Eurojet EJ200

Turbofan · EuroJet
Reaction Turbines
Maximum Takeoff Thrust
60 kN
Bypass Ratio
0.4
Diameter
736.6 mm
Length
3987.8 mm
Dry Weight
989 kg
Thrust To Weight
6.11

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 Annular
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 0.4 Overall Pressure Ratio — Afterburner Yes

Pictures

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Airplanes

Name Aircraft Engine Number of Engines Length (m) Flat Wing Span (m)
Eurofighter Typhoon Eurojet EJ200 2 15.96 10.95

Similar reaction turbines

Name Aircraft Engine Manufacturer Maximum Takeoff Thrust (kN) Bypass Ratio
Snecma M53 SNECMA 64 0.36 Compare
Pratt & Whitney PW1120 Pratt & Whitney 61.18 Compare
Volvo RM12 Volvo Aero 54 0.31 Compare
Lyulka AL-7 Lyulka-Saturn 67.1 Compare
Lyulka AL-5 Lyulka-Saturn 52 Compare
Pratt & Whitney J57 Pratt & Whitney 52 Compare
All data (17 fields)
Name
Eurojet EJ200
Aircraft Engine Manufacturer
EuroJet
Aircraft Engine Type
Turbofan
Dry Weight (kg)
989
Diameter (mm)
736.6
Length (mm)
3987.8
Wikipedia Article (URL)
en.wikipedia.org/wiki/Eurojet_EJ200
Geared Fan
No
Combustion Chamber
Annular
Afterburner
Yes
Streams
2
Bypass Ratio
0.4
Maximum Takeoff Thrust (kN)
60
Thrust To Weight
6.11
Afterburner Thrust (kN)
60
Compressor Description
Axial, 3-stage LP, 5-stage HP
Turbine Description
1-stage LP, 1-stage HP