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 5975-01-393-5202
NSN 6145-00-466-4068
NSN 5945-01-381-7491
NSN 4140-00-991-0766
NSN 6620-01-425-2517
NSN 6105-01-322-8246
NSN 6610-01-399-7613
NSN 6620-00-113-9145
NSN 5910-01-102-4347
NSN 5920-01-076-5467
NSN 6220-01-577-4667
NSN 5996-01-130-2992