Initial Operational Capability (IOC): 2001
Total Production: ?
Origin: United Kingdom and United States of America
Corporations: Honeywell and Rolls-Royce
Parent System: T800
Initial Operational Capability (IOC): 1993
Total Production: ?
Family Members: CTS800 and T800-LHT-800
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Description: The T800 is a family of turboshaft engines developed jointly between Honeywell and Rolls Royce under the Light Helicopter Turbine Engine Company (LHTEC). These engines are rated between 1,300 - 1,800-shp featuring modular design and ease of maintenance. The T800 engine was developed to power high performance light/medium helicopters operating in the military range such as the US Army RAH-66 Comanche (now cancelled).

LHTEC T800-LHT-801 was a variant of T800-LHT-800 turbine engine provided with increased power and intended to power production RAH-66 Comanche helicopters from 2006. Ultimately, the RAH-66 Comanche was cancelled by the US Army in 2004.

T800-LHT-801 Applications

Combat Aircraft RAH-66 Comanche

T800-LHT-801 Specifications

Max Power at TakeOff: 1,521 shp (1,135 kW)
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)

Operators & Related Equipment


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