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 6620-01-237-0254
NSN 6645-00-533-8037
NSN 6135-01-226-4071
NSN 5990-01-147-4811
NSN 5915-01-434-7781
NSN 6610-01-555-0842
NSN 5960-01-580-6360
NSN 5835-01-338-5176
NSN 6240-01-303-1003
NSN 5985-01-447-2723
NSN 4140-00-829-8765
NSN 6620-01-102-0008