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Deployable mesh reflector antennas are widely used on spacecraft. We present a general, rapid design method for a particular type of reflector architecture and derive scaling laws for mass and folded size across a wide range of reflector apertures.
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This page is a summary of: Scaling Laws for Deployable Mesh Reflector Antennas, AIAA Journal, October 2024, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j063940.
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