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 5935-01-420-2808
NSN 5915-00-979-8225
NSN 5895-01-485-3708
NSN 5985-01-196-1191
NSN 6610-00-659-8760
NSN 6145-01-548-5812
NSN 5935-01-200-7948
NSN 5920-01-534-8673
NSN 5998-01-433-4233
NSN 5965-00-033-5928
NSN 5999-00-489-5101
NSN 6220-00-932-4992