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Published April 2013 | Accepted Version
Book Section - Chapter Open

Deployable Helical Antennas for CubeSats

Abstract

This paper explores the behavior of a self-deploying helical pantograph antenna for CubeSats. The helical pantograph concept is described along with concepts for attachment to the satellite bus. Finite element folding simulations of a pantograph consisting of eight helices are presented and compared to compaction force experiments done on a prototype antenna. Reflection coefficient test are also presented, demonstrating the operating frequency range of the prototype antenna. The helical pantograph is shown to be a promising alternative to current small satellite antenna solutions.

Additional Information

© 2013 American Institute of Aeronautics and Astronautics. Support from the Air Force Research Laboratory Summer Space Scholars Program and AFOSR (award no. FA9550-13-1-0061, program manager Dr David Stargel) is gratefully acknowledged.

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August 19, 2023
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