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Reproducibility of PMR-15 graphite polymide materialInvestigation was made into the reproducibility of PMR polyimide/graphite prepreg reinforcement and the influence of these variabilities on processing characteristics and final composite properties. The purpose of these investigations was to establish specification controls and limits of acceptance/rejection on incoming materials. Prepreg samples were chemically analyzed and the results compared to the processing and property results of the resulting composites. The findings from these comparisons are discussed.
Document ID
19790031523
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Hoggatt, J. T.
(Boeing Aerospace Co. Seattle, WA, United States)
Hunter, A. B.
(Boeing Aerospace Co. Seattle, WA, United States)
Sheppard, C. H.
(Boeing Aerospace Co. Seattle, Wash., United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1978
Subject Category
Composite Materials
Meeting Information
Meeting: Reinforced Plastics/Composites Institute, Annual Conference
Location: Washington, DC
Start Date: February 7, 1978
End Date: February 10, 1978
Sponsors: Reinforced Plastics/Composites Institute
Accession Number
79A15536
Funding Number(s)
CONTRACT_GRANT: NAS1-15009
Distribution Limits
Public
Copyright
Other

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