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F-4 Phantom II
The F-4 Phantom II is a twin engine, two-seat, supersonic fighter developed by the U.S. Navy. It was developed as an attack aircraft and later changed into an advanced long-range all-weather interceptor with missile armament. The Phantom was in production from 1958 - 1981 and was used extensively in the Vietnam War. It has been used by 11 other nations and still remains in front line service for seven countries.
FACTS & STATS:
First Flown
1958
Range
1,615 miles (2,600 km)
Length
63 ft (19.2 m)
Engine
Two General Electric J79-GE-17A axial compressor turbojets, 17,845 lb. (79.6 kg) each
Wingspan
38 ft 4 in (11.7 m)
Max Speed
1,472 mph (2,370 km/h) (Mach 2)
Ceiling
60,000 ft (18,300 m)
Weight
Empty: 30,328 lbs (13,757 kgs);
Loaded: 41,500 lbs (18,824 kgs)
Number Built
5,195
Armament
One 20 mm M61A1 Vulcan gatling cannon; four AIM-9 Sidewinder AAMs; up to 16,000 (7,258 kg) of weapons
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