Airbus A320-200 vs. Lockheed C-69 Constellation

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Airbus A320-200 versus Lockheed C-69 Constellation
38.7 m 127 ft 0 in length 29.72 m 97 ft 6 in
17.4 m 57 ft 1 in height 6.02 m 19 ft 9 in
35.8 m 117 ft 5 in wingspan 37.49 m 123 ft
Choice between Pratt & Whitney GTF™ and the LEAP-1A from CFM International engines 4 x Wright R-3350 Duplex-Cyclone radial engines
Between 21,000 - 33,000 lbf thrust per engine 2,200 to 3,700 horsepower (1,640 to 2,760 kW)
Between 42,000 - 66,000 lbf total thrust 8,800 to 14,800 horsepower
77,000 kg 169,800 lb MTOW 44,453 kg 98,000 lb
5,700 km 3,078 nm range 5,200 km 2,808 nm
530 mph 853 km/h cruise speed 507 km/h 315 mph
Typically between 140-180 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.