McDonnell-Douglas MD-11 vs. Tupolev TU-155

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McDonnell-Douglas MD-11 versus Tupolev TU-155
61.20 m 200 ft 10 in length 47.63 m 156 ft 3 in
17.6 m 57 ft 9 in height 16.4 m 53 ft 10 in
51.6 m 169 ft 4 in wingspan 64.9 m 212 ft 11 in
3 (General Electric CF6-80C2D1F or Pratt & Whitney PW4460 or PW4462) engines 4 × Kuznetsov NK-321 turbofans
273.1 kN (GE CF6-80C2D1F) or 266.9 kN (PW4460) thrust per engine 304.5 kN (68,500 lbf)
819.3 kN (GE CF6-80C2D1F) or 800.7 kN (PW4460) total thrust 1,218 kN (274,000 lbf)
285,990 kg 630,400 lb MTOW 640,000 kg 1,411,000 lb
13,231 km 7,147 nm range 7,000 km 3,780 nm
961 km/h 597 mph cruise speed 850 km/h 528 mph
Max 410 passengers capacity 350 passengers
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.