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Reducing Thermal Expansivity of Composite PanelsCoefficient of thermal expansion of laminated graphite/epoxy composite panels altered after panels cured by postcuring heat treatment. Postcure decreases coefficient of thermal expansion by increasing crosslinking between molecules. Treatment makes it possible to reprocess costly panels for requisite thermal expansivity instead of discarding them.
Document ID
19840000117
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Smith, D. D. (Boeing Aerospace Co.)
Date Acquired
August 12, 2013
Publication Date
January 1, 1985
Publication Information
Publication: NASA Tech Briefs
Volume: 8
Issue: 3
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
MFS-25793
Accession Number
84B10117
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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