RR300
IOC: 2008
Origin United Kingdom
Program Status: Under Development
Contractor/s
Rolls-Royce
Applications
R66 RR500 S-434
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Description:
The Rolls Royce RR300 is an engine family featuring new technology and advanced design. The new turbine intended for rotary-wing aircraft applications will provide to end customers: lower acquisition and operating costs; low-weight, compact design; improved specific fuel consumption; an embedded engine monitoring system; and an optional, through-life, peace-of-mind maintenance program. FAA type certification is expected in 2008.
Specifications
Dimensions: Diameter 25 in
Weights: Weight 200 lb (91 kg)
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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: Friday, October 10, 2008
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