Procurement specification 204-20-11 fscm 80378, thickness is 0.500 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 5945-01-055-6540
NSN 6620-00-388-0047
NSN 6610-00-823-9159
NSN 5925-01-609-9497
NSN 5915-01-380-7623
NSN 6110-01-021-6712
NSN 5905-01-468-6390
NSN 5855-00-987-1171
NSN 5950-00-981-3295
NSN 5960-01-641-5493
NSN 6645-00-664-4665
NSN 5975-00-438-5602