Abstract

An X-band reflectarray antenna using 16 × 12 double square ring elements for satellite communications is proposed in this paper. The feed is a 4 × 3 elements microstrip patch array designed to create edge taper of approximately − 10 dB. A prototype with right-hand circular polarization (RHCP) is manufactured and tested, and the good agreements between simulations and measurements are demonstrated. The good performance is obtained with the aperture efficiency of 40.7% and the 3-dB gain bandwidth of about 10% which is beneficial to nanosatellites.

Highlights

  • In the last decade, nanosatellites for low-Earth orbit missions are becoming more and more popular due to their relatively low cost, relatively fast development, and satellite network application capabilities

  • This paper presents the recent work on a reflectarray antenna using 16 × 12 double square ring elements for a nanosatellite bus

  • The broadband microstrip patch array feed is designed to mitigate feed deployment complexity and the whole antenna is designed to fit into commercially available nanosatellite buses

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Summary

Reflectarray Antenna for Satellite

Bing Ma1,2, Fan Lu1,2*, Guoping Zhi[1,2], Xin Xue[1,2], Xiangni Zhao[1,2], Chao Ma1,2, Yong Fan1,2 & Mei Yang[1]. In order to analyze how the reflection phase-shift varies with the size of the double square r­ ings[16], we suppose that the element is located in an infinite array Though this is an approximation, it has a tiny effect on the simulation result. The measured antenna gain gives an aperture efficiency of 40.7% which is mainly caused by using the microstrip patch array feed with a low efficiency, and the 3-dB gain bandwidth is about 10% which is mainly caused by using foam layer and double square metal rings. It can be widely used in nanosatellite bus for high-speed data transmission and satellite communication

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