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 6240-01-100-3696
NSN 6150-00-789-7737
NSN 6240-00-253-7611
NSN 6130-01-550-5154
NSN 5990-01-057-4191
NSN 6240-01-349-8766
NSN 5985-01-611-9355
NSN 5999-00-465-0560
NSN 6620-01-241-9592
NSN 6240-01-631-8680
NSN 6220-00-605-0404
NSN 5935-00-661-0825