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Старожил
Форумчанин
Все верно, перепутал с F-8K. Только обрати самое пристальное внимание на носовой конус -он острый, а у E/J более оживальный.
F8U-2 (F-8C) - J57-P-16 engine with 16,900 lbf (75 kN) of afterburning thrust, ventral fins added under the rear fuselage in an attempt to rectify yaw instability, Y-shaped chin pylons allowing two Sidewinder missiles on each side of the fuselage, first flight 20 August 1957, 187 built. This variant was sometimes referred to as Crusader II.[8]
F8U-2N (F-8D) - all-weather version, unguided rocket pack replaced with an additional fuel tank, J57-P-20 engine with 18,000 lbf (80 kN) of afterburning thrust, landing system which automatically maintained present airspeed during approach, first flight 16 February 1960, 152 built.
YF8U-2N (YF-8D) - one aircraft used in the development of the F8U-2N.
YF8U-2NE - one F8U-1 converted to serve as an F8U-2NE prototype.
F8U-2NE (F-8E) - J57-P-20A engine, AN/APQ-94 radar in a larger nose cone, dorsal hump between the wings containing electronics for the AGM-12 Bullpup missile, payload increased to 5,000 lb (2,270 kg), Martin-Baker ejection seat, first flight 30 June 1961, 286 built.
F-8E(FN) - air superiority fighter version for the French Navy, significantly increased wing lift due to greater slat and flap deflection and the addition of a boundary layer control system, enlarged stabilators, 42 built.
F-8H - upgraded F-8D with strengthened airframe and landing gear, 89 rebuilt.
F-8J - upgraded F-8E, similar to F-8D but with wing modifications and BLC like on F-8E(FN), "wet" pylons for external fuel tanks, J57-P-20A engine, 136 rebuilt.
F-8K - upgraded F-8C with Bullpup capability and J57-P-20A engines, 87 rebuilt.
Последний раз редактировалось Sergei Galicky; 04.03.2009 в 15:19.
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