{"created":"2023-06-20T14:35:59.501824+00:00","id":2285,"links":{},"metadata":{"_buckets":{"deposit":"a24b3cec-150c-4087-b58f-535b344099a8"},"_deposit":{"created_by":1,"id":"2285","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"2285"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00002285","sets":["1887:1893","9:10:256:295"]},"author_link":["4946","4944","4947","4945"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Feasibility study of small magnetic sail demonstration satellite"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2006-01-31","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"63","bibliographicPageStart":"57","bibliographicVolumeNumber":"JAXA-RR-05-014","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構研究開発報告: 磁気プラズマセイルの推力発生メカニズムの解明"},{"bibliographic_title":"JAXA Research and Development Report: Elucidation of Thrust Generation Mechanism of Magnetic Sail","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"150kgクラス小型衛星を利用した磁気セイル飛翔実験の検討を行なった。衛星は直径2mの超電導コイルとその制御・電源系から構成され、液体ヘリウム冷却系によって4K低温超電導状態を実現する。地球磁気圏のmagnetopauseは太陽側に10Re程度であるから、衛星を太陽風を受けるべく地球磁気圏の外側の領域に配置するために、小型固体モータにより太陽側に遠地点がある250km×20Re軌道に投入する。軌道投入後、液体ヘリウムによる冷却が有効なおよそ1週間、地球磁気圏外になる遠地点付近でのみ推力1μNクラスの磁気セイルを作動し、衛星軌道の変化から磁気セイルの推進性能を確認する。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"A 150-kg-class engineering satellite for the demonstration of magnetic sail was studied. When the satellite is inserted into an orbit whose perigee is out of the geomagnetic field, a 2-m-diameter superconducting coil is initiated by a battery discharge, obtaining 3-T magnetic field at the surface of the superconducting coil. The coil will be cooled by liquid helium cryostat, hence the coil operation is valid only while the liquid helium is kept, maybe a week or so; during this duration, the magnetic sail is expected to produce 1 micro N thrust. Although the thrust level is very small, it will be measured by a precise orbit determination so as to demonstrate the world's first thrust production of the magnetic sail in space.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0049193008","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-RR-05-014","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":"1349-1113","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":"AA1192675X","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 宇宙科学研究本部"},{"subitem_text_value":"宇宙航空研究開発機構 宇宙科学研究本部"}]},"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 and Astronautical Science"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Institute of Space and Astronautical Science"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"船木, 一幸"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"山川, 宏"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Funaki, Ikko","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yamakawa, Hiroshi","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":"49193008.pdf","filesize":[{"value":"699.3 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"49193008.pdf","url":"https://jaxa.repo.nii.ac.jp/record/2285/files/49193008.pdf"},"version_id":"cf568714-3977-438a-9c2c-9f37dd88ae01"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"磁気セイル","subitem_subject_scheme":"Other"},{"subitem_subject":"超電導磁石","subitem_subject_scheme":"Other"},{"subitem_subject":"可能性分析","subitem_subject_scheme":"Other"},{"subitem_subject":"小型衛星技術","subitem_subject_scheme":"Other"},{"subitem_subject":"磁気圏界面","subitem_subject_scheme":"Other"},{"subitem_subject":"伝導冷却","subitem_subject_scheme":"Other"},{"subitem_subject":"光圧","subitem_subject_scheme":"Other"},{"subitem_subject":"推力特性","subitem_subject_scheme":"Other"},{"subitem_subject":"磁場","subitem_subject_scheme":"Other"},{"subitem_subject":"液体ヘリウム","subitem_subject_scheme":"Other"},{"subitem_subject":"magnetic sail","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"superconducting magnet","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"feasibility analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"small satellite technology","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"magnetopause","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"conduction cooling","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"photon pressure","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"thrust performance","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"magnetic field","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"liquid helium","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":"小型磁気セイル飛翔実験の検討","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"小型磁気セイル飛翔実験の検討"}]},"item_type_id":"3","owner":"1","path":["295","1893"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"2285","relation_version_is_last":true,"title":["小型磁気セイル飛翔実験の検討"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T09:25:17.890223+00:00"}