Adour Mk951  
Initial Operational Capability (IOC): 2005
Total Production: ?
Also Known As: Adour 951
Origin: France and United Kingdom
Corporations: Rolls-Royce and Snecma
Parent System: Adour
Initial Operational Capability (IOC):
Total Production: 2,600
Family Members: Adour Mk102, Adour Mk104, Adour Mk871 and F405-RR-401
There are no reviews so far

Description: The Adour is a family of turbofan engines developed in conjunction between Rolls-Royce and Turbomeca. These engines are available with or without afterburner. They were selected to power Jaguar, Hawk, T-45 Goshawk, Mitsubishi F-1 and T-2 aircraft.

The Adour Mk951 engine has been developed to power the latest variants of Hawk 100/200 aircraft. Adour 951 delivers 6,500 pounds of thrust and features 4,000 hours Time Between Overhaul and dual Full Authority Digital Engine Control (FADEC).

Adour Mk951 Applications

Combat Aircraft Hawk NEURON Taranis

Adour Mk951 Specifications

Fan Diameter: 580 millimeter (22.8 inch)
Length: 1,960 millimeter (77 inch)
Dry Weight: 610 kilogram (1,345 pound)
Thrust: 6,500 pound (2.95 ton)
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)

Adour Mk951 News

There are 2 news between
1 Dec 2012 and 12 Sep 2013
Thursday, September 12, 2013Rolls-Royce Joins BAE Systems' Hawk AJTS Team to Pursue US Air Force T-X Contract
Saturday, December 1, 2012European Unmanned Combat Aircraft Demonstrator nEUROn Makes its Maiden Flight

Operators & Related Equipment


Grand Total ?2
Copyright © 2003-2017 website. All rights reserved.
This website has been optimized for HTML 5 and CSS 3.