Abstract:Membrane reflectors are attractive for use as space based optics and antennas. Membranes offer small stowed volume, yet when deployed have a large surface area. Once deployed in orbit the membrane will be exposed to the solar thermal cycle. The purpose of this study is to determine the frequency response of a constant tension membrane due to temperature changes. Understanding how the frequency response of the membrane changes with temperature is critical to both spacecraft control and the performance of the re… Show more
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