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Fabrication of structural elementsThe laminate fabrication procedures and quality assurance ultrasonic C-scan results used for structural elements are described. These procedures are the result of processing eleven lots of graphite/PMR-15 prepreg tape materials and two lots of graphite/NR-150B2. Early processing difficulties with NR-150B2 composites were corrected, permitting the fabrication of quality specimens from either of the two currently prescribed matrix materials. The quality of all deliverable specimens is measured by the control of fiber content, glass transition temperature, and void content, as well as laminate ultrasonic C-scan data.
Document ID
19790022133
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Darms, F. J., Jr.
(Rockwell International Corp. Downey, CA, United States)
Date Acquired
August 9, 2013
Publication Date
August 1, 1979
Publication Information
Publication: NASA. Langley Res. Center Graphite(Polyimide Composites
Subject Category
Composite Materials
Accession Number
79N30304
Funding Number(s)
CONTRACT_GRANT: NAS1-15183
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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