首页 | 本学科首页   官方微博 | 高级检索  
     检索      

LEO太阳电池一次放电模型研究
引用本文:全荣辉,池卫英,贾巍,方美华,黄三玻.LEO太阳电池一次放电模型研究[J].航天器环境工程,2017,34(2):156-161.
作者姓名:全荣辉  池卫英  贾巍  方美华  黄三玻
作者单位:南京航空航天大学, 南京 210016;上海空间电源研究所, 上海 200040;上海空间电源研究所, 上海 200040;南京航空航天大学, 南京 210016;上海空间电源研究所, 上海 200040
基金项目:南京航空航天大学青年科技创新基金(编号:NS2014089)
摘    要:空间等离子体作用下,太阳电池一次放电是诱发二次放电的主要原因。目前缺乏适合工程应用的一次放电快速评估模型。文章借鉴辉光放电理论,针对太阳电池三联点结构提出一次放电一维简化模型,用于评估太阳电池设计对放电脉冲强弱的影响。模型计算结果表明,增加玻璃盖片厚度和电池串联间隙有助于提高一次放电起始电压,一次放电频率随着太阳电池偏压和表面二次电子发射系数增加而增大,放电电流随着太阳电池偏压和电池阵电容增加而增强。该模型计算结果与试验测试结果基本一致,且比其他模型计算过程简单,可以为太阳电池设计中一次放电现象快速评估提供参考。

关 键 词:一次放电  太阳电池  表面充电  气体放电  仿真分析
收稿时间:2016/11/23 0:00:00
修稿时间:2017/4/1 0:00:00

1D modelling of primary arcs on LEO solar array
QUAN Ronghui,CHI Weiying,JIA Wei,FANG Meihua and HUANG Sanbo.1D modelling of primary arcs on LEO solar array[J].Spacecraft Environment Engineering,2017,34(2):156-161.
Authors:QUAN Ronghui  CHI Weiying  JIA Wei  FANG Meihua and HUANG Sanbo
Institution:Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;Shanghai Institute of Space Power Sources, Shanghai 200040, China;Shanghai Institute of Space Power Sources, Shanghai 200040, China;Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;Shanghai Institute of Space Power Sources, Shanghai 200040, China
Abstract:The primary arcs on the solar arrays are the main cause of secondary arcs, a serious threat to the safety of spacecraft operation. The primary arcs were widely studied but without a fast assessment model. A 1D model of the primary arcs is developed to explain the experimental results under different discharging conditions. Both effects of the electric field enhanced emission and the electron impact ionization are included by using an equivalent capacity model for the boundary condition. The primary arc characteristics under different conditions can be predicted. The effects of the differential surface potential, the cover glass thickness, and the secondary emission coefficient are studied. It is shown that the onset voltage of the primary arc grows with the increase of cover glass thickness and the solar cell gap distance, the discharging frequency is affected by the bias voltage and the secondary emission coefficient, and the peak current is proportional to the bias voltage and the solar array capacitance. The results are consistent with experiments and can provide a fast assessment of the primary arc in a solar array design.
Keywords:primary arc  solar array  surface charging  gas discharging  simulation analysis
本文献已被 CNKI 等数据库收录!
点击此处可从《航天器环境工程》浏览原始摘要信息
点击此处可从《航天器环境工程》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号