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 6130-01-123-9041
NSN 5996-00-933-9615
NSN 6135-00-269-5843
NSN 5950-01-384-3834
NSN 6105-00-126-2620
NSN 5996-00-728-3654
NSN 5855-00-055-1694
NSN 6650-01-134-6186
NSN 5935-00-149-0618
NSN 6645-01-334-7326
NSN 6650-01-378-6075
NSN 4140-01-356-5614