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 5985-00-549-1511
NSN 6135-01-528-6896
NSN 2925-00-087-2465
NSN 4140-01-119-2879
NSN 6220-01-513-0060
NSN 5985-00-392-0522
NSN 5945-00-250-0722
NSN 5835-00-140-8646
NSN 6145-00-466-4068
NSN 5905-01-477-7152
NSN 6135-01-196-7399
NSN 5985-00-779-5697