de Havilland Canada DHC-2 Beaver vs. North American B-25 Mitchell

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de Havilland Canada DHC-2 Beaver versus North American B-25 Mitchell
13.56 m 44 ft 6 in length 16.15 m 53 ft 0 in
5 m 16 ft 5 in height 5 m 16 ft 4 in
16.56 m 54 ft 4 in wingspan 20.58 m 67 ft 6 in
2 x Armstrong Siddeley Double Mamba turboprop engines engines 2 x Wright R-2600-92 Twin Cyclone
Approximately 3,100 hp (2,312 kW) each thrust per engine 1,700 horsepower
Approximately 6,200 hp (4,624 kW) total total thrust 3,400 horsepower
24,200 lb 10,977 kg MTOW 7,484 kg 16,500 lb
2,535 km 1,369 nm range 1,350 mi 1,175 nm
228 mph 367 km/h cruise speed 233 MPH 375 km/h
Pilot and Observer, plus various configurations for reconnaissance, anti-submarine warfare, and aerial refueling capacity
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.