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 6650-00-346-8672
NSN 4140-01-412-3933
NSN 6150-00-404-3176
NSN 5835-01-519-3834
NSN 5935-01-290-3851
NSN 5999-01-024-8217
NSN 7035-01-548-6882
NSN 5835-00-233-6327
NSN 5920-01-506-2660
NSN 5985-01-310-1379
NSN 4140-01-378-4046
NSN 5930-01-034-8913