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 6320-01-215-1133
NSN 6135-00-990-1822
NSN 5935-01-039-3341
NSN 5950-00-863-5589
NSN 5835-01-028-0097
NSN 5855-01-323-5394
NSN 6150-00-624-6281
NSN 5950-01-280-5469
NSN 5985-01-634-0635
NSN 6145-00-394-4511
NSN 5950-00-597-3661
NSN 5950-01-152-2622