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Dependence of lunar surface charging on solar wind plasma conditions and solar irradiation

机译:月球表面电荷对太阳风等离子体条件和太阳辐射的依赖性

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摘要

The surface of the Moon is electrically charged by exposure to solar radiation on its dayside, as well as by the continuous flux of charged particles from the various plasma environments that surround it. An electric potential develops between the lunar surface and ambient plasma, which manifests itself in a near-surface plasma sheath with a scale height of order the Debye length. This study investigates surface charging on the lunar dayside and near-terminator regions in the solar wind, for which the dominant current sources are usually from the photoemission of electrons J_p, and the collection of plasma electrons J_e, and ions J_i. These currents are dependent on the following six parameters: plasma concentration n_O, electron temperature T_e, ion temperature T_i, bulk flow velocity V, photoemission current at normal incidence J_(PO), and photoelectron temperature T_p. Using a numerical model, derived from a set of eleven basic assumptions, the influence of these six parameters on surface charging - characterized by the equilibrium surface potential, Debye length, and surface electric field - is investigated as a function of solar zenith angle. Overall, T_e is the most important parameter, especially near the terminator, while J_(PO) and T_p dominate over most of the dayside. In contrast, V and T_i are found to be the least effective parameters. Typically, lunar surface charging in the solar wind can be reduced to a two-current problem: on the dayside in sunlight, J_p+J_e = 0, since |J_p|>|J_e|>|J_j|, while near the terminator in shadow, J_e+J_i = 0. However, situations can arise that result in a truly three-current problem with some important consequences; e.g., very cold T_e and/or very fast V can result in |J_p|>|J_e|>|J_j| on the dayside. The influence of surface charging pervades the environments of the Moon and other airless bodies, and the investigation presented here provides insights into the physical processes involved, as well as being useful for interpreting and understanding more complicated simulations.
机译:月球表面在白天暴露于太阳辐射下,并且围绕它周围的各种等离子体环境不断产生带电粒子,从而使月球表面带电。在月球表面和周围等离子之间会产生电势,这会在近表面等离子鞘层中显现出来,其尺度高度约为Debye长度。这项研究调查了太阳风中月球日面和近终结者区域的表面电荷,其主要电流源通常来自电子J_p的光发射以及等离子体电子J_e和离子J_i的收集。这些电流取决于以下六个参数:等离子体浓度n_O,电子温度T_e,离子温度T_i,体流速V,法向入射光发射电流J_(PO)和光电子温度T_p。使用从一组11个基本假设中得出的数值模型,研究了这六个参数对表面电荷的影响-以平衡表面电势,德拜长度和表面电场为特征-是太阳天顶角的函数。总体而言,T_e是最重要的参数,尤其是在终止符附近,而J_(PO)和T_p在白天的大部分时间中均占主导地位。相反,发现V和T_i是最无效的参数。通常,可以将太阳风中的月球表面电荷减少到两流问题:在日光下的白天,J_p + J_e = 0,因为| J_p |> | J_e |> | J_j |处于阴影中的终止子附近,J_e + J_i =0。但是,可能会出现导致真正的三潮流问题并带来一些重要后果的情况。例如,非常冷的T_e和/或非常快的V会导致| J_p |> | J_e |> | J_j |在白天。表面电荷的影响遍及月球和其他无空气物体的环境,此处介绍的研究提供了对所涉及物理过程的见识,并且对于解释和理解更复杂的模拟很有用。

著录项

  • 来源
    《Planetary and space science》 |2014年第1期|10-27|共18页
  • 作者单位

    NASA Goddard Space Flight Center, Greenbelt, MD 20771, USA,Formerly at Center for Research and Exploration in Space Science and Technology, University of Maryland, Baltimore County, Baltimore,MD 21250, USA;

    NASA Goddard Space Flight Center, Greenbelt, MD 20771, USA;

    Space Sciences Laboratory, University of California, Berkeley, CA 94720, USA;

    Department of Physics and Astronomy, University of Calgary, Calgary, AB T2N 1NA, Canada;

    NASA Goddard Space Flight Center, Greenbelt, MD 20771, USA;

    NASA Goddard Space Flight Center, Greenbelt, MD 20771, USA;

    NASA Goddard Space Flight Center, Greenbelt, MD 20771, USA;

    Space Sciences Laboratory, University of California, Berkeley, CA 94720, USA;

    NASA Goddard Space Flight Center, Greenbelt, MD 20771, USA;

  • 收录信息
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Moon; Surface charging; Solar wind; Plasma; Photoemission; Numerical model;

    机译:月亮;表面充电;太阳风;等离子体;光发射;数值模型;

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