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Evaluation of a high temperature adhesive for fabricating graphite/PMR-15 polyimide structuresTests are conducted to measure shear strength, shear modulus and flatwise tensile strength of the A7F (amide-imide modified LARC-13) adhesive system. An investigation is also conducted to determine the effect of geometric material parameters, and elevated temperature on the static strength of standard joints. Single-lap and double-lap composite joints, and single, double and step lap composite to metal joints are characterized. A series of advanced joints consisting of preformed adherends, adherends with scalloped edges and joints with hybrid interface plies are tested and compared to baseline single and double-lap designs.
Document ID
19860001801
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hill, S. G.
(Boeing Aerospace Co. Seattle, WA, United States)
Cushman, J. B.
(Boeing Aerospace Co. Seattle, WA, United States)
Date Acquired
August 12, 2013
Publication Date
September 1, 1985
Publication Information
Publication: NASA. Lewis Research Center High Temp. Polymer Matrix Composites
Subject Category
Nonmetallic Materials
Accession Number
86N11268
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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