NASA NTRS · 19880000351
Rebound Of Previously Compressed O-Ring
Abstract
Report presents theoretical and experimental analysis of relaxation characteristics of O-ring of vinylidene fluoride/hexafluoropropylene copolymer of same composition used in solid rocket boosters on Space Shuttle flight 51-L. Study covers range of temperatures from 10 to 120 degree F. Presents one-dimensional mathematical model of response provided for both elastic response and creep.
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Moore, Carleton J.. 1988-06-01. Rebound Of Previously Compressed O-Ring. https://ntrs.nasa.gov/citations/19880000351
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