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 5990-01-373-3104
NSN 5935-01-231-5250
NSN 5945-01-420-5891
NSN 5999-01-486-3960
NSN 5996-01-284-3572
NSN 5945-01-321-0226
NSN 6650-00-466-1697
NSN 6240-00-514-3507
NSN 4140-01-133-9011
NSN 6145-01-232-4253
NSN 6220-00-484-5937
NSN 6110-01-142-8339