Crew: 1

    Length: 19.8 m (65 ft)

    Wingspan: 13.95 m (45 ft 10 in)

    Height: 4.74 m (15 ft 7 in)

    Empty weight: 18,000 kg (39,680 lb)

    Loaded weight: 25,000 kg (55,115 lb) typical mission weight, 29,270 kg

    Max. takeoff weight: 35,000 kg (77,160 lb)

       Powerplant: 2 × Saturn AL-41F1 for initial production, izdeliye 30 for later production[102] turbofans

        Dry thrust: 93.1 kN / 107 kN (21,000 lbf / 24,054 lbf) each

        Thrust with afterburner: 147 kN / 176 kN (33,067 lbf / 39,566

Performance

Maximum speed:

    At altitude: Mach 2 (2,140 km/h; 1,320 mph

    Supercruise: Mach 1.6 (1,700 km/h; 1,060 mph)

Range: 3,500 km (2,175 mi; 1,890 nmi) subsonic

    1,500 km (930 mi; 810 nmi) supersonic

Service ceiling: 20,000 m (65,000 ft)

Thrust/weight:

    AL-41F1: 1.02 (1.19 at typical mission weight)

Armament

Guns: 1 × 30 mm Gryazev-Shipunov GSh-30-1 autocannon in right LEVCON root

Hardpoints: 12 hardpoints (6 × internal, 6 × external)  and provisions to carry combinations

Sukhoi: Sukhoi T-50/SU-57 Pakfa

General characteristics :

YEAR: 2010

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