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RolePrototype/DemonstratorManufacturerLockheed Martin AeronauticsFirst flight24 October 2000[1]StatusRetiredPrimaryuserDefense Advanced Research Projects AgencyNumber built2 (X-35A/B and X-35C)Developed into
F-35 Lightning II
General characteristics
Performance
F-35 Lightning II
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: 459.6ft2 (42.7m2)
- Empty weight: 26,000 lb (11,793 kg)
- Loaded weight: 44,400 lb (19,960 kg)
- Max. takeoff weight: 60,000 lb (27,220 kg)
- Powerplant: 1 Ã Pratt & Whitney F135 afterburning turbofan coupled to Rolls-Royce Lift System to give 18,000 lbf (80 kN) lift thrust
- Dry thrust: 28,000 lbf (128 kN)
- Thrust with afterburner: 43,000 lbf (191 kN)
- Dry thrust: 28,000 lbf (128 kN)
Performance
- Maximum speed: Mach 1.6 (1,200 mph, 1930 km/h)
- Range: approx. 1,200 nmi (roughly 2,222 km)on internal fuel
- Rate of climb: 315m/s ()
- Wing loading: 91.4 lb/ft² (446 kg/m²)
- Thrust/weight: 0.968 with full fuel, 1.22 with 50% fuel
Additional Notes
http://en.wikipedia.org/wiki/Lockheed_Martin_X-35Progress | 100% complete |
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