Crew: six
Capacity: Max 100,000 kg payload (T-6 military jet fuel)[34]
Length: 46.59 m (152 ft 10 in)
Wingspan: 50.5 m (165 ft 8 in)
Height: 14.76 m (48 ft 5 in)
Wing area: 300 m2 (3,200 sq ft)
Empty weight: 72,000 kg (158,733 lb)
Max takeoff weight: 210,000 kg (462,971 lb)
Special equipment: 3 x UPAZ-1M 'Sakhalin', (Unifitsirovaniy Podvesnoy Agregat Zaprahvki;— standardised suspended refuelling unit), refuelling pods; Two on pylons under the outer wings, and the third on the port side of the rear fuselage.
Fuel transfer rate: 900 to 2,200 liters/min
Powerplant: 4 × Aviadvigatel D-30 KP turbofan engines, 118 kN (27,000 lbf) thrust each
Performance
Maximum speed: 850 km/h (528 mph; 459 kn)
Range: 7,300 km (4,536 mi; 3,942 nmi)
Service ceiling: 12,000 m (39,000 ft)
Thrust/weight: 0.23
Capacity: Max 100,000 kg payload (T-6 military jet fuel)[34]
Length: 46.59 m (152 ft 10 in)
Wingspan: 50.5 m (165 ft 8 in)
Height: 14.76 m (48 ft 5 in)
Wing area: 300 m2 (3,200 sq ft)
Empty weight: 72,000 kg (158,733 lb)
Max takeoff weight: 210,000 kg (462,971 lb)
Special equipment: 3 x UPAZ-1M 'Sakhalin', (Unifitsirovaniy Podvesnoy Agregat Zaprahvki;— standardised suspended refuelling unit), refuelling pods; Two on pylons under the outer wings, and the third on the port side of the rear fuselage.
Fuel transfer rate: 900 to 2,200 liters/min
Powerplant: 4 × Aviadvigatel D-30 KP turbofan engines, 118 kN (27,000 lbf) thrust each
Performance
Maximum speed: 850 km/h (528 mph; 459 kn)
Range: 7,300 km (4,536 mi; 3,942 nmi)
Service ceiling: 12,000 m (39,000 ft)
Thrust/weight: 0.23