Airbus A321LR vs. Tupolev TU-155

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Airbus A321LR versus Tupolev TU-155
44.51 m 146 ft 0 in length 47.63 m 156 ft 3 in
11.76 m 38 ft 7 in height 16.4 m 53 ft 10 in
35.8 m 117 ft 5 in wingspan 64.9 m 212 ft 11 in
CFM International’s LEAP-1A or Pratt & Whitney’s PurePower PW1100G-JM engines 4 × Kuznetsov NK-321 turbofans
Over 33,000 lbs (147 kN) thrust per engine 304.5 kN (68,500 lbf)
66,000 lbs (294 kN) total thrust 1,218 kN (274,000 lbf)
97,000 kg 213,800 lb MTOW 640,000 kg 1,411,000 lb
7,400 km 4,000 nm range 7,000 km 3,780 nm
832 km/h 517 mph cruise speed 850 km/h 528 mph
180-220 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.