Civil Aerospace Defence Aerospace Marine Energy Services
Defence Aerospace

Introduction

Description

Technical data



The EJ200

EJ200

Technical data

Engine EJ200
Thrust (lbf) 20,000 (13,500 dry)
Bypass ratio 0.4
Pressure ratio 26
Length (in) 157
Diameter (in) 29
Basic weight (lb) 2,180
Compressor 3LP, 5HP
Turbine 1HP, 1LP
Technical data (ISA SLS)  

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