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 5960-01-300-6788
NSN 5996-01-459-5082
NSN 5905-01-499-9898
NSN 6145-01-219-6122
NSN 6110-00-865-4666
NSN 5996-01-646-1264
NSN 2925-01-443-1748
NSN 6645-01-532-7059
NSN 5835-01-123-8305
NSN 6620-00-028-3370
NSN 6645-01-354-7624
NSN 5915-01-013-8995