Saturday, September 06, 2008

MTR390

IOC: 1993

Origin:France, Germany, United Kingdom

Contractor/s: MTU Aero Engines, Rolls-Royce, Snecma

Description: The MTR390 engine was developed jointly by Rolls Royce, Turbomeca and MTU to meet the high performance requirements for Eurocopter's Tiger multipurpose helicopter.

MTR390 is suitable for civil and military uses having low ownership costs, low fuel consumption, low acceleration and simple maintenance.

Specifications
Dimensions: Height 680 mm, Length 1,080 mm, Width 440 mm

Weights: Max Weight 169 kg (373 lb)

Power: Power 1,285 shp

Applications
Tiger ARH, Tiger HAD, Tiger HAP, Tiger UHT

Notes
(*) lead contractor
IOC: Initial Operating Capability
FOC: Full Operating Capability
CEP: Circular Error Probable
Comm: Commissioning Date
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)

Last Updated: Sunday, August 24, 2008

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