NASA NTRS · 19780000427
Low-cost graphite/epoxy structural panels
Abstract
Manufacturing process precures components of composite panels prior to assembly. Process separately cures the graphite/epoxy skin, stiffener ribs, and stiffener grid. After curing, panels are assembled using special adhesive. With implementation of cost effective manufacturing techniques, uses of graphite-epoxy laminate panels may be found in other areas such as auto industry.
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Lager, J. R., Padilla, D., Thiemet, W. F., Thomas, D. A.. 1979-01-01. Low-cost graphite/epoxy structural panels. https://ntrs.nasa.gov/citations/19780000427
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