Multilayered Nonwoven Carbon Film Integrated with Flexible FSS for Aerospace Absorber Application

H. Baskey, V. K. Sutrakar, A. Dixit, S. Abbas, N. Prasad
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引用次数: 1

Abstract

This paper describes the electromagnetic design, simulation and fabrication of microwave absorber composite based on non woven carbon film and frequency selective surfaces. The filler ingredients i.e. the non woven carbon films were used in conjunction with the glass fabrics and epoxy for the fabrication of proposed absorber. The constituent electromagnetic properties i.e. dielectric constant and loss tangent of carbon films and glass fibers reinforced plastics have been measured and used in the electromagnetic simulation and optimization of absorber composite. Furthermore the optimized configuration have been used for composite fabrication and tested for its electromagnetic absorption. Experimental results shows minimum 10 dB reflection loss (90% electromagnetic absorption) in the entire 8.20-12.40 GHz frequency region. The fabricated composite shows potential application for radar cross section reduction in various strategic applications.
柔性FSS集成的多层非织造碳膜在航空吸收器中的应用
本文介绍了基于无纺布碳膜和频率选择表面的微波吸收复合材料的电磁设计、仿真和制造。填料成分,即无纺布碳薄膜,与玻璃织物和环氧树脂一起用于制造所建议的吸收剂。测量了碳膜和玻璃纤维增强塑料的介电常数和损耗正切等组成电磁性能,并将其应用于吸波复合材料的电磁模拟和优化。并将优化后的结构用于复合材料的制备和电磁吸收测试。实验结果表明,在整个8.20 ~ 12.40 GHz频段内,反射损耗最小为10 dB(90%电磁吸收)。所制备的复合材料在各种战略应用中显示出减少雷达横截面的潜在应用。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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