| 引用本文: | 郝建红,黄赛,赵强,等.太阳风作用下航天器表面充电效应分析.[J].国防科技大学学报,2022,44(3):131-138.[点击复制] |
| HAO Jianhong,HUANG Sai,ZHAO Qiang,et al.Analysis of charging effect on spacecraft surface under solar wind[J].Journal of National University of Defense Technology,2022,44(3):131-138[点击复制] |
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| 太阳风作用下航天器表面充电效应分析 |
| 郝建红1,黄赛1,赵强2,范杰清1,张芳2,董志伟2 |
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(1. 华北电力大学 电气与电子工程学院, 北京 102206;2. 北京应用物理与计算数学研究所, 北京 100094)
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| 摘要: |
| 针对太阳风等离子体中航天器的充电过程,基于欧洲航天局开发的航天器表面充电仿真软件,建立了航天器的数值计算模型,模拟了太阳风等离子体与航天器的相互作用,实现了不同表面材料时航天器表面电位以及尾迹结构的计算分析,给出了近日环境下航天器周围的空间电位结构以及等离子体密度分布情况。研究结果表明:表面材料的选择将影响空间势垒深度以及尾迹结构,表面充电至更低电位的表面材料具有较小尾迹区域；航天器向阳面电位分布主要由光电子以及二次电子主导,而背阳面的电位分布则主要受到尾迹效应的影响。以上结果对太阳风环境航天器探测和评估等相关工作以及工程研究具有一定的理论参考价值。 |
| 关键词: 航天器表面充电 太阳风 等离子体 尾迹效应 势垒 |
| DOI：10.11887/j.cn.202203016 |
| 投稿日期：2021-05-20 |
| 基金项目:国家自然科学基金资助项目(U1730247,11571047,61372050) |
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| Analysis of charging effect on spacecraft surface under solar wind |
| HAO Jianhong1, HUANG Sai1, ZHAO Qiang2, FAN Jieqing1, ZHANG Fang2, DONG Zhiwei2 |
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(1. School of Electrical and Electronic Engineering, North China Electric Power University, Beijing 102206, China;2. Institute of Applied Physics and Computational Mathematics, Beijing 100094, China)
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| Abstract: |
| Aiming at the charging process of the spacecraft in the solar wind plasma, based on the spacecraft surface charging simulation software developed by the European Space Agency, a numerical calculation model of the spacecraft was established. The interaction between the solar wind plasma and the spacecraft was simulated, and different surface materials were simulated. The calculation and analysis of the surface potential of the spacecraft and the structure of the wake were realized, and the spatial potential structure and plasma density distribution around the spacecraft in the near-day environment were given. The research results show that the choice of surface material will affect the depth of the space barrier and the structure of the wake, and the surface material whose surface is charged to a lower potential has a smaller wake area; the potential distribution of the spacecraft towards the sun is mainly dominated by photoelectrons and secondary electrons, while the back of the potential distribution of the positive side is mainly affected by the wake effect. The above results have certain theoretical reference value for related work such as detection and evaluation of solar wind environment spacecraft and engineering research. |
| Keywords: spacecraft surface charging solar wind plasma wake effects potential barrier |
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