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General Characteristics Primary Function: Air dominance, multi-role fighter Contractor: Lockheed-Martin, Boeing Power Plant: Two Pratt & Whitney F119-PW-100 turbofan engines with afterburners and two-dimensional thrust vectoring nozzles. Thrust: 35,000-pound class (each engine) Wingspan: 44 feet, 6 inches (13.6 meters) Length: 62 feet, 1 inch (18.9 meters) Height: 16 feet, 8 inches (5.1 meters) Weight: 43,340 pounds (19,700 kilograms) Maximum Takeoff Weight: 83,500 pounds (38,000 kilograms) Fuel Capacity: Internal: 18,000 pounds (8,200 kilograms); with 2 external wing fuel tanks: 26,000 pounds (11,900 kilograms) Payload: Same as armament air-to-air or air-to-ground loadouts; with or without 2 external wing fuel tanks. Speed: Mach 2 class with supercruise capability Range: More than 1,850 miles ferry range with 2 external wing fuel tanks (1,600 nautical miles) Ceiling: Above 50,000 feet (15 kilometers) Armament: One M61A2 20-millimeter cannon with 480 rounds, internal side weapon bays carriage of two AIM-9 infrared (heat seeking) air-to-air missiles and internal main weapon bays carriage of six AIM-120 radar-guided air-to-air missiles (air-to-air loadout) or two 1,000-pound GBU-32 JDAMs and two AIM-120 radar-guided air-to-air missiles (air-to-ground loadout) Crew: One |
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