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 5998-00-892-5623
NSN 6130-01-607-2997
NSN 5965-00-007-7863
NSN 4140-01-545-3482
NSN 4140-01-383-4738
NSN 2925-01-359-9818
NSN 2925-00-428-6349
NSN 2925-01-115-0306
NSN 5950-01-255-1879
NSN 6620-00-930-5680
NSN 5998-01-281-7510
NSN 2925-00-056-7112