Engine Specification

This Information focuses on the Eurofighter Typhoon''s powerplant, the EJ200 and the six high-end sub-systems incorporated into the aircraft''s overall system architecture. Please click on a tab to learn more about these systems.

EJ200 Engine
Sub-Systems

Overview
Engine Specification
Built in Growth Potential

Thrust - maximum, dry Thrust - with reheat 'g' limits	60 kn 90 kN +9/-3 'g'	(13500 lbs stat) (20000 lbs stat)
Bypass ratio	0.4
Overall pressure ratio	26:1
Thrust/Weight ratio	10:1
Average fuel consumption - max, dry - With reheat	21 - 23 g/kNs 47 - 49 g/kNs	(0.74 - 0.81 lb/lb/hr) (1.66 - 1.73 lb/lb/hr)
Overall length	4 m	(157 ins)
Inlet diameter	0.74 m	(29 ins)
Typical weight	990 - 1035 kg	(2180 - 2280 lb)