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 5915-01-041-3680
NSN 5960-00-321-5722
NSN 6240-01-358-5138
NSN 7035-01-267-4836
NSN 5920-00-226-0227
NSN 5855-01-203-4719
NSN 5960-01-254-3541
NSN 5965-00-285-0745
NSN 5945-01-399-0608
NSN 6685-01-459-8719
NSN 5925-00-018-3225
NSN 2925-00-997-1792