{"created":"2023-06-20T14:39:36.791257+00:00","id":6365,"links":{},"metadata":{"_buckets":{"deposit":"55b3cdbe-8e96-4d14-a48c-78e05d870046"},"_deposit":{"created_by":1,"id":"6365","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"6365"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00006365","sets":["1887:1891","9:789:1031:1066"]},"author_link":["32253","32249","32250","32251","32252"],"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2005-08-01","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"460","bibliographicPageStart":"450","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":"Spacecraft designs using solar sails for propulsion or thin membranes to shade instruments from the sun to achieve cryogenic operating temperatures are being considered for a number of missions in the next decades. A common feature of these designs are thin dielectric materials that will be exposed to the solar wind, solar energetic particle events, and the distant magnetotail plasma environments encountered by spacecraft in orbit about the Earth-Sun L2 point. This paper will discuss the relevant radiation and internal charging environments developed to support spacecraft design for both total dose radiation effects as well as dose rate dependent phenomenon, such as internal charging in the solar wind and distant magnetotail environments. We will describe the development of radiation and internal charging environment models based on nearly a complete solar cycle of Ulysses solar wind plasma measurements over a complete range of heliocentric latitudes and the early years of the Geotail mission where distant magnetotail plasma environments were sampled beyond X(sub GSE) = - 100 Re to nearly L2 (X(sub GSE) approximately equal to - 236 Re). Application of the environment models in example charging analyses demonstrate minimal but potential risks due to charging in interplanetary environments.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0049206050","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":"NASA, Marshall Space Flight Center"},{"subitem_text_value":"Jacobs Sverdrup Technology, Inc."},{"subitem_text_value":"Jacobs Sverdrup Technology, Inc."},{"subitem_text_value":"Jacobs Sverdrup Technology, Inc."},{"subitem_text_value":"Jacobs Sverdrup Technology, Inc."}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"NASA, Marshall Space Flight Center"},{"subitem_text_language":"en","subitem_text_value":"Jacobs Sverdrup Technology, Inc."},{"subitem_text_language":"en","subitem_text_value":"Jacobs Sverdrup Technology, Inc."},{"subitem_text_language":"en","subitem_text_value":"Jacobs Sverdrup Technology, Inc."},{"subitem_text_language":"en","subitem_text_value":"Jacobs Sverdrup Technology, Inc."}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"Minow, Joseph I.","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Parker, Linda Neergaard","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Altstatt, Richard L.","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Blackwell, William C.  Jr.","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Diekmann, Anne","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":"49206050.pdf","filesize":[{"value":"3.8 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"49206050.pdf","url":"https://jaxa.repo.nii.ac.jp/record/6365/files/49206050.pdf"},"version_id":"1ef12ead-0b17-428b-a639-508dd3f96544"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"惑星間空間","subitem_subject_scheme":"Other"},{"subitem_subject":"宇宙機設計","subitem_subject_scheme":"Other"},{"subitem_subject":"ソーラーセイル","subitem_subject_scheme":"Other"},{"subitem_subject":"誘電体","subitem_subject_scheme":"Other"},{"subitem_subject":"薄板","subitem_subject_scheme":"Other"},{"subitem_subject":"宇宙機推進","subitem_subject_scheme":"Other"},{"subitem_subject":"太陽風","subitem_subject_scheme":"Other"},{"subitem_subject":"地球磁気圏尾部","subitem_subject_scheme":"Other"},{"subitem_subject":"冷却","subitem_subject_scheme":"Other"},{"subitem_subject":"極低温","subitem_subject_scheme":"Other"},{"subitem_subject":"interplanetary space","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"spacecraft design","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"solar sail","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"dielectric","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"thin plate","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"spacecraft propulsion","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"solar wind","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"geomagnetic tail","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"cooling","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"cryogenic temperature","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":"Radiation and internal charging environments for thin dielectrics in interplanetary space","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Radiation and internal charging environments for thin dielectrics in interplanetary space","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":"6365","relation_version_is_last":true,"title":["Radiation and internal charging environments for thin dielectrics in interplanetary space"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:57:05.013950+00:00"}