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General Electric T700/CT7

The Engine Specifications (CT7-9B)
Introduced in 1978, the T700 was designed for the U.S. Army's Black Hawk helicopter with the lessons of Vietnam in mind.  The civil CT7 was available in 1984.
Compressor: 6-stage
Turbine: 2-stage LP/2-stage HP
Pressure ratio: 18
Models Used by
CT7-9B: 1,750 hp (1305 kW)
T700-401: 1,690 hp (1261 kW)
Saab 340
Sikorsky UH-60 Black Hawk
Related Pages Related Websites
More about General Electric
General Electric: CT7
General Electric: T700

page updated 04 July 2003



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