Rolls-Royce Turbomeca Adour

Turbofan · Rolls-Royce Turbomeca
Reaction Turbines
Bypass Ratio
0.75
Diameter
570 mm
Length
2900 mm
Dry Weight
809.2088 kg
Thrust To Weight
4.725

Architecture

Fan Fan Stages — Fan Blades — Fan Technology — Fan Pressure Ratio —
Gearbox Geared Fan No Gear — Reduction Ratio —
LP compressor Low-Pressure Compressor Stages — Low-Pressure Compressor Technology — BP Compressor Pressure Ratio —
IP compressor Intermediary-Pressure Compressor Stages — Intermediary-Pressure Compressor Technology — IP Compressor Pressure Ratio —
HP compressor High-Pressure Compressor Stages — High-Pressure Compressor Technology — HP Compressor Pressure Ratio —
Combustor Combustion Chamber —
HP turbine High Pressure Compressor Stages — High-Pressure Turbine Technology —
IP turbine Intermediary-Pressure Turbine Stages — Intermediary-Pressure Turbine Technology —
LP turbine Low-Pressure Turbine Stages — Low-Pressure Turbine Technology —
Whole engine Streams 2 Bypass Ratio 0.75 Overall Pressure Ratio — Afterburner No

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Airplanes

Name Aircraft Engine Number of Engines Length (m) Flat Wing Span (m)
BAE Systems Hawk Rolls-Royce Turbomeca Adour 1 12.192 9.7536
BAE Systems Taranis Rolls-Royce Turbomeca Adour 1 12.43 10
Dassault nEUROn Rolls-Royce Turbomeca Adour 1 9.5 12.5
All data (14 fields)
Name
Rolls-Royce Turbomeca Adour
Aircraft Engine Manufacturer
Rolls-Royce Turbomeca
Aircraft Engine Type
Turbofan
Dry Weight (kg)
809.2088
Diameter (mm)
570
Length (mm)
2900
Wikipedia Article (URL)
en.wikipedia.org/wiki/Rolls-Royce_Turbomeca_Adour
Geared Fan
No
Afterburner
No
Streams
2
Bypass Ratio
0.75
Thrust To Weight
4.725
Compressor Description
2-stage LP, 5-stage HP
Turbine Description
1-stage LP, 1-stage HP