de Havilland Canada DHC-2 Beaver vs. Mikoyan-Gurevich MiG-21

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de Havilland Canada DHC-2 Beaver versus Mikoyan-Gurevich MiG-21
13.56 m 44 ft 6 in length 15.76 m 51 ft 8 in
5 m 16 ft 5 in height 4.11 m 13 ft 6 in
16.56 m 54 ft 4 in wingspan 7.16 m 23 ft 6 in
2 x Armstrong Siddeley Double Mamba turboprop engines engines 1 x Tumansky R-25-300 afterburning turbojet
Approximately 3,100 hp (2,312 kW) each thrust per engine 15,640 lb with reheat
Approximately 6,200 hp (4,624 kW) total total thrust 15,640 lb
24,200 lb 10,977 kg MTOW 7,958 kg 17,500 lb
2,535 km 1,369 nm range 1,161 km 627 nm
228 mph 367 km/h cruise speed 1,386 mph 2,230 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.