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Description
General characteristics

* Crew: 1
* Length: 50 ft 6 in (15.37 m)
* Wingspan: 35 ft 0 in (10.65 m)
* Height: 17 ft 4 in (5.28 m)
* Wing area: 459.6 ft² (42.7 m²
* Empty weight: A; 29,036 lb B; 32,161 lb C; 32,070 lb (13,170 kg A; 14,588 kg B; 14547 kg C
* Loaded weight: 44,400 lb (20,100 kg)
* Max takeoff weight: 60,000 lb (27,200 kg)
* Powerplant: 1× Pratt & Whitney F135 afterburning turbofan
o Dry thrust: 25,000 lbf[68] (111 kN)
o Thrust with afterburner: 40,000+ lbf[68] (178+ kN)
* Secondary Powerplant: 1× General Electric/Rolls-Royce F136 afterburning turbofan, >40,000 lbf (178 kN) [in development]
* Lift fan (STOVL): 1× Rolls-Royce Lift System driven from either F135 or F136 power plant, 18,000 lbf (80 kN)
* Internal fuel: F-35A: 18,480 lb (8,382 kg); F-35B: 14,003 lb (6,352 kg); F-35C: 20,085 lb (9,110 kg)

Performance

* Maximum speed: Mach 1.6+[68] (1,200 mph, 1,931 km/h)
* Range: A: 1,200 nmi; B: 900 nmi; C: 1400 nmi[68] (A: 2,200 km; B: 1,667 km; C: 2,593 km) on internal fuel
* Combat radius: 600 nmi (690 mi, 1,110 km)
* Rate of climb: classified (not publicly available)
* Wing loading: 91.4 lb/ft² (446 kg/m²
* Thrust/weight:
o With full fuel: A: 0.89; B: 0.92; C: 0.81[68]
o With 50% fuel: A: 1.12; B: 1.10; C: 1.01[68]

g-Limits[86]

* F-35A: 9 g
* F-35B: 9 g
* F-35C: 9 g

Armament

* Guns: 1 × GAU-22/A 25 mm cannon — slated to be mounted internally with 180 rounds in the F-35A and fitted as an external pod with 220 rounds in the F-35B and F-35C.[68]
* Hardpoints: 6 with a capacity of 15,000 lb (6,800 kg)[68],
* Missiles: Internal: 4 air-air missiles or 2 air-air missiles and 2 air-surface weapons; External: 2 missiles and 4 missiles/bombs

Description
General characteristics

* Crew: 1
* Length: 50 ft 6 in (15.37 m)
* Wingspan: 35 ft 0 in (10.65 m)
* Height: 17 ft 4 in (5.28 m)
* Wing area: 459.6 ft² (42.7 m²
* Empty weight: A; 29,036 lb B; 32,161 lb C; 32,070 lb (13,170 kg A; 14,588 kg B; 14547 kg C
* Loaded weight: 44,400 lb (20,100 kg)
* Max takeoff weight: 60,000 lb (27,200 kg)
* Powerplant: 1× Pratt & Whitney F135 afterburning turbofan
o Dry thrust: 25,000 lbf[68] (111 kN)
o Thrust with afterburner: 40,000+ lbf[68] (178+ kN)
* Secondary Powerplant: 1× General Electric/Rolls-Royce F136 afterburning turbofan, >40,000 lbf (178 kN) [in development]
* Lift fan (STOVL): 1× Rolls-Royce Lift System driven from either F135 or F136 power plant, 18,000 lbf (80 kN)
* Internal fuel: F-35A: 18,480 lb (8,382 kg); F-35B: 14,003 lb (6,352 kg); F-35C: 20,085 lb (9,110 kg)

Performance

* Maximum speed: Mach 1.6+[68] (1,200 mph, 1,931 km/h)
* Range: A: 1,200 nmi; B: 900 nmi; C: 1400 nmi[68] (A: 2,200 km; B: 1,667 km; C: 2,593 km) on internal fuel
* Combat radius: 600 nmi (690 mi, 1,110 km)
* Rate of climb: classified (not publicly available)
* Wing loading: 91.4 lb/ft² (446 kg/m²
* Thrust/weight:
o With full fuel: A: 0.89; B: 0.92; C: 0.81[68]
o With 50% fuel: A: 1.12; B: 1.10; C: 1.01[68]

g-Limits[86]

* F-35A: 9 g
* F-35B: 9 g
* F-35C: 9 g

Armament

* Guns: 1 × GAU-22/A 25 mm cannon — slated to be mounted internally with 180 rounds in the F-35A and fitted as an external pod with 220 rounds in the F-35B and F-35C.[68]
* Hardpoints: 6 with a capacity of 15,000 lb (6,800 kg)[68],
* Missiles: Internal: 4 air-air missiles or 2 air-air missiles and 2 air-surface weapons; External: 2 missiles and 4 missiles/bombs