Military Engines: 
General Electric F404-GE-402 


 
Characteristics
Maximum thrust: 17,700 lbs.  78.7 kN
Weight: 2,282 lbs  1,035 kg
Length: 154 inches  391 cm
Inlet diameter: 31 inches  79 cm
Maximum diameter: 35 inches  89 cm
Airflow: 146 lbs/sec  66 kg/sec
Pressure Ratio: 26-to-1

   The F404-GE-402 Enhanced Performance Engine (EPE) provides higher power, improved fuel efficiency and increased mission capability for the F/A-18C/D Hornet. It retains the proven design characteristics of the baseline F404, while achieving increased performance through improved thermodynamic cycle and increased temperature. These performance improvements with no loss in durability were made possible by applying the latest technology and materials to the turbine and afterburner sections of the engine.