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Thin flat flexures are often used in deployable space structures, since they can be folded and work as hinges. We propose a design framework to decide on hinge dimensions (such as length and separation of the flexures) to avoid material failure.
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This page is a summary of: Stowage Analysis of a Flat Flexure Elastic Hinge for Deployable Space Structures, AIAA Journal, February 2025, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j064266.
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