{"created":"2023-06-20T14:39:18.302024+00:00","id":6038,"links":{},"metadata":{"_buckets":{"deposit":"7dd07150-4533-4de3-90f9-30d2e0a7c6b9"},"_deposit":{"created_by":1,"id":"6038","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"6038"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00006038","sets":["1887:1893","9:789:998:1028"]},"author_link":["30047","30054","30052","30053","30050","30051","30048","30049"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Effects of discharge on backside of solar paddle on satellite power system"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2006-11-01","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"252","bibliographicPageStart":"247","bibliographicVolumeNumber":"JAXA-SP-06-006","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構特別資料: 平成18年度　宇宙航空研究開発機構　総合技術研究本部　宇宙科学研究本部　研究成果報告書"},{"bibliographic_title":"JAXA Special Publication: Report on Research Achievements for FY2006 Institute of Space and Astronautical Science, Institute of Aerospace Technology, Japan Aerospace Exploration Agency","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The surface potential depends on the plasma environment, the sunshine condition, the constituent material and so on. Therefore non-earthed surface materials on the satellite have the different potential from the satellite ground. As the differential potential builds up between two points, an arc may occur. The discharge is well known as causing the failure to the satellite power system, for instance, it is reported that the discharge sometimes causes loss of the power generation. So we should investigate the influence of the discharge on the orbit. When the charge with the high potential by the discharge is inputted to the power line or ground line, the transient voltage is applied to the base-emitter of the shunt transistor. This 'transient voltage' sometimes exceeds the level of the maximum rating voltage and breaks down the shunt transistor. We found that the breeder resistance and conductive adhesive were effective as a way of preventing this failure. In this paper, we show the analysis result about the effects of the discharge on the backside of the solar paddle on satellite power system.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0049500054","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-SP-06-006","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":"1349-113X","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":"AA11984031","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 総合技術研究本部"},{"subitem_text_value":"宇宙航空研究開発機構 総合技術研究本部"},{"subitem_text_value":"宇宙航空研究開発機構 総合技術研究本部"},{"subitem_text_value":"宇宙航空研究開発機構 総合技術研究本部"}]},"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 Aerospace Technology"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Institute of Aerospace Technology"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Institute of Aerospace Technology"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Institute of Aerospace Technology"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"瀬上, 剛"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"艸分, 宏昌"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"高橋, 真人"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"岐部, 公一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Segami, Go","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kusawake, Hiroaki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Takahashi, Masato","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kibe, Koichi","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":"49500054.pdf","filesize":[{"value":"626.9 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"49500054.pdf","url":"https://jaxa.repo.nii.ac.jp/record/6038/files/49500054.pdf"},"version_id":"ed732346-4b75-4442-8dda-d0dc344dd9f8"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"極軌道","subitem_subject_scheme":"Other"},{"subitem_subject":"ソーラーパドル","subitem_subject_scheme":"Other"},{"subitem_subject":"アーク放電","subitem_subject_scheme":"Other"},{"subitem_subject":"衛星電源システム","subitem_subject_scheme":"Other"},{"subitem_subject":"宇宙機帯電","subitem_subject_scheme":"Other"},{"subitem_subject":"オーロラ層","subitem_subject_scheme":"Other"},{"subitem_subject":"熱防御システム","subitem_subject_scheme":"Other"},{"subitem_subject":"表面電位","subitem_subject_scheme":"Other"},{"subitem_subject":"放電","subitem_subject_scheme":"Other"},{"subitem_subject":"回路","subitem_subject_scheme":"Other"},{"subitem_subject":"polar orbit","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"solar paddle","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"arc discharge","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"satellite power system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"spacecraft charging","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"auroral zone","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"thermal protection system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"surface potential","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"electric discharge","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"circuit","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":"衛星パドル裏面放電の電源システムへの影響解析","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"衛星パドル裏面放電の電源システムへの影響解析"}]},"item_type_id":"3","owner":"1","path":["1028","1893"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"6038","relation_version_is_last":true,"title":["衛星パドル裏面放電の電源システムへの影響解析"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T08:03:30.798469+00:00"}