA, Takashi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"ISHII, Shinichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"MITANI, Tohru","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":"naltr00372.pdf","filesize":[{"value":"4.1 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr00372.pdf","url":"https://jaxa.repo.nii.ac.jp/record/44620/files/naltr00372.pdf"},"version_id":"0545da1b-bdf0-4436-9a6a-095b90c30daa"}]},"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":"スピンを与えた固体ロケットモータの燃焼圧力-時間曲線","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"スピンを与えた固体ロケットモータの燃焼圧力-時間曲線"}]},"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":"44620","relation_version_is_last":true,"title":["スピンを与えた固体ロケットモータの燃焼圧力-時間曲線"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:53:58.417341+00:00"}