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 6240-01-502-6405
NSN 6620-01-068-0046
NSN 6130-01-532-9326
NSN 6685-01-252-3569
NSN 6610-00-986-2095
NSN 6650-00-211-6302
NSN 5935-01-200-8652
NSN 2925-00-078-0525
NSN 6685-01-618-0113
NSN 6620-00-233-6839
NSN 5835-01-439-0180
NSN 5920-01-010-3293