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EUROJET EJ200

EUROJET EJ200 is a two-shaft afterburning turbofan developed by an international European consortium of MTU Aero Engines, Rolls-Royce, Avio Aero, and ITP Aero for the Eurofighter Typhoon. MTU's technical brochure reports 13,500 lbf (60.05 kN) maximum thrust without afterburner, 20,000 lbf (88.96 kN) maximum thrust with afterburner, a 26:1 overall pressure ratio, and a 0.4:1 bypass ratio. The engine entered service in 2013 and remains in production; exact aircraft installations and later upgrade variants remain separate.

Identity

Aliases
EJ200Eurojet EJ200EUROJET Turbo EJ200
Domains
aviation
Identity Level
family
Kind
turbofan
Name
EUROJET EJ200
Status
active

Details

Air Breathing Specs
Afterburning Thrust Kn
88.96
Bypass Ratio
0.4
Max Thrust Kn
60.05
Overall Pressure Ratio
26
Spool Count
2
Description
EUROJET EJ200 is a two-shaft afterburning turbofan developed by an international European consortium of MTU Aero Engines, Rolls-Royce, Avio Aero, and ITP Aero for the Eurofighter Typhoon. MTU's technical brochure reports 13,500 lbf (60.05 kN) maximum thrust without afterburner, 20,000 lbf (88.96 kN) maximum thrust with afterburner, a 26:1 overall pressure ratio, and a 0.4:1 bypass ratio. The engine entered service in 2013 and remains in production; exact aircraft installations and later upgrade variants remain separate.
Developers
Manufacturers
Service Entry Date
2013

Links

Assets & Meta

Creation Time
August 6, 2026 at 18:39:20 UTC
Updated Time
August 23, 2026 at 20:53:22 UTC

Other

Sources