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Rebound Of Previously Compressed O-RingReport 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.
Document ID
19880000351
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Moore, Carleton J. (NASA Marshall Space Flight Center, Huntsville, Ala.)
Date Acquired
August 13, 2013
Publication Date
June 1, 1988
Publication Information
Publication: NASA Tech Briefs
Volume: 12
Issue: 6
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
MFS-27186
Accession Number
88B10351
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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