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 5965-00-144-2543
NSN 5990-01-645-2592
NSN 5920-01-343-6838
NSN 5920-01-147-5652
NSN 5996-00-417-9706
NSN 6130-01-146-4221
NSN 5905-01-527-4633
NSN 2925-00-139-8309
NSN 5999-00-306-3289
NSN 6610-01-160-8815
NSN 2925-01-602-1975
NSN 5915-01-338-4792