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 5998-01-560-7502
NSN 6135-00-497-0491
NSN 5895-01-068-3279
NSN 7035-01-537-0033
NSN 6645-00-570-0092
NSN 5895-00-140-1817
NSN 5925-01-467-8494
NSN 6240-00-451-8587
NSN 5915-00-503-3773
NSN 6145-01-278-3832
NSN 5965-00-458-7321
NSN 5965-00-831-2134