{"created":"2023-06-20T14:39:22.134447+00:00","id":6118,"links":{},"metadata":{"_buckets":{"deposit":"865319a9-dc91-40de-ba6b-158d020473a4"},"_deposit":{"created_by":1,"id":"6118","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"6118"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00006118","sets":["1887:1891","9:789:1031:1049"]},"author_link":["30577","30575","30578","30580","30579","30576"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Present status and future prospect of the VASIMR type plasma thruster"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2006-02-28","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"69","bibliographicPageStart":"64","bibliographicVolumeNumber":"JAXA-SP-05-020","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構特別資料: 2005年度宇宙関連プラズマ研究会講演集"},{"bibliographic_title":"JAXA Special Publication: Proceedings of Space Plasma Symposium 2005","bibliographic_titleLang":"en"}]}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"有人火星探査を目指した高性能の比推力可変電気推進機VASIMR(Variable Specific Impulse Magnetoplasma Rocket)がNASAを中心に提案され実用化研究が進められている。このシステムでは一定電力下で自由に推力と比推力の比を制御することが出来る。このシステムを実現するには高周波によるプラズマ流の加熱と磁気ノズルによるプラズマ流の加速が重要な2つの技術課題である。我々はHITOP装置を用いてこの2つの課題が実現可能であることを実験的に明らかにした、VASIMR型のプラズマ宇宙推進機の現状と課題について報告する。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"In the Variable Specific Impulse Magnetoplasma Rocket (VASIMR) project under development in NASA, it is proposed to control a ratio of specific impulse to thrust at constant power. Ion heating by electromagnetic waves and magnetic nozzle acceleration of fast-flowing plasma are two key issues for the development of the advanced space thruster. In the HITOP experiments, we have successfully demonstrated these two tasks experimentally. Present status and future tasks of the VASIMR-type plasma thruster is presented.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0049213009","subitem_description_type":"Other"}]},"item_5_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: JAXA-SP-05-020","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Japan Aerospace Exploration Agency (JAXA)"}]},"item_5_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"1349-113X","subitem_source_identifier_type":"ISSN"}]},"item_5_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AA11984031","subitem_source_identifier_type":"NCID"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"東北大学 大学院工学研究科"},{"subitem_text_value":"東北大学 大学院工学研究科"},{"subitem_text_value":"東北大学 大学院工学研究科"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Tohoku University Graduate School of Engineering"},{"subitem_text_language":"en","subitem_text_value":"Tohoku University Graduate School of Engineering"},{"subitem_text_language":"en","subitem_text_value":"Tohoku University Graduate School of Engineering"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"安藤, 晃"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"服部, 邦彦"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"犬竹, 正明"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ando, Akira","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hattori, Kunihiko","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Inutake, Masaaki","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":"2020-01-16"}],"displaytype":"detail","filename":"49213009.pdf","filesize":[{"value":"1.0 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"49213009.pdf","url":"https://jaxa.repo.nii.ac.jp/record/6118/files/49213009.pdf"},"version_id":"6a3a0c98-704f-46f1-9b9f-4c126ad142e1"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"VASIMR","subitem_subject_scheme":"Other"},{"subitem_subject":"プラズマ推進","subitem_subject_scheme":"Other"},{"subitem_subject":"イオン加熱","subitem_subject_scheme":"Other"},{"subitem_subject":"HITOP","subitem_subject_scheme":"Other"},{"subitem_subject":"磁気プラズマ発電アークジェット","subitem_subject_scheme":"Other"},{"subitem_subject":"MPDA","subitem_subject_scheme":"Other"},{"subitem_subject":"比推力","subitem_subject_scheme":"Other"},{"subitem_subject":"磁気ノズル","subitem_subject_scheme":"Other"},{"subitem_subject":"イオン温度","subitem_subject_scheme":"Other"},{"subitem_subject":"火星探査","subitem_subject_scheme":"Other"},{"subitem_subject":"ヘリカルアンテナ","subitem_subject_scheme":"Other"},{"subitem_subject":"プラズマ流","subitem_subject_scheme":"Other"},{"subitem_subject":"VASIMR","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"plasma propulsion","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"ion heating","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"HITOP","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"magneto-plasma-dynamic arcjet","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"MPDA","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"specific impulse","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"magnetic nozzle","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"ion temperature","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Mars exploration","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"helical antenna","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"plasma flow","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":"conference paper","resourceuri":"http://purl.org/coar/resource_type/c_5794"}]},"item_title":"VASIMR型プラズマ推進機の研究開発状況と課題","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"VASIMR型プラズマ推進機の研究開発状況と課題"}]},"item_type_id":"5","owner":"1","path":["1049","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"6118","relation_version_is_last":true,"title":["VASIMR型プラズマ推進機の研究開発状況と課題"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T08:01:54.312969+00:00"}