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Miniaturized patch antenna for the S-band communication subsystem of the 3U University CubeSat

International Journal of Electrical and Computer Engineering (IJECE) · Vol. 16 No. 4 (2026)

DOI
10.11591/ijece.v16i4.pp1913-1926
ISSN
2722-2578, 2088-8708
Published
2026-08-01
Publisher
Institute of Advanced Engineering and Science
License
creativecommons.org/licenses/by-sa/4.0

Abstract

This paper introduces a miniaturized patch antenna for the reception module of the 3U University CubeSat in the S-band communications subsystem. In order to reduce the physical characteristics of the antenna (dimensions, mass) and achieve circular polarization (CP), as well as increasing its performances, two techniques are used: the first consists of introducing semicircle truncation on both sides of the square patch, and the second consists of modifying the ground plane with networks of symmetrical slots along the main axes (x,y). The fabricated antenna prototype has overall dimensions of 55×55×3.27 mm and a total mass of 20.59 g. The developed antenna spans the uplink band (2.025 to 2.110 GHz) for payload and telemetry operations. The designed antenna achieves a reflection coefficient below minus 10 dB across the target frequency band, along with a minus 3 dB axial ratio bandwidth that is well appropriate to space communication links. The comparisons of the prototype results to the simulation results using CST and HFSS provide close agreement of around 90%.

Collaboration network of the authors

14 authors · 25 co-authorship links · 9 across different organisations

Hover or tap a name to highlight its co-authors. Double-click to open the author's page.

  • Mohammed V University
  • École Supérieure d'Ingénieurs en Génie Électrique
  • Ecole Mohammadia d'Ingénieurs
  • Different organisations
  • Same organisation
  • Affiliation unknown
  • Thicker line = more joint articles · bigger circle = more articles
Show as table
Co-authorOrganisationJoint articles
Adnane AddaimMohammed V University3
Lahbib ZenkouarMohammed V University2
Said LakhalMohammed V University1
Omar BarkiEcole Mohammadia d'Ingénieurs1
Mohamed Amine ChararEcole Mohammadia d'Ingénieurs1
Aziz El FatimiMohammed V University1
Hassan AmmorMohammed V University1
Zakaria Er-ReguigMohammed V University1
Samiya QanouneMohammed V University1

Affiliations come from OpenAlex; journal OAI-PMH metadata carries none. Authors without an OpenAlex ID are matched by name, which can merge or split people.

This record comes from Crossref (what the publisher deposited), because the journal's own OAI-PMH endpoint could not be harvested.

Metadata source: Crossref API (cadangan, berdasarkan ISSN) https://api.crossref.org/journals/2088-8708/works, first harvested 27 Okt 2026, last seen 27 Okt 2026.
Metadata as oai_dc, converted from Crossref
<oai_dc:dc xmlns:dc="http://purl.org/dc/elements/1.1/" xmlns:oai_dc="http://www.openarchives.org/OAI/2.0/oai_dc/"><dc:title>Miniaturized patch antenna for the S-band communication subsystem of the 3U University CubeSat</dc:title><dc:creator>El Hassainate, Nabil</dc:creator><dc:creator>Berrich, Loubna</dc:creator><dc:creator>Benjelloun, Nabil</dc:creator><dc:creator>Said, Ahmed Oulad</dc:creator><dc:creator>Guennoun, Zouhair</dc:creator><dc:description>&lt;jats:p&gt;This paper introduces a miniaturized patch antenna for the reception module of the 3U University CubeSat in the S-band communications subsystem. In order to reduce the physical characteristics of the antenna (dimensions, mass) and achieve circular polarization (CP), as well as increasing its performances, two techniques are used: the first consists of introducing semicircle truncation on both sides of the square patch, and the second consists of modifying the ground plane with networks of symmetrical slots along the main axes (x,y). The fabricated antenna prototype has overall dimensions of 55×55×3.27 mm and a total mass of 20.59 g. The developed antenna spans the uplink band (2.025 to 2.110 GHz) for payload and telemetry operations. The designed antenna achieves a reflection coefficient below minus 10 dB across the target frequency band, along with a minus 3 dB axial ratio bandwidth that is well appropriate to space communication links. The comparisons of the prototype results to the simulation results using CST and HFSS provide close agreement of around 90%.&lt;/jats:p&gt;</dc:description><dc:publisher>Institute of Advanced Engineering and Science</dc:publisher><dc:date>2026-08-01</dc:date><dc:type>info:eu-repo/semantics/article</dc:type><dc:format>application/pdf</dc:format><dc:identifier>https://doi.org/10.11591/ijece.v16i4.pp1913-1926</dc:identifier><dc:identifier>10.11591/ijece.v16i4.pp1913-1926</dc:identifier><dc:source>International Journal of Electrical and Computer Engineering (IJECE); Vol 16 No 4 (2026); 1913</dc:source><dc:source>2722-2578</dc:source><dc:source>2088-8708</dc:source><dc:relation>https://ijece.iaescore.com/index.php/IJECE/article/viewFile/41277/18822</dc:relation><dc:rights>http://creativecommons.org/licenses/by-sa/4.0</dc:rights></oai_dc:dc>