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Aging problems in graphite phenolic nozzle linersAge related cracks in the graphite phenolic linear and/or ATJ insert in several nine year old Altair IIA solid rocket nozzles were investigated and determined to be limited to a single lot of nozzles. Test results and photomicrographs of fracture surfaces are presented which establish that in the discrepant nozzles the bond between the graphite fibers and the phenolic resin was tenacious, resulting in a nearly homogenous behavior. These materials are shown to have a relatively weak resin - fiber bond and behave more like a released fiber composite. Lot qualification fiber directional tensile strength and the chemical composition of the two materials were comparable, indicating that standard acceptance testing could not have differentiated between the desirable and undesirable material. Review of processing records failed to reveal any cause for the difference in the aging characteristics.
Document ID
19800008852
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Mccorkle, G. S.
(Vought Corp. Dallas, TX, United States)
Date Acquired
August 10, 2013
Publication Date
March 1, 1979
Publication Information
Publication: APL The 1979 JANNAF Propulsion Meeting, Vol. 1
Subject Category
Spacecraft Propulsion And Power
Accession Number
80N17112
Funding Number(s)
CONTRACT_GRANT: NAS1-15100
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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