A combination of hrms and spring loaded hinges for deployable panels is a simple and reliable so lution. The deployment will be accomplished by a newly developed mechanism consisting of two hinges and two binders per panel. In abaqus the initial strain was simulated by assigning different thermal expansion coefficients to the two materials in the bilayer and applying a temperature difference to the hinge region to realize the initial strain differential 2 2 1 1 e e t σ σ.
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