{"created":"2023-06-20T14:39:37.733218+00:00","id":6386,"links":{},"metadata":{"_buckets":{"deposit":"c56687a6-a414-4a66-886f-1877444fe19d"},"_deposit":{"created_by":1,"id":"6386","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"6386"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00006386","sets":["1887:1891","9:789:1031:1066"]},"author_link":["32389","32388"],"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2005-08-01","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"652","bibliographicPageStart":"633","bibliographicVolumeNumber":"JAXA-SP-05-001E","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構特別資料"},{"bibliographic_title":"JAXA Special Publication: 9th Spacecraft Charging Technology Conference","bibliographic_titleLang":"en"}]}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Recently, lots of electric thruster are in practical use because of their high specific impulses suitable for long space missions. The exhaust plasma plume characteristics strongly depend on thruster species. In this study, three kinds of plasma thruster were investigated in order to understand their plasma plume characteristics concerned with thruster performance and spacecraft interaction. Several plasma diagnostic measurements were carried out. The laboratory-model low-power Hall-effect thruster THT-4, the low-power radiation-cooled arcjet thruster RAT-7 and the quasisteady Magnetoplasmadynamic (MPD) arcjet thruster MY-3 were operated, and their performances and plasma characteristics are discussed.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0049206071","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-05-001E","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":"大阪大学 大学院基礎工学研究科"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Osaka University Graduate School of Engineering Science"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"田原, 弘一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tahara, Hirokazu","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":"49206071.pdf","filesize":[{"value":"5.0 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"49206071.pdf","url":"https://jaxa.repo.nii.ac.jp/record/6386/files/49206071.pdf"},"version_id":"46b06613-fc4d-46c0-9c7a-c471c12f7610"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"宇宙機推進","subitem_subject_scheme":"Other"},{"subitem_subject":"電気推進","subitem_subject_scheme":"Other"},{"subitem_subject":"比推力","subitem_subject_scheme":"Other"},{"subitem_subject":"プラズマスラスタ","subitem_subject_scheme":"Other"},{"subitem_subject":"プラズマプルーム","subitem_subject_scheme":"Other"},{"subitem_subject":"ホールスラスタ","subitem_subject_scheme":"Other"},{"subitem_subject":"アークジェットスラスタ","subitem_subject_scheme":"Other"},{"subitem_subject":"電磁プラズマ力スラスタ","subitem_subject_scheme":"Other"},{"subitem_subject":"プラズマ相互作用","subitem_subject_scheme":"Other"},{"subitem_subject":"spacecraft propulsion","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"electric propulsion","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"specific impulse","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"plasma thruster","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"plasma plume","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Hall thruster","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"arcjet thruster","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"magnetoplasmadynamic thruster","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"plasma interaction","subitem_subject_language":"en","subitem_subject_scheme":"Other"}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"eng"}]},"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":"Plasma plume characteristics of electric thrusters","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Plasma plume characteristics of electric thrusters","subitem_title_language":"en"}]},"item_type_id":"5","owner":"1","path":["1066","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"6386","relation_version_is_last":true,"title":["Plasma plume characteristics of electric thrusters"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:56:43.038051+00:00"}