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WIRE, ELECTRICAL, POLYTETRAFLUOROETHYLENE/POLYMIDE INSULATED, SMOOTH SURFACE, LIGHT WEIGHT, NICKEL COATED, EXTRA HIGH STRENGTH COPPER ALLOY, 260 °C, 600 VOLTS ROHS
- Aerospace Standard
Published July 22, 2016 by SAE International in United States
Downloadable datasets availableAnnotation ability available
SPECIFICATION DEVELOPED FOR APPLICATIONS REQUIRING HIGHER CONDUCTOR TENSILE STRENGTH WHILE MAINTAINING ELECTRICAL CONDUCTIVITY. THIS SPECIFICATION USES THE EXTRA HIGH STRENGTH CLASSIFICATION OF NICKEL PLATED COPPER ALLOY CONDUCTOR FROM AS29606.
Data Sets - Support Documents
|TABLE 1||CONSTRUCTION DETAILS FOR FINISHED WIRE|
|TABLE 2||WIRE INSULATION MATERIALS|
|TABLE 3||TAPE OVERLAP REQUIREMENTS|
|TABLE 4||FINISHED WIRE INSULATION PROPERTIES REQUIREMENTS|
|TABLE 5||TEST MANDREL AND TEST LOAD REQUIREMENTS|
|TABLE 6||FINISH WIRE PERFORMANCE CHARACTERISTICS|
AE-8D Wire and Cable Committee
SAE Subcommittee AE-8D Wire & Cable, shall be associated with those activities directed by the parent SAE Aerospace Council, the SAE Aerospace Electronics & Electrical System Division, and the SAE AE-8 Aerospace Electrical/Electronic Distribution Systems Committee, for the development and application of wires and cables and associated hardware standards and specifications.
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