{"created":"2023-06-20T15:03:42.818273+00:00","id":32927,"links":{},"metadata":{"_buckets":{"deposit":"a8b4302b-00de-478c-b3e7-83b90ce4f6f3"},"_deposit":{"created_by":1,"id":"32927","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"32927"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00032927","sets":["1887:1890","1896:1898:1899:1912"]},"author_link":["412704","412703","412705","412706"],"item_9_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1986-10","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"136","bibliographicPageStart":"113","bibliographicVolumeNumber":"16","bibliographic_titles":[{"bibliographic_title":"宇宙科学研究所報告. 特集: 観測ロケット研究報告: M-3S型ロケット特集"}]}]},"item_9_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"M-3S型ロケットの主推進系は, M-3H型のそれと基本的に共通で, 第1段 : M-13モータと補助ブースタSB-310 8本, 第2段 : M-22モータ, および, 第3段 : M-3Aモータによって構成された。M-3H型との主な相違点は, 第1段姿勢制御の導入によりM-13モータのノズル部が再設計され比例制御LITVC装置が付加装備されたこと, および, M-3Aモータに改良設計が加えられ逐次性能向上が図られたことにある。M-3S型ロケットの機体構成と主要寸法を第1図に, 各号機の質量諸元を第1表に示す。各段モータの公称性能諸元を第2表に, それらの標準真空推力曲線を第2図に示す。M-3S推進系の改良・性能向上に関連して, 2回の地上燃焼試験 : M-13-2 TVC SLTおよびM-3A改SPIN HATが行われた。前者はM-3Sシリーズ以降これに続くM-3S IIシリーズでも継続使用されているM-3S型M-13モータの飛翔型試作モータの大気燃焼試験であり, 後者はM-3S-4でEXOS-Cを準極軌道に投入するために搭載されたM-3Aモータの最終性能向上型M-3A_4の基礎試作モータの高空性能試験である。","subitem_description_type":"Abstract"}]},"item_9_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: SA0166741000","subitem_description_type":"Other"}]},"item_9_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙科学研究所"}]},"item_9_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Institute of Space and Astronautical Science"}]},"item_9_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0285-9920","subitem_source_identifier_type":"ISSN"}]},"item_9_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AN00354485","subitem_source_identifier_type":"NCID"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"倉谷, 健治"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"秋葉, 鐐二郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"岩間, 彬"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"高野, 雅弘"}],"nameIdentifiers":[{}]}]},"item_files":{"attribute_name":"ファイル情報","attribute_type":"file","attribute_value_mlt":[{"accessrole":"open_date","date":[{"dateType":"Available","dateValue":"2020-01-24"}],"displaytype":"detail","filename":"SA0166741.pdf","filesize":[{"value":"1.5 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"SA0166741.pdf","url":"https://jaxa.repo.nii.ac.jp/record/32927/files/SA0166741.pdf"},"version_id":"0ae23799-7999-4241-aaa7-2075115eadb8"}]},"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":"departmental bulletin paper","resourceuri":"http://purl.org/coar/resource_type/c_6501"}]},"item_title":"M-3S のロケット・モータ","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"M-3S のロケット・モータ"}]},"item_type_id":"9","owner":"1","path":["1890","1912"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"32927","relation_version_is_last":true,"title":["M-3S のロケット・モータ"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T00:20:20.307577+00:00"}