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 5930-00-737-2630
NSN 5975-01-499-2118
NSN 6150-01-549-3436
NSN 5990-01-355-4694
NSN 6145-01-473-9503
NSN 5930-01-417-9796
NSN 6145-00-246-9776
NSN 6105-01-392-0500
NSN 5960-01-533-2115
NSN 5999-01-608-8451
NSN 5935-01-521-8939
NSN 6220-00-628-1410