Matlinconel foil per ams 5540, 0.0025 in. Min 0.0035 in. Max thk w/thermal insulation, 7.700 in. Min 7.750 in. Max o/l lg, 4.700 in. Min 0.750 in. Max o/a w
A flexible covering, fabricated from appropriate insulating materials, designed to reduce thermal radiation in the hot section of an engine, gas turbine, aircraft. see also shield, heat, aircraft gas turbine engine.
Classification: Parts of gas turbine aircraft engines, other than for use in civil aircraft
NSN 5910-01-520-3323
NSN 5920-01-181-5248
NSN 5835-01-459-8664
NSN 6685-01-411-5969
NSN 5965-01-256-9460
NSN 6610-01-346-1426
NSN 5960-01-017-0989
NSN 7035-01-629-0082
NSN 5996-01-476-7550
NSN 5950-01-336-0939
NSN 6105-01-593-8283
NSN 5915-00-375-5000