A continuous combustion type engine. consists primarily of a compressor, nonaircraft gas turbine engine; chamber, combustion, nonaircraft gas turbine engine and a turbine assembly, nonaircraft gas turbine engine. it may have 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 and/or pneumatic 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 6105-00-925-9906
NSN 5895-01-447-8993
NSN 5915-01-057-4505
NSN 5855-01-147-4785
NSN 5960-01-495-0859
NSN 6145-01-361-4613
NSN 5925-01-500-1219
NSN 5985-01-369-1008
NSN 6620-00-999-2425
NSN 5999-01-145-4096
NSN 5930-00-601-6353
NSN 6145-01-284-4030