de Havilland Canada DHC-2 Beaver vs. North American F-100 Super Sabre

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de Havilland Canada DHC-2 Beaver versus North American F-100 Super Sabre
13.56 m 44 ft 6 in length 16.46 m 54 ft 2 in
5 m 16 ft 5 in height 4.93 m 16 ft 2 in
16.56 m 54 ft 4 in wingspan 11.84 m 38 ft 1
2 x Armstrong Siddeley Double Mamba turboprop engines engines 1 Pratt & Whitney J57-P-21A
Approximately 3,100 hp (2,312 kW) each thrust per engine 16,000 lb. thrust in afterburner
Approximately 6,200 hp (4,624 kW) total total thrust 16,000 lb. (afterburner)
24,200 lb 10,977 kg MTOW 17,609 kg 38,800 lb
2,535 km 1,369 nm range 2,673 km 1,444 nm
228 mph 367 km/h cruise speed 587 mph 945 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.