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一种降低弹翼RCS的技术方案研究 被引量:2

Research of a Technology in Radar Cross Section Reduction of Missile Wing
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摘要 简述了弹翼电磁散射机理 ,阐述了电磁阻抗匹配的基本原理 ,设计了弹翼前缘阻抗匹配技术方案及其电磁模型。散射特性实验结果表明 ,在 8GHz~ 18GHz内 ,弹翼RCS可降低 6dB~ 12dB ,说明了所设计的电磁阻抗匹配技术方案对降低弹翼雷达截面 (RCS)具有明显的效果。 In this paper, electromagnetic scattering mechanism of missile wing is briefly described, and the basic theory of electromagnetic impedance matching technology is expounded. The electromagnetic impedance matching technology project of missile wing lead edge and its electromagnetic model are designed. The results of electromagnetic scattering characteristic experiments are 6 to 12dB reduction in wing's RCS compared with its basis within frequency from 8 to 18GHz, and this shows that the efforts has obvious effect in radar cross section reduction of missile wing.\;
出处 《系统工程与电子技术》 EI CSCD 2000年第7期40-41,52,共3页 Systems Engineering and Electronics
基金 国防预研基金资助课题!(970 30 0 0 6)
关键词 弹翼 雷达截面 电磁波散射 飞行器 Impedance matching\ \ Guided missile wing\ \ Radar cross section\ \ Electromagnetic scattering
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二级参考文献6

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共引文献18

同被引文献13

  • 1黄爱凤,余雄庆,姚卫星.翼面隐身结构电磁散射特性的数值模拟[J].航空学报,2005,26(4):422-425. 被引量:17
  • 2聂毅,余雄庆,黄爱凤.低成本翼面隐身结构的设计和RCS测试分析[J].系统工程与电子技术,2005,27(9):1594-1596. 被引量:5
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