Low-Profile Aperture-Coupled Patch Antenna Array for CubeSat Applications

This paper presents the design, simulation, and measurement results of a dual aperture-coupled microstripline-fed antenna array with circular polarization at the C-band for small satellites applications. The antenna array was designed at a center frequency of 5.5 GHz, and it has a two-port isolation...

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Main Authors: Patricia Bouca, Joao Nuno Matos, Sergio Reis Cunha, Nuno Borges Carvalho
Format: Article
Language:English
Published: IEEE 2020-01-01
Series:IEEE Access
Subjects:
Online Access:https://ieeexplore.ieee.org/document/8963908/
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spelling doaj-c201ac03d3f84aa2bbc3b41d16732d082021-03-30T01:16:47ZengIEEEIEEE Access2169-35362020-01-018204732047910.1109/ACCESS.2020.29680608963908Low-Profile Aperture-Coupled Patch Antenna Array for CubeSat ApplicationsPatricia Bouca0https://orcid.org/0000-0002-7800-6897Joao Nuno Matos1https://orcid.org/0000-0001-7907-1028Sergio Reis Cunha2https://orcid.org/0000-0002-9919-7071Nuno Borges Carvalho3https://orcid.org/0000-0002-7402-2099Departamento de Eletrónica, Telecomunicações e Informática, Instituto de Telecomunicações, Universidade de Aveiro, Aveiro, PortugalDepartamento de Eletrónica, Telecomunicações e Informática, Instituto de Telecomunicações, Universidade de Aveiro, Aveiro, PortugalDepartamento de Engenharia Eletrotécnica e de Computadores, Faculdade de Engenharia, Universidade do Porto, Porto, PortugalDepartamento de Eletrónica, Telecomunicações e Informática, Instituto de Telecomunicações, Universidade de Aveiro, Aveiro, PortugalThis paper presents the design, simulation, and measurement results of a dual aperture-coupled microstripline-fed antenna array with circular polarization at the C-band for small satellites applications. The antenna array was designed at a center frequency of 5.5 GHz, and it has a two-port isolation bandwidth of 25 MHz above 20 dB while the axial ratio is below 1 dB. The main objective is to produce a four-patch antenna array to be mounted on CubeSat deployable wings along with a layer of solar panels, maximizing the usable space and obtaining a better link budget for a standardized Cubesat of 10 cm × 10 cm × 10 cm. The orthogonal feedlines' isolation between Tx/Rx signals and a minimization of the multi-layer design provide a lower profile approach considering the state-of-the-art. The significant thickness reduction combined with a new perspective of having both deployable wings transmitting and receiving signals lead to a notable improvement of the overall system. This work is relevant due to the demand for high-performance antenna systems that may expand the capabilities of CubeSats, considering the importance of using an antenna array instead of a single element approach.https://ieeexplore.ieee.org/document/8963908/Antenna arraycircular polarizationCubeSatssmall satellites
collection DOAJ
language English
format Article
sources DOAJ
author Patricia Bouca
Joao Nuno Matos
Sergio Reis Cunha
Nuno Borges Carvalho
spellingShingle Patricia Bouca
Joao Nuno Matos
Sergio Reis Cunha
Nuno Borges Carvalho
Low-Profile Aperture-Coupled Patch Antenna Array for CubeSat Applications
IEEE Access
Antenna array
circular polarization
CubeSats
small satellites
author_facet Patricia Bouca
Joao Nuno Matos
Sergio Reis Cunha
Nuno Borges Carvalho
author_sort Patricia Bouca
title Low-Profile Aperture-Coupled Patch Antenna Array for CubeSat Applications
title_short Low-Profile Aperture-Coupled Patch Antenna Array for CubeSat Applications
title_full Low-Profile Aperture-Coupled Patch Antenna Array for CubeSat Applications
title_fullStr Low-Profile Aperture-Coupled Patch Antenna Array for CubeSat Applications
title_full_unstemmed Low-Profile Aperture-Coupled Patch Antenna Array for CubeSat Applications
title_sort low-profile aperture-coupled patch antenna array for cubesat applications
publisher IEEE
series IEEE Access
issn 2169-3536
publishDate 2020-01-01
description This paper presents the design, simulation, and measurement results of a dual aperture-coupled microstripline-fed antenna array with circular polarization at the C-band for small satellites applications. The antenna array was designed at a center frequency of 5.5 GHz, and it has a two-port isolation bandwidth of 25 MHz above 20 dB while the axial ratio is below 1 dB. The main objective is to produce a four-patch antenna array to be mounted on CubeSat deployable wings along with a layer of solar panels, maximizing the usable space and obtaining a better link budget for a standardized Cubesat of 10 cm × 10 cm × 10 cm. The orthogonal feedlines' isolation between Tx/Rx signals and a minimization of the multi-layer design provide a lower profile approach considering the state-of-the-art. The significant thickness reduction combined with a new perspective of having both deployable wings transmitting and receiving signals lead to a notable improvement of the overall system. This work is relevant due to the demand for high-performance antenna systems that may expand the capabilities of CubeSats, considering the importance of using an antenna array instead of a single element approach.
topic Antenna array
circular polarization
CubeSats
small satellites
url https://ieeexplore.ieee.org/document/8963908/
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