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 5990-00-350-2352
NSN 4140-00-027-5150
NSN 6650-01-497-5782
NSN 5930-01-105-3930
NSN 6645-01-426-0206
NSN 5990-00-292-5017
NSN 6130-01-268-1703
NSN 5895-01-431-9790
NSN 5950-00-495-5214
NSN 5990-01-485-0260
NSN 7035-00-922-5700
NSN 5996-01-341-4313