
General characteristics
Crew: 1
Length: 62 ft 1 in (18.92 m)
Wingspan: 44 ft 6 in (13.56 m)
Height: 19 ft 8 in (5.9 m)
Wing area: 840 ft² (78.04 m²)
Airfoil: NACA 64A?05.92 root, NACA 64A?04.29 tip
Empty weight: 43,340 lb (19,700 kg)
Loaded weight: 64,840 lb (29,410 kg)
Max. takeoff weight: 83,500 lb (38,000 kg)
Powerplant: 2 × Pratt & Whitney F135 afterburning turbofan
Dry thrust: 28,000 lb (125 kN) each
Thrust with afterburner: 43,000+ lb (191 kN+ kN) each
Fuel capacity: 8,000 lb (8,200 kg) internally, or 26,000 lb (12,000 kg) with two external fuel tanks
Performance
Maximum speed
At altitude: Mach 2.25 (1,500 mph, 2,410 km/h)
Supercruise: Mach 1.82 (1,220 mph, 1,960 km/h)
Range: >1,600 nmi (1,840 mi, 2,960 km) with 2 external fuel tanks
Combat radius: 410 nmi (with 100 nmi in supercruise) (470 mi, 760 km)
Ferry range: 2,000 mi (1,740 nmi, 3,220 km)
Service ceiling: >65,000 ft (20,000 m)
Wing loading: 77.2 lb/ft² (377 kg/m²)
Thrust/weight: 1.08
Maximum design g-load: −3.0/+9.0 g
Avionics
AN/APG-77 radar: 125–150 miles (200–240 km) against 1 m2 (11 sq ft) targets (estimated range)
AN/AAR-56 Missile Launch Detector (MLD)
AN/ALR-94 radar warning receiver (RWR): 250 nmi (463 km) or more detection range
MJU-39/40 flares for protection against IR missiles
Armament
Guns: 1× 20 mm (0.787 in) M61A2 Vulcan 6-barrel Gatling cannon in right wing root, 480 rounds
Air to air loadout:
6× AIM-120 AMRAAM
2× AIM-9 Sidewinder
Air to ground loadout:
2× 1,000 lb (450 kg) JDAM or 8× 250 lb (110 kg) GBU-39 Small Diameter
Bombs
2× AIM-120 AMRAAM
2× AIM-9 Sidewinder
Hardpoints: 4× under-wing pylon stations can be fitted to carry 600 U.S. gallon drop tanks or weapons, each with a capacity of 5,000 lb (2,270 kg).