Rolls-Royce Avon was the first axial flow jet engine designed and produced by Rolls-Royce. Introduced in 1950, it went on to become one of their most successful post-World War II engine designs. It was used in a wide variety of aircraft, both military and civilian, as well as versions for stationary and maritime power. Production of the Avon aero engine version ended after 24 years in 1974.
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General characteristics :
Type: Turbojet
Length: 126 in (3,200 mm)
Diameter: 35.7 in (907 mm)
Dry weight: 2,890 lb (1,310 kg)
Components:
Compressor: 15-stage axial flow
Combustors: Cannular, 150 lb/s (68 kg/s)
Turbine: Two-stage axial flow
Fuel type: Kerosene
Performance :
Maximum thrust: 12,690 lbf (56.4 kN)dry/16,360 lbf (72.8 kN) with reheat
Overall pressure ratio: 7.45:1
Specific fuel consumption: 0.932 lb/lbf h (28 g/kN•s) (dry) 1.853 lb/lbf h (wet)
Thrust-to-weight ratio: 5.66:1 (56 N/kg)
S&S Turbine Services Middle East LLC
No. 49 , DIP Dubai-UAE
POBOX: 450630/Dubai
Tel: +97 14 88 00 281
Fax: + 97 14 88 00 291
Mob: +97 150 55 16 779
Email: info@ssturbineme.com
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