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T-50 / Project 701 / PAK FA
[Perspektivnyi Aviatsionnyi Kompleks Frontovoi Aviatsyi]

Although T-50 specifications remain classified, fragmentary data on its engines imply that this heavy-duty fighter will have a take-off weight of more than 30 metric tons and will be close in dimension to the well-known Sukhoi Su-27 Flanker.

Crew 1 and 2 (pilot)
Length 22 m (70 ft)
Wingspan 14 m (45 ft)
Height 6 m (20 ft)
Wing area 80 m (850 ft)
Empty weight 18,000 kg (40,000 lb)
Loaded weight 25,000 kg (55,000 lb)
Useful load 7,500 kg (16,000 lb)
Max takeoff weight 37,000 kg (80,000 lb)
Powerplant 2 Saturn-Lyulka 117S (upgraded AL-31) turbofan
Dry thrust 96 kN (9,800 kgf, 22,000 lbf) each
Thrust with afterburner 150 kN (15,500 kgf, 34,000 lbf) each
Maximum speed Mach 2+ at altitude (2500+ km/h, 1,500+ mph)
g-limits (9 g)
Cruise speed 1,300 km/h (800 mph)
Ferry range 5,500 km (3,400 mi)
Service ceiling 20,000 m (65,000 ft)
Rate of climb 350 m/s (70,000 ft/min)
Wing loading 450 kg/m (100 lb/ft)
Runway length requirement 300-400 meters (1,100 ft)
Endurance 3 hrs (200 mins)
Armament - Guns 2 30 mm internal cannon
Hardpoints 8 total, 4 on each side
8 - R-77 missile
Radar N050(?)BRLS AESA/PESA Radar (Enhancement of IRBIS-E) on SU-35
Frequency 3 mm (0.1 in)
Diameter 0.7 m (2 ft )
Targets 32 tracked, 8 engaged
Range 400 km (250 mi)
EPR 3 m (30 ft) at 150 km (100 mi)
RCS 0.01 m at 100 km (50 mi)
Azimuth +/-70, +90/-50
Power 4,000 W



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