Description:

108.000 inches overall length, 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 deg fahrenheit .

Special Features:

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

Properties:

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.