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F-4 Phantom II

F-4 Phantom II

F-4 Phantom II

F-4 Phantom II

F-4 Phantom II

F-4 Phantom II
       
    Contractor: McDonnell Douglas
First flight: May 27, 1958 (prototype YF4H-1)
Wingspan: 38 feet 5 inches
Length: 58 feet 3 inches
Height: 16 feet 6 inches
Ceiling: 56,100 feet
Range: 1,750 miles
Weight: 55,597 pounds
Power plant: Two 17,900-pound-thrust General Electric J79-GE-17 jet engines
Speed: 1,485 mph (max.)
Accommodation: Two crew
Armament: 15,983 pounds of weapons, including 20 mm nose-mounted M-61 "Vulcan" cannon