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 5975-01-164-1135
NSN 5915-01-129-3268
NSN 5985-01-338-4790
NSN 2925-01-364-7926
NSN 6650-00-684-3060
NSN 6150-01-088-2398
NSN 5990-00-524-2293
NSN 6130-00-186-0737
NSN 6240-01-148-4627
NSN 5985-01-502-9303
NSN 5996-00-598-4839
NSN 6145-01-634-0388