NASA NTRS · 19880000377
Graphite/Epoxy Deicing Heater
Abstract
Heat applied close to surface protected. One ply of highly electrically- and thermally-conductive brominated-graphite fiber composite laminated between two plies of electrically-insulating composite material, with michel foil making contact with end portions of graphite fibers. Part of foil exposed beyond composite to serve as electrical contact. Graphite/Epoxy composite heater developed to prevent and reverse formation of ice on advanced composite surfaces of aircraft.
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Hung, Ching-Cheh, Dillehay, Michael E., Stahl, Mark. 1988-07-01. Graphite/Epoxy Deicing Heater. https://ntrs.nasa.gov/citations/19880000377
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