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NASA NTRS · 19820003620

Study of foldable elastic tubes for large space structure applications, phase 3

Abstract

A bi-convex foldable elastic tube, suitable for use in self deploying space structures, was subjected to a series of buckling tests to deterine initial buckling loads, collapse loads, and the buckling mode. The tube is cylindrical with a cross-section that is lenticular-like with flared edges. It is capable of being flattened in the center and folded compactly, storing up strain energy in the process. Upon removal of constraint, it springs back to its original straight configuration, releasing the stored strain energy. The tests showed that this type of tube has good resistance to buckling, with the initial buckling loads all falling within or above the range of those for comparable circular cylindrical tubes.

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BibTeXRIS

Jones, I. W., Mitchell, S. O.. 1981-09-01. Study of foldable elastic tubes for large space structure applications, phase 3. https://ntrs.nasa.gov/citations/19820003620

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