Material is steel, corrosion resisting & sheet fiber, ceramic; layer thickness 0.004 in.
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 5905-01-182-3459
NSN 5910-00-613-6756
NSN 5910-01-519-5791
NSN 6650-01-279-0658
NSN 6130-01-088-9290
NSN 6105-00-463-9108
NSN 5999-01-499-6278
NSN 5996-01-649-3986
NSN 6110-01-484-1904
NSN 5835-01-300-6869
NSN 5925-01-401-5314
NSN 5930-01-207-1012