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 5990-00-351-5479
NSN 5996-01-175-7881
NSN 6110-01-535-7162
NSN 5990-01-400-3299
NSN 5855-01-503-3452
NSN 5905-01-420-1012
NSN 5925-00-092-0578
NSN 5945-00-928-8249
NSN 5915-01-071-0297
NSN 6620-01-510-3501
NSN 5965-01-264-8761
NSN 5950-01-580-8893