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 5925-01-344-4901
NSN 6105-00-248-5772
NSN 5930-00-913-9665
NSN 5960-00-116-9989
NSN 5999-01-052-3516
NSN 6610-01-399-1295
NSN 5975-01-152-2635
NSN 5950-00-208-6148
NSN 5945-01-189-7533
NSN 6150-00-222-5302
NSN 6645-01-394-1923
NSN 5835-00-106-2120