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Radiation and internal charging environments for thin dielectrics in interplanetary space
https://jaxa.repo.nii.ac.jp/records/6365
https://jaxa.repo.nii.ac.jp/records/636546d7dec1-5898-431b-85e7-d9a89b25943a
名前 / ファイル | ライセンス | アクション |
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49206050.pdf (3.8 MB)
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Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
言語 | en | |||||
タイトル | Radiation and internal charging environments for thin dielectrics in interplanetary space | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 惑星間空間 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 宇宙機設計 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ソーラーセイル | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 誘電体 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 薄板 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 宇宙機推進 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 太陽風 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 地球磁気圏尾部 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 冷却 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 極低温 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | interplanetary space | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | spacecraft design | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | solar sail | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | dielectric | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | thin plate | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | spacecraft propulsion | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | solar wind | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | geomagnetic tail | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | cooling | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | cryogenic temperature | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_5794 | |||||
資源タイプ | conference paper | |||||
著者 |
Minow, Joseph I.
× Minow, Joseph I.× Parker, Linda Neergaard× Altstatt, Richard L.× Blackwell, William C. Jr.× Diekmann, Anne |
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著者所属 | ||||||
NASA, Marshall Space Flight Center | ||||||
著者所属 | ||||||
Jacobs Sverdrup Technology, Inc. | ||||||
著者所属 | ||||||
Jacobs Sverdrup Technology, Inc. | ||||||
著者所属 | ||||||
Jacobs Sverdrup Technology, Inc. | ||||||
著者所属 | ||||||
Jacobs Sverdrup Technology, Inc. | ||||||
著者所属(英) | ||||||
en | ||||||
NASA, Marshall Space Flight Center | ||||||
著者所属(英) | ||||||
en | ||||||
Jacobs Sverdrup Technology, Inc. | ||||||
著者所属(英) | ||||||
en | ||||||
Jacobs Sverdrup Technology, Inc. | ||||||
著者所属(英) | ||||||
en | ||||||
Jacobs Sverdrup Technology, Inc. | ||||||
著者所属(英) | ||||||
en | ||||||
Jacobs Sverdrup Technology, Inc. | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構 | |||||
出版者(英) | ||||||
出版者 | Japan Aerospace Exploration Agency (JAXA) | |||||
書誌情報 |
宇宙航空研究開発機構特別資料 en : JAXA Special Publication: 9th Spacecraft Charging Technology Conference 巻 JAXA-SP-05-001E, p. 450-460, 発行日 2005-08-01 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | 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. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1349-113X | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA11984031 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0049206050 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: JAXA-SP-05-001E |