{"created":"2023-06-20T14:39:36.016933+00:00","id":6350,"links":{},"metadata":{"_buckets":{"deposit":"2a678e59-5a57-44f0-a04c-5762b766489e"},"_deposit":{"created_by":1,"id":"6350","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"6350"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00006350","sets":["1887:1891","9:789:1031:1066"]},"author_link":["32175","32178","32177","32173","32176","32174"],"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2005-08-01","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"279","bibliographicPageStart":"272","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":"Space plasma can build up high differential potentials on satellite surfaces resulting in Electrostatic Discharges (ESD), sometimes causing anomalous behavior of satellite systems. As these phenomena give rise to possible risks affecting the performance of satellite, the charging is one of major concerns for satellite manufacturers. It has been investigated the influence of charging phenomena on satellite systems and its mitigation techniques. Our activities include not only investigation of influences on power systems but also that of other risks such as Electromagnetic Compatibility (EMC) or immediate surge to electronic device. In this paper, some of our assessments and the concerned problems are reported. It is obvious that international standardized guidelines for designing satellite systems against ESD will be established in the near future. It would be desirable if the requirements shall be appropriate and practical for satellite systems design, manufacturing and testing.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0049206035","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":"三菱電機 鎌倉製作所　宇宙システム部"},{"subitem_text_value":"三菱電機 鎌倉製作所　宇宙システム部"},{"subitem_text_value":"三菱電機 鎌倉製作所　相模工場"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Electric Corporation Space Systems Department, Kamakura Works"},{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Electric Corporation Space Systems Department, Kamakura Works"},{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Electric Corporation Sagami Factory, Kamakura Works"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"小野寺, 範義"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"村上, 洋一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"小圷, 秀明"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Onodera, Noriyoshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Murakami, Yoichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Koakutsu, Hideaki","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":"49206035.pdf","filesize":[{"value":"2.4 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"49206035.pdf","url":"https://jaxa.repo.nii.ac.jp/record/6350/files/49206035.pdf"},"version_id":"9e1fa904-38c7-4723-b91c-6ab2c0341509"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"衛星設計","subitem_subject_scheme":"Other"},{"subitem_subject":"静電放電","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":"宇宙プラズマ","subitem_subject_scheme":"Other"},{"subitem_subject":"電磁干渉","subitem_subject_scheme":"Other"},{"subitem_subject":"宇宙機電子機器","subitem_subject_scheme":"Other"},{"subitem_subject":"設計指針","subitem_subject_scheme":"Other"},{"subitem_subject":"電磁適合性","subitem_subject_scheme":"Other"},{"subitem_subject":"satellite design","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"electrostatic discharge","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":"space plasma","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"electromagnetic interference","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"spacecraft electronic equipment","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"design guideline","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"electromagnetic compatibility","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":"Robust design of satellite systems against spacecraft charging","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Robust design of satellite systems against spacecraft charging","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":"6350","relation_version_is_last":true,"title":["Robust design of satellite systems against spacecraft charging"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:57:22.541625+00:00"}