NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Material characterization and specification development for 350 F curing epoxy-graphite materialsNew analytical techniques and a processability laminate have been used in the development of a material specification for 350 F curing epoxy-graphite materials. The development of the specification required the evaluation of prepregs which had variations in their processing behavior that were detected only in production. Chemical techniques were used to analyze the prepregs and establish limits on the concentrations of the various chemical constituents. A batch acceptance test laminate was designed to determine suitability of prepregs for production useage. The new specification requires that the processability laminate be ultrasonically and micrographically inspected for voids and porosity. Incorporation of these and other requirements will help to insure material consistency and processability.
Document ID
19830039225
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Rogers, A. K.
(Lockheed-California Co. Burbank, CA, United States)
Tajima, Y. A.
(Lockheed-California Co. Burbank, CA, United States)
Young, R. C.
(Lockheed-California Co. Burbank, CA, United States)
Date Acquired
August 11, 2013
Publication Date
January 1, 1982
Subject Category
Composite Materials
Meeting Information
Meeting: In: National SAMPE Symposium and Exhibition
Location: San Diego, CA
Start Date: May 4, 1982
End Date: May 6, 1982
Accession Number
83A20443
Funding Number(s)
CONTRACT_GRANT: NAS1-14000
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available