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 5960-01-452-1907
NSN 5915-00-196-1417
NSN 5855-01-144-4837
NSN 5930-01-211-7779
NSN 6240-01-633-9357
NSN 6135-00-461-3590
NSN 6145-01-599-9935
NSN 6220-01-288-3058
NSN 5975-01-373-1724
NSN 6645-01-075-7722
NSN 5835-00-148-9719
NSN 6645-00-533-8037