高功率微波对空间太阳电池阵的耦合效应OA
Coupling effect of high-power microwave on space solar arrays
空间太阳电池阵作为航天器的重要能源组成部分,在未来对抗中极易受到以高功率微波为代表的外来强电磁脉冲侵袭.为研究空间太阳电池阵的高功率微波耦合效应,以典型太阳电池阵结构和布局作为参考,搭建了高功率微波辐照作用下的太阳电池阵样品三维模型,研究了不同激励源参数条件(频率、极化方向、入射角度等)下的太阳电池阵耦合效应规律.结果表明:在 2~18 GHz频率范围内,垂直极化的S波段微波辐照最容易对太阳电池阵造成诱发放电损伤,电池串间隙三结合部感应场强远高于互连片位置间隙;在微波辐照作用下太阳电池样品会感应出极强的瞬态电场,垂直极化情况下,感应场主要集中分布在电池串间隙、汇流条附近、电池片边缘;电池三结合部感应电场稳定峰值随微波入射角度的增大而减小,随微波功率密度的增大而增大;微波上升下降沿对感应电场值无明显影响;太阳电池阵串间隙周围空间的电场由间隙中心向外侧逐渐减小.该研究将为空间太阳电池阵的电磁防护设计提供参考.
[Background]Space solar arrays,as a crucial part of satellite power systems,are essential for maintaining normal satellite operation.Their large surface area and complex insulation structure make them highly vulnerable to strong external electromagnetic fields.High-power microwaves(HPM),with their wide bandwidth,high power,and rapid action,can readily damage such structures.Therefore,investigating the HPM coupling effects on space solar arrays is of significant importance.[Purpose]This study aims to investigate the electric field coupling of space solar cell array samples under high-power microwave exposure.[Methods]Using a representative solar cell array structure and layout as a reference,we construct a three-dimensional model under high-power microwave irradiation and examines the coupling behavior of the array under varying excitation source parameters,including frequency,polarization direction,incidence angle and so on.[Results](1)Within the frequency range of 2-18 GHz,vertically polarized S-band microwave irradiation is most likely to induce discharge damage to the solar cell array,with the induced electric field at the triple junction in cell string gaps being much higher than that at interconnect gaps.(2)Under microwave irradiation,the solar cell samples exhibit intense transient electric fields;in the case of vertical polarization,the induced field is mainly concentrated in the cell string gaps,near the busbars,and along the cell edges.(3)The steady peak of the induced electric field at the triple junction decreases with increasing microwave incidence angle and increases with higher microwave power density.(4)The rise and fall times of the microwave pulse have no significant effect on the induced electric field magnitude.(5)The electric field in the space around the cell string gap gradually decreases from the gap center toward the outer region.[Conclusions]The findings of this study provide valuable references for the electromagnetic protection design of space solar cell arrays.
由俞宁;连汝慧;曹柯涵;吴建超;宋法伦;宋佰鹏;张冠军
西安交通大学 电气工程学院,西安 710049西安交通大学 电气工程学院,西安 710049西安交通大学 电气工程学院,西安 710049北京卫星制造厂有限公司,北京 100190中国工程物理研究院 应用电子学研究所,四川 绵阳 621900西安交通大学 电气工程学院,西安 710049西安交通大学 电气工程学院,西安 710049
信息技术与安全科学
空间太阳电池阵高功率微波耦合瞬态场影响规律电磁防护
space solar arrayshigh power microwavecoupled transient fieldinfluence lawelectromagnetic protection
《强激光与粒子束》 2026 (2)
49-57,9
国家自然科学基金项目(12375205)高功率微波技术重点实验室项目(2023-JKW-WBSYS-02)中央高校基本科研业务费专项资金项目(xzy012023153)
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