Inclosure not included; power output for which designed is a shaft; shaft horsepower rating 3200.0; shaft horsepower rating speed in rpm 1500.0; altitude at which horsepower is rated at sea level 0.0; inlet air temp at which power is rated 80 degrees fahrenheit
No other part numbers with same form, fit, and function found.
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 5920-01-092-1148
NSN 5975-01-502-9391
NSN 4140-01-446-6007
NSN 6645-01-379-2769
NSN 6645-01-363-5944
NSN 2925-00-295-8109
NSN 5835-01-055-6859
NSN 5905-00-275-0361
NSN 5895-01-251-7869
NSN 5855-00-167-7893
NSN 5905-01-360-3957
NSN 5895-00-056-1512