Lockheed-Martin F-35 Lightning II
2006
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Lockheed-Martin F-35 Lightning II

The F-35 Lightning II — descended from the X-35 of the Joint Strike Fighter (JSF) program — is a single-seat, single-engined military strike fighter, a multi-role aircraft that can perform close air support, tactical bombing, and air-to-air combat. Its development is being funded by the United States, the United Kingdom, and other partner governments. It is being designed and built by an aerospace industry team led by Lockheed Martin and major partners BAE Systems and Northrop Grumman. Demonstrator aircraft flew in 2000; a production model first took flight on 15 December 2006.

SEE ALSO

Lockheed-Martin F-35 Lightning II


Specification 
 MODELF-35 Lightning II
 CREW1
 ENGINE1 x 12700kg Pratt & Whitney F135 turbofan + 1 x 8170kg Rolls-Royce Lift System
 WEIGHTS
    Take-off weight27200 kg59966 lb
    Empty weight12000 kg26456 lb
 DIMENSIONS
    Wingspan10.65 m34 ft 11 in
    Length15.37 m50 ft 5 in
    Height5.28 m17 ft 4 in
    Wing area42.7 m2459.62 sq ft
 PERFORMANCE
    Max. speed1930 km/h1199 mph
    Range2200 km1367 miles
 ARMAMENT1 x 25mm cannon

Comments 
Akim, akim(@)mail.ru, 25.10.2008

amerikosi otsasivayut! russkaya aviaciya samaya aviacionnaya v mire ))))

Mayakovskij, 08.09.2008

Letaet, strelyaet. Znachit mozhet i popast' )))

Pushkin, 23.06.2008

Stopudov chuvak

bmilic, generalbmilic(@)yahoo.com, 19.05.2008

Sranje, govno

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