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Thermoplastic coating of carbon fibersNow that quantities of prepreg were made on the thermoplastic coating line, they are being formed into both textile preform structures and directly into composite samples. The textile preforms include both woven and knitted structures which will be thermoformed into a finished part. In order to determine if the matrix resin is properly adhering to the fibers or if voids are being formed in the coating process, the tensile strength and modulus of these samples will be tested. The matrix uniformity of matrix distribution in these samples is also being determined using an image analyzer.
Document ID
19880017023
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Edie, D. D.
(Clemson Univ. SC, United States)
Lickfield, G. C.
(Clemson Univ. SC, United States)
Drews, M. J.
(Clemson Univ. SC, United States)
Ellison, M. S.
(Clemson Univ. SC, United States)
Allen, L. E.
(Clemson Univ. SC, United States)
Mccollum, J. R.
(Clemson Univ. SC, United States)
Thomas, H. L.
(Clemson Univ. SC, United States)
Date Acquired
September 5, 2013
Publication Date
July 23, 1988
Subject Category
Composite Materials
Report/Patent Number
NASA-CR-183067
NAS 1.26:183067
Report Number: NASA-CR-183067
Report Number: NAS 1.26:183067
Accession Number
88N26407
Funding Number(s)
CONTRACT_GRANT: NAG1-680
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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