{"created":"2023-06-20T14:39:34.597774+00:00","id":6324,"links":{},"metadata":{"_buckets":{"deposit":"0a988dd9-9c36-4198-9aff-983be4ac59af"},"_deposit":{"created_by":1,"id":"6324","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"6324"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00006324","sets":["1887:1891","9:789:1031:1066"]},"author_link":["31953","31952"],"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2005-08-01","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"81","bibliographicPageStart":"75","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":"As satellite power levels of advanced spacecraft climb above 20-50 kW, higher solar array operating voltages become attractive. For Solar Power Satellites, voltages well above 1,000 V have been suggested. However, micrometeoroid impacts on such high voltage arrays may have catastrophic results. To assess these effects, contemporary GaAs modules and samples of the Stretched Lens Array (SLA) modules were exposed to hypervelocity impact with 100 micrometer diameter soda lime glass spheres at velocities up to 12 km/sec. The two strings of GaAs cells were held at differential voltages above 60 V and bias voltages near - 200 V. A plasma environment typical of Low Earth Orbit (LEO) was also present. The SLA was held at bias voltages up to - 1,000 V. Several types of arcs were observed in the GaAs strings. Higher bias voltages were limited by lack of cover glass overhang, but in the case of the SLA no arcing occurred.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0049206009","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":"Auburn University Space Research Inst., 231 Leach Center"},{"subitem_text_value":"Auburn University Space Research Inst., 231 Leach Center"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Auburn University Space Research Institute, 231 Leach Center"},{"subitem_text_language":"en","subitem_text_value":"Auburn University Space Research Institute, 231 Leach Center"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"Brandhorst, Henry W.  Jr.","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Best, Stevie R.","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":"49206009.pdf","filesize":[{"value":"3.5 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"49206009.pdf","url":"https://jaxa.repo.nii.ac.jp/record/6324/files/49206009.pdf"},"version_id":"06337e43-704a-4eb4-9de8-29b654f44ccd"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"宇宙機設計","subitem_subject_scheme":"Other"},{"subitem_subject":"太陽電池アレイ","subitem_subject_scheme":"Other"},{"subitem_subject":"太陽発電衛星","subitem_subject_scheme":"Other"},{"subitem_subject":"放電","subitem_subject_scheme":"Other"},{"subitem_subject":"流星塵衝突","subitem_subject_scheme":"Other"},{"subitem_subject":"超高速衝突","subitem_subject_scheme":"Other"},{"subitem_subject":"太陽電池","subitem_subject_scheme":"Other"},{"subitem_subject":"プラズマ環境","subitem_subject_scheme":"Other"},{"subitem_subject":"航空宇宙環境","subitem_subject_scheme":"Other"},{"subitem_subject":"spacecraft design","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"solar array","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"solar power satellite","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"electric discharge","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"micrometeoroid impact","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"hypervelocity impact","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"solar cell","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"plasma environment","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerospace environment","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":"Hypervelocity impact testing of solar cells in a plasma environment","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Hypervelocity impact testing of solar cells in a plasma environment","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":"6324","relation_version_is_last":true,"title":["Hypervelocity impact testing of solar cells in a plasma environment"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:57:51.404836+00:00"}