Airbus A310-300 vs. Lockheed C-69 Constellation

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Airbus A310-300 versus Lockheed C-69 Constellation
46.66 m 153 ft 1 in length 29.72 m 97 ft 6 in
15.8 m 51 ft 10 in height 6.02 m 19 ft 9 in
43.9 m 144 ft wingspan 37.49 m 123 ft
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines 4 x Wright R-3350 Duplex-Cyclone radial engines
52,000 lb thrust per engine 2,200 to 3,700 horsepower (1,640 to 2,760 kW)
104,000 lb total thrust 8,800 to 14,800 horsepower
148,768 kg 328,000 lb MTOW 44,453 kg 98,000 lb
8,050 km 4,348 nm range 5,200 km 2,808 nm
482 knots 279 mph cruise speed 507 km/h 315 mph
190-230 passengers capacity Up to 109 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.