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Rolls-Royce Pegasus ✕ PW6124A ✕
EASA ID 7PW084
Aircraft Engine Manufacturer Bristol Engine Company (Bristol) Pratt & Whitney
Aircraft Engine Type Turbofan Turbofan
Dry Weight (kg) 1796.226
Diameter (mm) 1219.2
Length (mm) 3479.8
Wikipedia Article (URL) en.wikipedia.org/wiki/Rolls-Royce_Pegasus
Fuel Jet A
Geared Fan No No
Combustion Chamber Annular Talon II
Afterburner No No
Streams 2 2
Bypass Ratio 4.8
Overall Pressure Ratio 28
Maximum Takeoff Thrust (kN) 106 105.87
Thrust To Weight 6
Specific Fuel Consumption (g/(kN·s)) 21.527
Hydrocarbon Take Off (g/kg fuel) 0
Hydrocarbon Climb Out (g/kg fuel) 0.002
Hydrocarbon Approach (g/kg fuel) 0.001
Hydrocarbon Idle (g/kg fuel) 0.002
Hydrocarbon Unitary Average (g/kN) 0
Hydrocarbon Unitary Characteristic (g/kN) 0
Hydrocarbon Unitary Characteristicto Regulatory (% of limit) 0.1
Hydrocarbon LTO (g) 1
Carbon Monoxide Take Off (g/kg fuel) 0.68
Carbon Monoxide Climb Out (g/kg fuel) 0.81
Carbon Monoxide Approach (g/kg fuel) 3.69
Carbon Monoxide Idle (g/kg fuel) 25.19
Carbon Monoxide Unitary Average (g/kN) 46.2
Carbon Monoxide Unitary Characteristic (g/kN) 56.7
Carbon Monoxide Unitary Characteristicto Regulatory (% of limit) 48.2
NOx Take Off (g/kg fuel) 21.03
NOx Climb Out (g/kg fuel) 15.85
NOx Approach (g/kg fuel) 6.88
NOx Idle (g/kg fuel) 3.58
NOx Unitary Average (g/kN) 39.4
NOx Unitary Characteristic (g/kN) 45.7
NOx Unitaryto Standard (% of limit) 47.6
NOx Unitaryto CAEP2 (% of limit) 59.5
NOx Unitaryto CAEP4 (% of limit) 71.6
NOx Unitaryto CAEP6 (% of limit) 81.4
NOx Unitaryto CAEP8 (% of limit) 96.6
NOx LTO (g) 4170
Smoke Take Off (SN) 5.16
Smoke Climb Out (SN) 4.71
Smoke Approach (SN) 1.32
Smoke Idle (SN) 1.51
Smoke Max (SN) 5.16
Smoke Characteristic (SN) 6.7
Smoke Characteristicto Regulatory (% of limit) 28.5
Fuel Flow Take Off (kg/s) 1.169
Fuel Flow Climbout (kg/s) 0.939
Fuel Flow Approach (kg/s) 0.325
Fuel Flow Idle (kg/s) 0.114
Fuel LTO (kg) 429
Fuel Venting Compliant No
Carbon Monoxide LTO (g) 4901
Compressor Description 3-stage low pressure, 8-stage high pressure axial flow
Emissions Data Status C
Engine Status Out of production
NOx Compliance Demonstration 2.3.2 e)
Turbine Description 2-stage high pressure, 2-stage low pressure