Deployment Dynamics of Thin-Shell Space Structures

نویسندگان

چکیده

This study was motivated by the desire to develop accurate simulation models for deployment dynamics of future, ultralight deployable structures consisting multiple thin shells packaged elastically, through a combination folding and coiling. The specific problem studied is packaging unconstrained rectangular space frame formed two thin-shell longerons connected transverse rods, called strip. included experiments on high-quality test articles, using suspension system with low inertia friction. elastic folds in strips were tracked high-speed three-dimensional digital image correlation both air near-vacuum. also developed high-fidelity finite element model that captures elastic, localized deformation occurs during initial folding, self-contact between different parts structure as develops, strain energy stored process. accurately captured self-latching strips, well effects deployment.

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ژورنال

عنوان ژورنال: Journal of Spacecraft and Rockets

سال: 2022

ISSN: ['1533-6794', '0022-4650']

DOI: https://doi.org/10.2514/1.a35172