Lockheed Martin F-35 Lightning II

The Lockheed Martin F-35 Lightning II is a single-seat, single-engined, all-weather stealth multirole fighters. The development of the F-35 started in 1992 with the Joint Strike Fighter program. The X-35 first flew on 24 October 2000 and the F-35A on 15 December 2006. The F-35 was developed to replace most US fighter jets with variants of one design common to all branches of the military.

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: 669 nmi (1,239 km) interdiction mission on internal fuel, 760 nmi (1,407 km) for internal air to air configuration
Service ceiling: 50,000+ ft (15,240+ m)
Wing loading: 107.5 lb/ft² (525 kg/m²; 745 kg/m² max loaded)
Thrust/weight:
With full fuel: 0.87
With 50% fuel: 1.07
Maximum g-load: 9 g