Biography


Three Types of F35 Fighter Jet:
1. F-35A, conventional take off and landing (CTOL) variant.
2. F-35B, short-take off and vertical-landing (STOVL) variant.
3. F-35C, carrier-based CATOBAR (CV) variant.


General characteristics
  • Crew: 1
  • Length: 51.4 ft (15.67 m)
  • Wingspan: 35 ft (10.7 m)
  • Height: 14.2 ft (4.33 m)
  • Wing area: 460 ft² (42.7 m²)
  • Empty weight: 29,300 lb (13,300 kg)
  • Loaded weight: 49,540 lb (22,470 kg)
  • Max takeoff weight: 70,000 lb (31,800 kg)
  • Powerplant: 1 × Pratt & Whitney F135 afterburning turbofan
    • Dry thrust: 28,000 lbf (125 kN)
    • Thrust with afterburner: 43,000 lbf (191 kN)
  • Internal fuel capacity: 18,480 lb (8,382 kg)
Performance
  • Maximum speed: Mach 1.6+ (1,200 mph, 1,930 km/h)
  • Range: 1,200 nmi (2,220 km) on internal fuel
  • Combat radius: over 590 nmi (1,090 km) on internal fuel[274]
  • Service ceiling: 60,000 ft (18,288 m)
  • Rate of climb: classified (not publicly available)
  • Wing loading: 91.4 lb/ft² (446 kg/m²)
  • Thrust/weight:
    • With full fuel: 0.87
    • With 50% fuel: 1.07
  • g-Limits:g
  • Missiles:
  • Air-to-air missiles:
    • AIM-120 AMRAAM
    • AIM-132 ASRAAM
    • AIM-9X Sidewinder
    • IRIS-T
    • MBDA Meteor (Pending further funding)
    • JDRADM (after 2020)
  • Air-to-surface missiles:
    • AGM-154 JSOW
    • AGM-158 JASSM
    • Brimstone missile
    • Joint Air-to-Ground Missile
  • Anti-ship missiles:
    • JSM
  • Bombs:
    • Mark 84, Mark 83 and Mark 82 GP bombs
    • Mk.20 Rockeye II cluster bomb
    • Wind Corrected Munitions Dispenser capable
    • Paveway-series laser-guided bombs
    • Small Diameter Bomb (SDB)
    • JDAM-series
    • B61 nuclear bomb

F-35A
CTOL
F-35B
STOVL
F-35C
Carrier version
Length 51.4 ft (15.7 m) 51.3 ft (15.6 m) 51.5 ft (15.7 m)
Wingspan 35 ft (10.7 m) 35 ft (10.7 m) 43 ft (13.1 m)
Wing Area 460 ft² (42.7 m²) 460 ft² (42.7 m²) 668 ft² (62.1 m²)
Empty weight 29,300 lb (13,300 kg) 32,000 lb (14,500 kg) 34,800 lb (15,800 kg)
Internal fuel 18,500 lb (8,390 kg) 13,300 lb (6,030 kg) 19,600 lb (8,890 kg)
Max takeoff weight 70,000 lb (31,800 kg) 60,000 lb (27,000 kg) 70,000 lb (31,800 kg)
Range 1,200 nmi (2,220 km) 900 nmi (1,670 km) 1,400 nmi (2,520 km)
Combat radius on
internal fuel
590 nmi (1,090 km) 450 nmi (833 km) 640 nmi (1,185 km)
Thrust/weight
full fuel
50% fuel
0.87
1.07
0.90
1.04
0.75
0.91