{"created":"2023-06-20T14:39:17.160338+00:00","id":6012,"links":{},"metadata":{"_buckets":{"deposit":"b4445127-eee5-4bcc-babb-398ffd2db2a4"},"_deposit":{"created_by":1,"id":"6012","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"6012"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00006012","sets":["1887:1893","9:789:998:1028"]},"author_link":["29889","29887","29888","29890"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"A new solar-proton fluence model for ISO specification"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2006-11-01","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"132","bibliographicPageStart":"129","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":"Solar energetic protons degrade performance and reliability of spacecraft systems, such as single-event effects, total dose effects of electronic components, and especially displacement damage of solar cell. On designing a solar cell panel, a low-energetic solar proton fluence model is needed to estimate radiation damage over mission life. Nowadays solar panel area of spacecraft is increasing as spacecraft mission life becomes longer (15-18 years). Thus an accurate solar proton model is strongly required for the cost-minimum design from the aerospace industry. The solar proton flux model, JPL-91 proposed by Feynman et al., is currently used widely for solar cell designing. However, it is known that the JPL-91 model predicts higher fluence of protons than values actually experienced in space, especially after seven years on orbit. In addition, the model is based on several assumptions on solar proton events, and also needs Monte-Carlo simulations for calculating fluence. In this study, we propose a new solar-proton model especially focused on solar cell designing. The newly-proposed model is an empirical model, which is constructed directly upon proton flux measurement data taken by instruments onboard spacecraft. This method has no assumptions or no dependence on solar-proton event selection both of which are needed in JPL-91. Our model shows lower fluence in longer missions compared to JPL-91. This model has been proposed to ISO (International Organization for Standardization) and has been discussed as a new standard solar-proton model.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0049500028","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"}]},"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"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"風間, 洋一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"五家, 建夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kazama, Yoichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Goka, Tateo","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":"49500028.pdf","filesize":[{"value":"328.0 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"49500028.pdf","url":"https://jaxa.repo.nii.ac.jp/record/6012/files/49500028.pdf"},"version_id":"a3170224-3aac-42ac-87ee-6a176680d131"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"太陽陽子","subitem_subject_scheme":"Other"},{"subitem_subject":"性能劣化","subitem_subject_scheme":"Other"},{"subitem_subject":"フルーエンス","subitem_subject_scheme":"Other"},{"subitem_subject":"宇宙機電子機器","subitem_subject_scheme":"Other"},{"subitem_subject":"宇宙機環境","subitem_subject_scheme":"Other"},{"subitem_subject":"航空宇宙環境","subitem_subject_scheme":"Other"},{"subitem_subject":"太陽電池設計","subitem_subject_scheme":"Other"},{"subitem_subject":"寿命","subitem_subject_scheme":"Other"},{"subitem_subject":"太陽放射","subitem_subject_scheme":"Other"},{"subitem_subject":"solar proton","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"performance degradation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"fluence","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"spacecraft electronic equipment","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"spacecraft environment","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerospace environment","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"solar cell design","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"life","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"solar radiation","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":"国際標準規格のための新しい太陽陽子フルーエンスモデルの提案","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"国際標準規格のための新しい太陽陽子フルーエンスモデルの提案"}]},"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":"6012","relation_version_is_last":true,"title":["国際標準規格のための新しい太陽陽子フルーエンスモデルの提案"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T08:04:11.546470+00:00"}