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Deployable Helical Antennas for CubeSats

Olson, Gina M. and Pellegrino, Sergio and Banik, Jeremy and Constantine, Joseph (2013) Deployable Helical Antennas for CubeSats. In: 54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA , Reston, VA, Art. No. 1671. ISBN 978-1-62410-223-3. http://resolver.caltech.edu/CaltechAUTHORS:20131120-152814552

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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.


Item Type:Book Section
Related URLs:
URLURL TypeDescription
http://arc.aiaa.org/doi/abs/10.2514/6.2013-1671PublisherArticle
http://dx.doi.org/10.2514/6.2013-1671DOIArticle
ORCID:
AuthorORCID
Pellegrino, Sergio0000-0001-9373-3278
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.
Group:GALCIT
Funders:
Funding AgencyGrant Number
Air Force Research Laboratory (AFRL)UNSPECIFIED
Air Force Office of Scientific Research (AFOSR)FA9550-13-1-0061
Record Number:CaltechAUTHORS:20131120-152814552
Persistent URL:http://resolver.caltech.edu/CaltechAUTHORS:20131120-152814552
Usage Policy:No commercial reproduction, distribution, display or performance rights in this work are provided.
ID Code:42601
Collection:CaltechAUTHORS
Deposited By: Kristin Buxton
Deposited On:20 Nov 2013 23:48
Last Modified:07 Apr 2017 22:58

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