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 6620-01-262-9489
NSN 5895-01-100-0281
NSN 5990-01-118-0151
NSN 6105-00-248-5772
NSN 5895-01-437-6572
NSN 6150-00-238-1352
NSN 6645-01-529-8822
NSN 5925-00-913-9784
NSN 5996-00-931-7378
NSN 6135-01-397-2170
NSN 5985-00-375-1837
NSN 6130-01-435-5105