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Initial Operational Capability (IOC):
Also Known As: RTM 322 04/7
and United Kingdom
Rolls-Royce and Turbomeca* (*) lead contractor
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Description: In the 1990s, Rolls Royce and Turbomeca jointly developed the RTM322 turboshaft family to suit a wide range of commercial and military helicopter applications powered by two or three engines. The turboshaft family was designed to develop 2,100-shp at takeoff with future growth to 3,300-shp. The RTM 322 engine has been selected to power the AgustaWestland AW101, NH Industries NH90 and GKN Westland WAH-64 helicopters with approximately 1,600 engines ordered or on order. More than 900 RTM 322 engines have been produced so far, logging more than 450,000 flight hours.
The RTM322-04/7 turboshaft engine was proposed as an alternative powerplant for the Sikorsky S-92 helicopter.
Max Power at TakeOff: 2,647 shp (1,975 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)
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