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 6130-00-153-3136
NSN 5950-01-193-5994
NSN 5930-00-993-0440
NSN 5975-00-679-6738
NSN 5990-00-444-9993
NSN 6645-00-292-5053
NSN 6220-00-231-2687
NSN 5945-00-243-6786
NSN 6110-00-571-1749
NSN 7035-01-506-8018
NSN 6620-00-707-4195
NSN 2925-01-004-5627