用于航天飞机通信的小型化超宽带FSS

A. Suganya, K. Vinayagam, N. Rajesh
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引用次数: 0

摘要

提出了一种用于Ku波段航天飞机的超宽带频率选择表面(FSS)。在基板的顶层采用圆形环路(CL),底层采用小型化的方形环路(MSL),形成了所提出的FSS。FSS晶胞尺寸为5mm × 5mm,设计在1.6 mm厚的阻燃4 (FR4)基板上。所提出的FSS覆盖了11.76GHz到20.93GHz的宽带宽范围。FSS具有良好的入射角和高达60度的偏振稳定性。设计的FSS在参考-10 dB时具有9.17GHZ的大分数带宽。我们提供了理论发现的横向电(TE)和横向磁(TM)极化在正常和斜入射角。对于直入射角和离轴入射角,给出了TE和TM偏振的理论结果。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Miniaturized UWB FSS for Space Shuttle Communication
An Ultra-wideband (UWB) Frequency selective surface (FSS) is proposed for Ku band space shuttle applications. A combination of circular loop (CL) on top layer and miniaturized square loop (MSL) on bottom layer of the substrate formed the proposed FSS. The FSS unit cell size is 5 mm x 5mm, which is designed on Fire-Retardant 4 (FR4) substrate with the thickness of 1.6 mm. The proposed FSS covers broad bandwidth range from 11.76GHz to 20.93GHz stop band frequency response. The FSS exhibits good angle of incidence and polarisation stability up to 60 degrees. The designed FSS is having a large fractional bandwidth of 9.17GHZ at -10 dB reference. We provide theoretical findings for both transverse Electric (TE) and transverse Magnetic (TM) polarisation at both normal and oblique incidence angles. For both straight-on and off-axis angles of incidence, theoretical results for TE and TM polarisation are presented.
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