{"created":"2023-06-20T14:39:35.293990+00:00","id":6339,"links":{},"metadata":{"_buckets":{"deposit":"2df8e3a5-ed6a-47ab-91bf-c31c0376209d"},"_deposit":{"created_by":1,"id":"6339","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"6339"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00006339","sets":["1887:1891","9:789:1031:1066"]},"author_link":["32072","32073","32071","32075","32076","32077","32079","32080","32074","32078"],"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2005-08-01","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"191","bibliographicPageStart":"179","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":"Arcing on satellite solar array due to interaction with space plasma may cause permanent loss of satellite power, once the arc becomes permanent sustained arc. An arc on solar array becomes a secondary arc when solar array circuit is short-circuited and provides energy to the arc plasma. The permanent sustained arc, the final stage of the secondary arc, destroys a solar array string or the complete power circuits at the worst case. To investigate the threshold conditions for the secondary arc formation, laboratory tests are carried out in a xenon plasma chamber simulating LEO plasma environment with an external circuit simulating a spacecraft power system. Solar array coupon panels simulating the hot and return ends of a string circuit are tested for various combinations of string voltage and string current. Experimental results show that formation of secondary arc strongly depends on the string voltage and duration of secondary arc depends on the string current.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0049206024","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":"九州工業大学 工学部　電気工学科"},{"subitem_text_value":"九州工業大学 工学部　電気工学科"},{"subitem_text_value":"九州工業大学 工学部　電気工学科"},{"subitem_text_value":"九州工業大学 工学部　電気工学科"},{"subitem_text_value":"宇宙航空研究開発機構"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Kyushu Institute of Technology Department of Electrical Engineering, Faculty of Engineering"},{"subitem_text_language":"en","subitem_text_value":"Kyushu Institute of Technology Department of Electrical Engineering, Faculty of Engineering"},{"subitem_text_language":"en","subitem_text_value":"Kyushu Institute of Technology Department of Electrical Engineering, Faculty of Engineering"},{"subitem_text_language":"en","subitem_text_value":"Kyushu Institute of Technology Department of Electrical Engineering, Faculty of Engineering"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"Kim, Jeongho"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"麻生, 誠司"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"細田, 聡史"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Cho, Mengu"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"香河, 英史"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kim, Jeongho","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Aso, Seiji","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hosoda, Satoshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Cho, Mengu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kagawa, Hideshi","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":"49206024.pdf","filesize":[{"value":"1.3 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"49206024.pdf","url":"https://jaxa.repo.nii.ac.jp/record/6339/files/49206024.pdf"},"version_id":"f2082858-8104-4d0d-9044-7c49b2547815"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"アーク放電","subitem_subject_scheme":"Other"},{"subitem_subject":"低高度地球周回軌道","subitem_subject_scheme":"Other"},{"subitem_subject":"持続的アーク","subitem_subject_scheme":"Other"},{"subitem_subject":"宇宙機帯電","subitem_subject_scheme":"Other"},{"subitem_subject":"航空宇宙環境","subitem_subject_scheme":"Other"},{"subitem_subject":"太陽電池アレイ","subitem_subject_scheme":"Other"},{"subitem_subject":"宇宙機電力供給","subitem_subject_scheme":"Other"},{"subitem_subject":"閾条件","subitem_subject_scheme":"Other"},{"subitem_subject":"arc discharge","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"low Earth orbit","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"sustained arc","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"spacecraft charging","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerospace environment","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"solar array","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"spacecraft power supply","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"threshold condition","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":"Threshold conditions to induce the sustained arc on the solar array panel of LEO satellite","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Threshold conditions to induce the sustained arc on the solar array panel of LEO satellite","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":"6339","relation_version_is_last":true,"title":["Threshold conditions to induce the sustained arc on the solar array panel of LEO satellite"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:57:34.632190+00:00"}