{"created":"2023-06-20T15:13:49.070018+00:00","id":43787,"links":{},"metadata":{"_buckets":{"deposit":"9a012402-8a28-4a35-9907-b97014922a44"},"_deposit":{"created_by":1,"id":"43787","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"43787"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00043787","sets":["1887:1893","1896:1898:1913:1916"]},"author_link":["465585","465590","465586","465584","465591","465583","465588","465582","465587","465589"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Standard Ballistic Test Evaluation System for Solid Rocket Propellants"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1971-06","bibliographicIssueDateType":"Issued"},"bibliographicPageStart":"26","bibliographicVolumeNumber":"203","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":"An accurate and standard specific impulse measurement system with an overall error not exceeding 0.1% for solid rocket propellants is described. After investigating a con- ventional specific impulse measurement system existing at the National Aerospace Laboratory, some new design concepts, consideration of ballistic evaluation of a solid rocket motor, an accurate thrust stand, and electronic equipment and environmental conditions are discussed. The results of system tests, static calibration and motor firing tests are also described.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALTM0203000","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-203","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"},{"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":"五代, 富文"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"岡部, 裕二郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"清水, 昭紀"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"伊藤, 克弥"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"西村, 久男"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"GODAI, Tomifumi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"OKABE, Yujiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"SHIMIZU, Shoki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"ITO, Katsuya","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"NISHIMURA, Hisao","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":"naltm00203.pdf","filesize":[{"value":"3.4 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltm00203.pdf","url":"https://jaxa.repo.nii.ac.jp/record/43787/files/naltm00203.pdf"},"version_id":"cdfe6366-5854-4081-9075-2a45f81dcc86"}]},"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":"固体ロケットの比推力測定の標準化","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"固体ロケットの比推力測定の標準化"}]},"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":"43787","relation_version_is_last":true,"title":["固体ロケットの比推力測定の標準化"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:07:54.579982+00:00"}