The portion of an engine, gas turbine, aircraft in which fuel is burned. it may be an annular type in which the space between the circular inner and outer cylinders form the burning chamber or it may be the multi-arrangement can type in which separate can like burn cylinders are positioned in a circular arrangement within an inner and outer case.
Classification: Parts of gas turbine aircraft engines, other than for use in civil aircraft
NSN 6145-01-032-8078
NSN 6320-01-495-1244
NSN 6220-00-980-0052
NSN 5950-01-654-9793
NSN 5915-01-142-2018
NSN 6320-00-925-0558
NSN 6220-01-593-7209
NSN 6150-01-633-8838
NSN 5999-01-613-9897
NSN 6650-00-177-6390
NSN 5910-00-003-5842
NSN 6150-00-862-9095