Airbus A310-300 vs. Concorde

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Airbus A310-300 versus Concorde
46.66 m 153 ft 1 in length 61.66 m 202 ft 4 in
15.8 m 51 ft 10 in height 11.4 m 37 ft 5 in
43.9 m 144 ft wingspan 25.56 m 83 ft 1
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines 4 Rolls Royce/Snecma Olympus 593 turbo jet engines
52,000 lb thrust per engine 18.7 tons (180 kN)
104,000 lb total thrust 74.8 tons (720 kN)
148,768 kg 328,000 lb MTOW 185,000 kg 408,000 lb
8,050 km 4,348 nm range 6,580 km 3,554 nm
482 knots 279 mph cruise speed Mach 2.04 2,179 km/h
190-230 passengers capacity 92–120 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.