This Aerospace Recommended Practice (ARP) describes a manufacturing method for processing unidirectional graphite fiber/epoxy resin impregnated sheet and tape into multi-ply broadgoods and tape produced on an automated cross-plying machine. Broadgoods or tape of two or more ply configurations may be processed, where ply orientations of 0°, 45°, 90°, and 135° (as examples) may be automatically layed in a programmed sequence. In all configurations, the 0° ply direction is parallel to the length of the broadgoods roll or sheet, or tape.
This specification and its supplementary detail specifications cover boron filaments in the form of tape impregnated with epoxy resin, the resin to be supplied in a "B" stage condition.
This specification and its supplementary detail specifications cover boron filaments in the form of tape impregnated with epoxy resin, the resin to be supplied in a "B" stage condition.
This specification covers one type of epoxy-resin-impregnated boron filaments 0.004 in. (0.10 mm) in diameter in the form of continuous tape supported on a glass fabric carrier.
This specification covers one type of epoxy-resin-impregnated boron filaments 0.004 in. (0.100 mm) in diameter in the form of continuous tape supported on a glass cloth carrier.
This specification covers one type of epoxy-resin-impregnated boron filaments 0.004 in. (0.100 mm) in diameter in the form of continuous tape supported on a glass cloth carrier.