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 6610-00-931-1291
NSN 5915-01-502-6623
NSN 5905-01-349-6468
NSN 6685-01-584-5861
NSN 6645-00-181-1877
NSN 5895-00-189-8095
NSN 6610-00-420-8475
NSN 5985-01-297-2292
NSN 6320-00-504-1214
NSN 6645-00-947-0625
NSN 4140-01-246-4267
NSN 5960-01-632-6576