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Deployment Mechanisms for High Packing Efficiency OneMeter Reflectarray Antenna (OMERA)While the capabilities of CubeSats have greatly increased in the past years, large, deployable high frequency apertures remain a limitation. The goal of this work was to develop a large 1 meter antenna operating at 35.75 Ghz for RADAR applications. A reflectarray design was selected, as the flat panels were compatible with the CubeSat form factor. A center-fed, Cassegrain configuration was selected for the feed, to minimize deployed height. The flat panel configuration and Cassegrain feed allowed the entire 1 meter antenna to be compatible with a 6U bus, leaving a little under 4U of volume for remaining instrument and spacecraft components. Several iterations of the design have been built and tested, with an RF test of a fully deployed assembly being completed most recently. The goal is to have the antenna flight ready before 2020.
Document ID
20210008565
Acquisition Source
Jet Propulsion Laboratory
Document Type
Preprint (Draft being sent to journal)
External Source(s)
Authors
Cwik, Tom
Agnes, Greg
Shi, Megjan
Dunphy, Sean
Thiel, Ellen
Chahat, Nacer
Arya, Manan
Sauder, Jonathan F.
Date Acquired
January 7, 2019
Publication Date
January 7, 2019
Publication Information
Publisher: Pasadena, CA: Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2019
Distribution Limits
Public
Copyright
Other
Technical Review

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