A Deployable High-Gain Antenna Bound for Mars Developing a new folded-panel reflectarray for the first CubeSat mission to Mars

被引：157

作者：

Hodges, Richard E. ^{[1
,2
]}

Chahat, Nacer ^{[2
]}

Hoppe, Daniel J. ^{[2
]}

Vacchione, Joseph D. ^{[2
]}

机构：

[1] Spacecraft Antennas Grp, Pasadena, CA 91109 USA

[2] Jet Prop Lab, Pasadena, CA 91109 USA

来源：

IEEE ANTENNAS AND PROPAGATION MAGAZINE | 2017年 / 59卷 / 02期

关键词：

REFLECTARRAYS; ARRAY;

D O I：

10.1109/MAP.2017.2655561

中图分类号：

TM [电工技术]; TN [电子技术、通信技术];

学科分类号：

0808 ; 0809 ;

摘要：

This article describes the development of a deployable high-gain antenna (HGA) for the proposed Mars Cube One (MarCO) CubeSat mission to Mars. The antenna is a new folded-panel reflectarray (FPR) designed to fit on a 6U (10 x 20 x 34 cm(3)) CubeSat bus and support 8.425-GHz Mars-to-Earth telecommunications. The FPR provides a gain of 29.2 dBic with right-hand circular polarization (RHCP). Small stowage volume is a key advantage of the FPR design, as it only consumes similar to 4% of the usable spacecraft payload volume with a mass of less than 1 kg.

引用

页码：39 / 49

页数：11

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