Military Engines: 
General Electric F414-GE-400 


 
Characteristics
Maximum thrust: 22,000 lbs.  98 kN
Thrust-to-Weight: 9 to 1 class
Length: 154 inches  391 cm
Inlet diameter: 32 inches  81 cm
Maximum diameter: 35 inches  89 cm
Airflow: 170 lbs/sec 77.1 kg/sec
Pressure Ratio: 30-to-1

   The F414-GE-400 builds upon the excellent reliability, operability and readiness of the F404 engine. The F414 delivers 35% more thrust than the original F404, significantly improving the Boeing F/A-18 E/F Super Hornet's range, payload and survivability. Advanced technology features such as a Full Authority Digital Electronic Control (FADEC) improve operational characteristics of the engine while the latest materials and cooling techniques allow for higher temperatures and pressures without sacrificing component life.