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 6320-01-236-9562
NSN 5960-01-560-8461
NSN 2925-00-771-7521
NSN 5975-01-378-7355
NSN 5905-00-781-7770
NSN 6650-00-740-7338
NSN 5960-01-181-2143
NSN 6130-01-240-8801
NSN 5945-00-250-7911
NSN 5975-00-036-9157
NSN 6145-00-170-9415
NSN 5985-01-461-3062