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 6150-00-835-5587
NSN 6645-00-884-5845
NSN 6685-01-385-1484
NSN 5925-00-379-0920
NSN 6645-01-076-4655
NSN 5985-00-100-4902
NSN 5835-01-267-3388
NSN 6220-01-143-8943
NSN 5915-01-315-0268
NSN 5895-01-201-7700
NSN 5920-01-455-8619
NSN 6150-01-224-9020