Concorde vs. de Havilland Canada DHC-2 Beaver

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Concorde versus de Havilland Canada DHC-2 Beaver
61.66 m 202 ft 4 in length 13.56 m 44 ft 6 in
11.4 m 37 ft 5 in height 5 m 16 ft 5 in
25.56 m 83 ft 1 wingspan 16.56 m 54 ft 4 in
4 Rolls Royce/Snecma Olympus 593 turbo jet engines engines 2 x Armstrong Siddeley Double Mamba turboprop engines
18.7 tons (180 kN) thrust per engine Approximately 3,100 hp (2,312 kW) each
74.8 tons (720 kN) total thrust Approximately 6,200 hp (4,624 kW) total
185,000 kg 408,000 lb MTOW 24,200 lb 10,977 kg
6,580 km 3,554 nm range 2,535 km 1,369 nm
Mach 2.04 2,179 km/h cruise speed 228 mph 367 km/h
92–120 passengers capacity Pilot and Observer, plus various configurations for reconnaissance, anti-submarine warfare, and aerial refueling
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.