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Physical aging and its influence on the reliability of network epoxies and epoxy-matrix compositesThe matrix-dominated physical and mechanical properties of a carbon fiber reinforced epoxy composite and a neat epoxy resin were found to be affected by sub-Tg annealing in nitrogen and dark atmosphere. Postcured specimens of Thornel 300 carbon-fiber/Fiberite 934 epoxy as well as Fiberite 934 epoxy resin were quenched from above Tg and given annealing at 140 C, 110 C, or 80 C, for time up to one-hundred thousand minutes. No weight loss was observed during annealing at these temperatures. Significant variations were found in density, modulus, hardness, damping, moisture absorption ability, thermal expansivity. Moisture-epoxy interactious were also studied. The kinetics of aging as well as the molecular aggregation during this densification process were monitored by differential scanning calorimetry, dynamic mechanical analysis, density gradient column, microhardness tester, Instron, and solid-state nuclear magnetic resonance spectroscopy.
Document ID
19840023219
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Heinemann, K.
(Stanford Univ. CA, United States)
Date Acquired
September 4, 2013
Publication Date
July 31, 1983
Subject Category
Composite Materials
Report/Patent Number
NAS 1.26:173870
NASA-CR-173870
Report Number: NAS 1.26:173870
Report Number: NASA-CR-173870
Accession Number
84N31289
Funding Number(s)
CONTRACT_GRANT: NCC2-103
PROJECT: RTOP 505-33-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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