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 6240-01-420-6495
NSN 5960-01-367-0981
NSN 5998-01-578-7052
NSN 4140-00-547-8918
NSN 6620-00-456-0404
NSN 5915-00-992-4687
NSN 5905-01-434-1070
NSN 6130-00-692-2916
NSN 6240-00-646-6931
NSN 6150-01-119-7807
NSN 7035-01-007-1802
NSN 5990-01-142-0538