Design of X-and Ka-Band Reflectarray Antennas for Intercelestial Communication Using CubeSat Relay

Nishanth Virushabadoss, Nikita Mahjabeen, Harshpreet Singh Phull Bakshi, R. Henderson
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引用次数: 3

Abstract

This paper presents the design of reflectarray antennas operating at X- and Ka- bands with gains of 27 dBi and 34 dBi, respectively, which will be used for 3U CubeSat relay communication. The Lunar Reconnaissance Orbiter (LRO) collects around 573 GB of data per day and the data is sent to the ground station (WS1) located in White Sands, New Mexico [1]. The LRO communicates with the earth station an average of 4 times per day throughout the year [2]. The LRO has several instruments in the lunar orbit, ranging from passive imagers to an active altimeter, as well as a synthetic aperture radar [2]. There is a growing need to transfer more data to the earth station for future missions. In order to accomplish this goal, we propose to use a CubeSat relay between earth and the moon orbiter. This CubeSat will communicate with the deep space network (DSN) instead of communicating with WS1 and this will help in improving the connection time between the moon orbiter and ground station. The data rate of the proposed method would be 4.5 Mbps with binary phase shift keying (BPSK) modulation.
基于立方体卫星中继的星际通信x波段和ka波段反射天线设计
设计了一种增益分别为27dbi和34dbi的X波段和Ka波段反射天线,用于3U立方体卫星中继通信。月球勘测轨道飞行器(LRO)每天收集大约573 GB的数据,这些数据被发送到位于新墨西哥州白沙的地面站(WS1)。LRO全年平均每天与地面站通信4次。LRO在月球轨道上有几个仪器,从被动成像仪到主动高度计,以及合成孔径雷达[2]。为了今后的任务,越来越需要向地面站传送更多的数据。为了实现这一目标,我们建议在地球和月球轨道器之间使用立方体卫星中继器。这颗立方体卫星将与深空网络(DSN)通信,而不是与WS1通信,这将有助于改善月球轨道器和地面站之间的连接时间。该方法采用二进制相移键控(BPSK)调制,数据速率为4.5 Mbps。
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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