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Study of foldable elastic tubes for large space structure applications, phase 3A 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.
Document ID
19820003620
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Jones, I. W.
(Howard Univ. Washington, DC, United States)
Mitchell, S. O.
(Howard Univ. Washington, DC, United States)
Date Acquired
September 4, 2013
Publication Date
September 1, 1981
Subject Category
Structural Mechanics
Report/Patent Number
NASA-CR-164929
Report Number: NASA-CR-164929
Accession Number
82N11493
Funding Number(s)
CONTRACT_GRANT: NSG-1320
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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