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 6150-00-757-4853
NSN 6105-01-022-2407
NSN 6650-01-510-9488
NSN 6240-01-392-0458
NSN 6610-00-769-6826
NSN 6145-01-139-6557
NSN 6105-00-974-8237
NSN 5945-00-989-5314
NSN 5930-01-434-8879
NSN 5855-00-688-9954
NSN 6110-00-766-0886
NSN 5945-01-281-1551