Airbus A300-600F vs. Lockheed C-69 Constellation

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Airbus A300-600F versus Lockheed C-69 Constellation
54.08 m 177 ft 5 in length 29.72 m 97 ft 6 in
17.05 m 55 ft 11 in height 6.02 m 19 ft 9 in
44.84 m 147 ft 1 in wingspan 37.49 m 123 ft
2 x General Electric CF6-80C2A5 turbofan engines engines 4 x Wright R-3350 Duplex-Cyclone radial engines
Approximately 59,000 lbf per engine thrust per engine 2,200 to 3,700 horsepower (1,640 to 2,760 kW)
Approximately 118,000 lbf total total thrust 8,800 to 14,800 horsepower
170,000 kg 374,786 lb MTOW 44,453 kg 98,000 lb
4,830 km 2,608 nm range 5,200 km 2,808 nm
860 km/h 534 mph cruise speed 507 km/h 315 mph
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.