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Published in 2025 at "Multibody System Dynamics"
DOI: 10.1007/s11044-025-10080-2
Abstract: The paper describes the methodology developed to simulate the stowing and deployment phases of a flexible reflector to be deployed from a microsatellite (CubeSat). The reflector structure is modeled as a nonlinear shell with viscoelastic…
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Keywords:
simulation folding;
shell;
reflector;
methodology ... See more keywords