Abstract
在基于磁流体动力学和电磁波传播理论的基础上，针对航天飞行器再入过程中的黑障问题，提出了一种物理模型.利用数值分析方法，研究电磁窗周围的电子密度在不同的飞行器轴向距离下，随着飞行器法向距离增加呈现出的变化趋势；改变外加电场和磁场的交叉角度，分析不同角度下电磁窗周围电子密度的变化趋势；研究有外加正交电磁场的电子密度与无外加电磁场电子密度比值的变化趋势和电磁波衰减的变化趋势.结果表明：当外加正交电磁场时，接收天线周围的电子密度随飞行器法向距离的增加而不断减小，其与无外加电磁场时电子密度之比呈现不断下降的趋势；电磁波的衰减在不同飞行高度和外加磁场强度下，随着电磁波频率的增加而不断减小.这为减缓“黑障”问题提供了一种新的方法.
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