| 一种降低弹翼RCS的技术方案研究 |
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| 引用本文： | 戴全辉,朱绪宝.一种降低弹翼RCS的技术方案研究[J].系统工程与电子技术,2000,22(7):40-41. |
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| 作者姓名： | 戴全辉 朱绪宝 |
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| 作者单位： | 航天机电集团公司三院三部,北京,100074 |
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| 基金项目： | 国防预研基金资助课题!(970 30 0 0 6) |
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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。
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| 关 键 词： | 阻抗匹配 弹翼 雷达截面 电磁波散射 |
| 修稿时间： | 1999-06-04 |
Research of a Technology in Radar Cross Section Reduction of Missile Wing |
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| Dai Quanhui,Zhu Xubao.Research of a Technology in Radar Cross Section Reduction of Missile Wing[J].System Engineering and Electronics,2000,22(7):40-41. |
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| Authors: | Dai Quanhui Zhu Xubao |
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| Abstract: | 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. |
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| Keywords: | Impedance matching Guided missile wing Radar cross section Electromagnetic scattering |
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