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General Characteristics Primary function: Tactical fighter Contractor: McDonnell Douglas Corp. Power plant: Two Pratt & Whitney F100-PW-100, 220 or 229 turbofan engines with afterburners Thrust: (C/D models) 23,450 pounds each engine Wingspan: 42.8 feet (13 meters) Length: 63.8 feet (19.44 meters) Height: 18.5 feet (5.6 meters) Weight: 31,700 pounds Maximum takeoff weight: (C/D models) 68,000 pounds (30,844 kilograms) Fuel Capacity: 36,200 pounds (three external plus conformal fuel tanks) Payload: depends on mission Speed: 1,875 mph (Mach 2 class) Ceiling: 65,000 feet (19,812 meters) Range: 3,450 miles (3,000 nautical miles) ferry range with conformal fuel tanks and three external fuel tanks Crew: F-15A/C: one. F-15B/D/E: two Armament: One internally mounted M-61A1 20-mm, six-barrel cannon with 940 rounds of ammunition; four AIM-9L/M Sidewinder and four AIM-7F/M Sparrow air-to-air missiles, or eight AIM-120 AMRAAMs, carried externally. |
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