22.300-23.540 in. Radius up to the thermal coating
An item designed to sustain flame and assist combustion stability in the conbustion section of a turbine engine afterburner by creating turbulence which provides even fuel and air mixture to assure continuous burnig.
Classification: Parts of gas turbine aircraft engines, other than for use in civil aircraft
NSN 5999-01-366-8001
NSN 5945-01-315-7126
NSN 5930-01-653-5935
NSN 5998-00-388-0259
NSN 2925-01-014-0118
NSN 6145-01-529-9831
NSN 2925-00-203-8735
NSN 5975-00-783-3674
NSN 5920-01-314-6341
NSN 5999-00-725-0016
NSN 2925-00-471-1128
NSN 6130-00-354-0251