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BR700
IOC: 1997
BR710
Production: 500
Also Known As
BR710A2-20
Origin
United Kingdom
Contractor/s
Rolls-Royce
Applications
Global 5000
Global Express XRS
Gulfstream G500
Gulfstream G550
Sentinel R Mk 1
Family Members
BR715
BR725
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Description:
The BR700 engine was developed by Rolls Royce to achieve new emissions, fuel consumption and noise levels. BR700 engines were developed to meet the requirements of regional aircraft (80-130 passengers).
The BR710 engines, a derivative of BR700, power the newest Nimrod maritime patrol aircraft variant, known as MRA4 with certification on the aircraft achieved in 2001. The BR710 engine has been certified on the Gulfstream V (1997), Gulfstream G500 (2004), Gulfstream G550 (2004), Bombardier Global Express (1999) and Tupolev Tu-334 (2003).
Specifications
Dimensions: Diameter 1,220 mm, Length 3.4 m
Weights: Max Weight 1,633 kg (3,600 lb)
Engine/s Performance: Thrust 15,000 lb (6,804 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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