A continuous combustion type engine. consists primarily of a compressor, aircraft gas turbine engine, chamber, combustion, aircraft gas turbine engine and a turbine assembly, aircraft gas turbine engine. it may have an afterburner, turbine engine and/or a fan section. air is compressed and heated by a combustible fuel and expanded through the turbine. it is designed to furnish a source of rotary shaft, pneumatic power or thrust power. the pneumatic power is obtained by a bleedoff of the engine compressor. for a complete operating power unit, mounted on a base, see power unit, gas turbine engine.
Classification: Gas turbine engine, except aircraft nesoi, of a power not exceeding 5,000 kw
NSN 6240-01-534-4007
NSN 5975-01-519-4292
NSN 5965-01-079-7939
NSN 6135-01-531-1413
NSN 4140-01-216-0008
NSN 4140-00-525-3197
NSN 5910-01-270-6216
NSN 4140-01-350-3277
NSN 5935-01-109-7966
NSN 5915-01-323-7154
NSN 5965-01-571-7958
NSN 6685-01-612-2825