Turbo-Union RB199

Turbofan · Turbo-Union
Reaction Turbines
Diameter
718.82 mm
Length
3606.8 mm
Dry Weight
975.6772 kg
Thrust To Weight
7.6

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 — Overall Pressure Ratio — Afterburner No

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Airplanes

Name Aircraft Engine Number of Engines Length (m) Flat Wing Span (m)
British Aerospace EAP Turbo-Union RB199 2 14.6304 11.5824
HAL HF-73 Turbo-Union RB199 2 15.13 9
Panavia Tornado Turbo-Union RB199 2 16.72 13.91
All data (13 fields)
Name
Turbo-Union RB199
Aircraft Engine Manufacturer
Turbo-Union
Aircraft Engine Type
Turbofan
Dry Weight (kg)
975.6772
Diameter (mm)
718.82
Length (mm)
3606.8
Wikipedia Article (URL)
en.wikipedia.org/wiki/Turbo-Union_RB199
Geared Fan
No
Afterburner
No
Streams
2
Thrust To Weight
7.6
Compressor Description
3-stage LP, 3-stage IP, 6-stage HP
Turbine Description
Single-crystal HP, single-crystal IP, 2-stage LP