{"created":"2023-06-20T14:36:24.051833+00:00","id":2714,"links":{},"metadata":{"_buckets":{"deposit":"34a404b0-5e8a-4047-8a07-5ec2070d1af9"},"_deposit":{"created_by":1,"id":"2714","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"2714"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00002714","sets":["1887:1893","9:1090:1311:1324"]},"author_link":["8490","8492","8489","8494","8493","8488","8491","8487"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Fruitful results of MicroLabSat and ambitious development of MicroLabSat 2"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2004-10-29","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"114","bibliographicPageStart":"109","bibliographicVolumeNumber":"JAXA-RM-04-010","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構研究開発資料: 平成15年度総合技術研究本部宇宙領域研究成果報告書:衛星系"},{"bibliographic_title":"JAXA Research and Development Memorandum: FY15 Annual Report of Research & Development on Space Technology in the Institute of Space Technology and Aeronautics: Satellite System","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The Space Technology Demonstration Research Center in JAXA has researched on the development of 50 to 100 kg class small satellites which is used to carry newly-developed components and devices into space and to check their normal work. There is a plan to develop several types of such small 'space demonstration satellites' as a series. MicroLabSat, the first one of the series, is a 50 kg class of spin stabilized satellite launched in December 2002 as a piggy back satellite on H-2A rocket. It has successfully completed all the planned experiments and continues healthy operation. Following MicroLabSat, MicroLabSat 2 is being developed with the three axis stabilized attitude control system. The results of two satellites will be brought into the following space demonstration satellites of the series. The fruitful results of MicroLabSat and the recent status of developing MicroLabSat 2 will be expressed in this paper.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0048057023","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: JAXA-RM-04-010","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Japan Aerospace Exploration Agency (JAXA)"}]},"item_3_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"1349-1121","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":"AA11983593","subitem_source_identifier_type":"NCID"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"宇宙航空研究開発機構 総合技術研究本部"},{"subitem_text_value":"宇宙航空研究開発機構 総合技術研究本部"},{"subitem_text_value":"宇宙航空研究開発機構 総合技術研究本部"},{"subitem_text_value":"宇宙航空研究開発機構 総合技術研究本部"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"立原, 裕司"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"高橋, 伸宏"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"吉原, 圭介"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"橋本, 英一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tachihara, Hiroshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Takahashi, Nobuhiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yoshihara, Keisuke","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hashimoto, Hidekazu","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":"2020-01-15"}],"displaytype":"detail","filename":"48057023.pdf","filesize":[{"value":"2.9 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"48057023.pdf","url":"https://jaxa.repo.nii.ac.jp/record/2714/files/48057023.pdf"},"version_id":"66c9d597-4ee3-4cab-bd05-d8b89b13a965"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"MicroLabSat-2","subitem_subject_scheme":"Other"},{"subitem_subject":"H-2Aロケット","subitem_subject_scheme":"Other"},{"subitem_subject":"姿勢制御","subitem_subject_scheme":"Other"},{"subitem_subject":"マイクロ衛星","subitem_subject_scheme":"Other"},{"subitem_subject":"ピギーバックシステム","subitem_subject_scheme":"Other"},{"subitem_subject":"Ni-MH電池","subitem_subject_scheme":"Other"},{"subitem_subject":"磁気嵐","subitem_subject_scheme":"Other"},{"subitem_subject":"衛星通信","subitem_subject_scheme":"Other"},{"subitem_subject":"MicroLabSat-2","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"H-2A rocket","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"attitude control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"microsatellite","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"piggyback system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Ni-MH battery","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"magnetic storm","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"satellite communication","subitem_subject_language":"en","subitem_subject_scheme":"Other"}]},"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":"マイクロラブサットシリーズの成果と展望:1号機の成果と2号機設計状況","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"マイクロラブサットシリーズの成果と展望:1号機の成果と2号機設計状況"}]},"item_type_id":"3","owner":"1","path":["1324","1893"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"2714","relation_version_is_last":true,"title":["マイクロラブサットシリーズの成果と展望:1号機の成果と2号機設計状況"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T09:17:19.840973+00:00"}