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 5999-01-299-9268
NSN 6645-01-136-4447
NSN 5950-01-186-0001
NSN 6620-00-529-6275
NSN 5835-01-412-5325
NSN 6150-00-273-9014
NSN 6610-01-467-7068
NSN 6135-01-510-4663
NSN 5855-00-013-1244
NSN 7035-00-126-1899
NSN 5945-00-561-1396
NSN 5935-00-597-5055