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Description
General characteristics

    Crew: 2
    Length: 30.06 m (98 ft 7 in)
    Wingspan: 17.53 m (57 ft 6 in)
    Height: 7.15 m (23 ft 5 in)
    Wing area: 96.94 m2 (1,043.5 sq ft)
    Empty weight: 24,500 kg (54,013 lb)
    Gross weight: 40,000 kg (88,185 lb)
    Max takeoff weight: 43,000–43,700 kg (94,799–96,342 lb)
    Fuel capacity: 13,600 kg (29,983 lb) maximum (estimated)
    Powerplant: 2 × Lyulka AL-7F-2 afterburning turbojet engines, 72.8 kN (16,400 lbf) thrust each dry, 99.1 kN (22,300 lbf) with afterburner

Performance

    Maximum speed: 1,665 km/h (1,035 mph, 899 kn) / M1.5 armed

                1,929 km/h (1,199 mph; 1,042 kn) un-armed

    Range: 1,560 km (970 mi, 840 nmi)
    Endurance: >3 hours
    Service ceiling: 15,600 m (51,200 ft)
    Absolute ceiling: 20,000 m (66,000 ft)
    g limits: +2.5

Armament

    Hardpoints: 4
    Missiles: 4 × Bisnovat R-4 air-to-air missiles (usually 2 × radar-guided R-4R and 2 × infrared-homing R-4T); other armament or tanks not used

Description
General characteristics

    Crew: 2
    Length: 30.06 m (98 ft 7 in)
    Wingspan: 17.53 m (57 ft 6 in)
    Height: 7.15 m (23 ft 5 in)
    Wing area: 96.94 m2 (1,043.5 sq ft)
    Empty weight: 24,500 kg (54,013 lb)
    Gross weight: 40,000 kg (88,185 lb)
    Max takeoff weight: 43,000–43,700 kg (94,799–96,342 lb)
    Fuel capacity: 13,600 kg (29,983 lb) maximum (estimated)
    Powerplant: 2 × Lyulka AL-7F-2 afterburning turbojet engines, 72.8 kN (16,400 lbf) thrust each dry, 99.1 kN (22,300 lbf) with afterburner

Performance

    Maximum speed: 1,665 km/h (1,035 mph, 899 kn) / M1.5 armed

                1,929 km/h (1,199 mph; 1,042 kn) un-armed

    Range: 1,560 km (970 mi, 840 nmi)
    Endurance: >3 hours
    Service ceiling: 15,600 m (51,200 ft)
    Absolute ceiling: 20,000 m (66,000 ft)
    g limits: +2.5

Armament

    Hardpoints: 4
    Missiles: 4 × Bisnovat R-4 air-to-air missiles (usually 2 × radar-guided R-4R and 2 × infrared-homing R-4T); other armament or tanks not used