F-4 Phantom II
F-4G Advanced Wild Weasel
Specifications | ||||
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Primary Function | All-weather fighter-bomber. | |||
Contractor | McDonnell Aircraft Co., McDonnell Corporation. | |||
Power Plant | Two General Electric turbojet engines with afterburners. | |||
Thrust | 17,900 pounds (8,055 kilograms). | |||
Length | 62 feet, 11 inches (19.1 meters). | |||
Height | 16 feet, 5 inches (5 meters). | |||
Wingspan | 38 feet, 11 inches (11.8 meters). | |||
Speed | More than 1,600 mph (Mach 2). | |||
Ceiling | 60,000 feet (18,182 meters). | |||
Climb Rate | 49,000 ft per minute | |||
Maximum Takeoff Weight | 62,000 pounds (27,900 kilograms). | |||
Range | 1,300 miles (1,130 nautical miles). | |||
Armament | Four AIM-7 Sparrow and four AIM-9M Sidewinder missiles, AGM-65 Maverick missiles, AGM-88 HARM missile capability, and one fuselage centerline bomb rack and four pylon bomb racks capable of carrying 12,500 pounds (5,625 kilograms) of general purpose bombs.
15 CBU-52 15 CBU-58 15 CBU-71 15 CBU-87 15 CBU-89 12 MK-20 6 BL-755 | |||
Systems |
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Cost | $18.4 million. | |||
Crew | Two (pilot and electronic warfare officer). | |||
Date Deployed | May 1963. | |||
Production |
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Inventory | None - retired December 1995 [formerly F-4G -- Active force, 24; ANG, 24; Reserve, 0.] |
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