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 6620-01-476-7355
NSN 5925-01-077-9949
NSN 6145-01-068-3234
NSN 2925-01-642-3255
NSN 5960-00-907-4194
NSN 5905-01-379-7028
NSN 6105-00-242-1221
NSN 5905-01-490-2295
NSN 5855-00-337-3679
NSN 5930-01-357-9662
NSN 6240-01-246-8213
NSN 5965-01-537-0023