Airbus A310-300 vs. Tu-144

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Airbus A310-300 versus Tu-144
46.66 m 153 ft 1 in length 65.7 m 215 ft 6 in
15.8 m 51 ft 10 in height 12.55 m 41 ft 2 in
43.9 m 144 ft wingspan 28.8 m 94 ft 6 in
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines 4 Kolesov RD-36-51 or Kuznetsov NK-144 engines
52,000 lb thrust per engine 44,000 pounds (full afterburner)
104,000 lb total thrust 176,000 pounds (full afterburner)
148,768 kg 328,000 lb MTOW 207,000 kg 456,300 lb
8,050 km 4,348 nm range 3,500 nm 6,482 km
482 knots 279 mph cruise speed Mach 2.17 2680 km/h
190-230 passengers capacity 150 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.