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 6620-01-147-5615
NSN 6105-00-138-2849
NSN 6645-01-040-5233
NSN 5960-01-321-2750
NSN 5910-01-513-1608
NSN 5935-01-441-0769
NSN 6145-00-500-5679
NSN 6645-00-958-5299
NSN 5835-00-466-8544
NSN 5945-00-100-1261
NSN 6620-00-583-2687
NSN 6220-00-959-5970