de Havilland Canada DHC-2 Beaver vs. Lockheed C-69 Constellation

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de Havilland Canada DHC-2 Beaver versus Lockheed C-69 Constellation
13.56 m 44 ft 6 in length 29.72 m 97 ft 6 in
5 m 16 ft 5 in height 6.02 m 19 ft 9 in
16.56 m 54 ft 4 in wingspan 37.49 m 123 ft
2 x Armstrong Siddeley Double Mamba turboprop engines engines 4 x Wright R-3350 Duplex-Cyclone radial engines
Approximately 3,100 hp (2,312 kW) each thrust per engine 2,200 to 3,700 horsepower (1,640 to 2,760 kW)
Approximately 6,200 hp (4,624 kW) total total thrust 8,800 to 14,800 horsepower
24,200 lb 10,977 kg MTOW 44,453 kg 98,000 lb
2,535 km 1,369 nm range 5,200 km 2,808 nm
228 mph 367 km/h cruise speed 507 km/h 315 mph
Pilot and Observer, plus various configurations for reconnaissance, anti-submarine warfare, and aerial refueling 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.