F/A-18 Hornet

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F/A-18 Hornet

Prime contractor:   Boeing
Principal contractor (airframe):  Northrop Corporation
Powerplant: Two General Electric F404-GE-400 low-bypass, turbofan engines; each in the 16,000-pound thrust class
Radar: Hughes APG-65 with long-range detection in both head-on and tail-on aspects
Length:   56 Feet
Height:   15.3 feet
Wingspan:   40.4 feet (with missles)
Wing area:   400 square feet
Speed:   Mach 1.7+ (1,200 mph)
First flight:   November 1978
Crew:   One (two in two-seat trainer version)
Combat radius:   500-plus nautical miles
Combat ceiling:   50,000 feet (approx.)
Fuel:   (approx.) 11,000 lbs. internal, 16,000 lbs. with external tanks.
Maximum takeoff weight:  56,000 lbs. (approx.) fighter escort missions
Cost:   Approximately $18 million

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