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AUTOMATED MANUFACTURE OF CONTINUOUS MULTI-PLY GRAPHITE FIBER/EPOXY RESIN IMPREGNATED BROADGOODS

1980-10-01
HISTORICAL
ARP1674
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.
Standard

CORE, HONEYCOMB, GLASS/POLYIMIDE

1993-04-01
HISTORICAL
AMS3712B
This specification covers expanded honeycomb core made of glass cloth impregnated with polyimide resin and supplied in the form of blocks, slices, and ordered shapes.
Standard

FILM, COPPER CLAD POLYESTER

1992-04-01
HISTORICAL
AMS3613B
This specification covers a polyester resin in the form of a film clad on one or both sides with copper foil.
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