Basic information:
Crew: 1 Length: 63.8 ft (19.44 m) Wingspan: 42.8 ft (13 m) Height: 18.5 ft (5.6 m) Wing area: 608 ft² (56.5 m²) Airfoil: NACA 64A006.6 root, NACA 64A203 tip Empty weight: 28,000 lb (12,700 kg) Loaded weight: 44,500 lb (20,200 kg) Max takeoff weight: 68,000 lb (30,845 kg) Powerplant: 2× Pratt & Whitney F100-220 or 229 afterburning turbofans Dry thrust: 17,450 lbf (77.62 kN) each Thrust with afterburner: 25,000 lbf for -220; 29,000 lbf for -229 (111.2 kN for -220; 129.0 kN for -229) each Performance Maximum speed: Low altitude: Mach 1.2 (900 mph, 1,450 km/h) High altitude: Mach 2.5 (1,875 mph, 3,018 km/h) Ferry range: 3,000 nm (3,500 mi, 5,600 km) with external fuel and conformal fuel tanks Service ceiling: 65,000 ft (20,000 m) Rate of climb: >50,000 ft/min (254 m/s) Wing loading: 73.1 lb/ft² (358 kg/m²) Thrust/weight: 1.12 (-220), 1.30 (-229) Armament Guns: 1× internally mounted 20 mm (0.787 in) M61A1 gatling gun, 940 rounds Hardpoints: 4 wing, 4 fuselage, 2 wing stations, centerline station, optional fuselage pylons with a capacity of 16,000 lb (7,300 kg), Missiles: AIM-7F Sparrow AIM-120 AMRAAM AIM-9 Sidewinders Avionics Radar: Raytheon AN/APG-63 or AN/APG-70 or Raytheon AN/APG-63(V)2 Active Electronically Scanned Array (AESA) Countermeasures: AN/APX-76 IFF interrogator AN/ALQ-128 radar warning suite AN/ALR-56 radar warning receiver ALQ-135 internal countermeasures system AN/ALE-45 chaff/flare dispensers
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