T700-T6E  
Initial Operational Capability (IOC):
Total Production: ?
Also Known As: T6E
Origin: United States of America
Corporations: General Electric
Parent System: T700
Initial Operational Capability (IOC): 1978
Total Production: 20,100
Family Members: CT7, CT7-2, CT7-8, CT7-8C, CT7-8E, T700-GE-401, T700-GE-401C, T700-GE-700, T700-GE-701, T700-GE-701C, T700-GE-701D, T700-GE-701E, T700-T6A, T700-T6A1, T700-T6E1 and T706-GE-700
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Description: The T700 engine was designed for the US Army's UH-60A Black Hawk helicopter as a result of lessons learned in Vietnam. The key requirements of this engine were reliability, operation under adverse environmental conditions and low maintainability.

The T6E engine is the most powerful derivative to date of T700 engine. T6E reduces pilot workload and enhances maintainability. The T6E is one of two alternative propulsion systems approved to power NH90 helicopters.

T700-T6E Specifications

Dimensions
Diameter: 400 millimeter (15.7 inch)
Length: 1,190 millimeter (47 inch)
Power
Max Power at TakeOff: 2,542 shp (1,896 kW)
Weight
Dry Weight: 233 kilogram (514 pound)
CEP: Circular Error Probable
Meters (m)   Kilometers (km)   Nautic Miles (nm)   Inch (in)   Yard (yd)   Foot (ft)   Millimeter (mm)
Pound (lb)   Kilogram (kg)   kN (KiloNewton)   Ton (t)
Meters per Second (mps)   Kilometers per Hour (kph)   Knot (kt)   Miles per Hour (mph)
Liter (l)   Galon (gl)
Year (yr)   Minutes (min)   Second (sec)
Shaft-Horse-Power (shp)
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