Concorde vs. North American B-25 Mitchell

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Concorde versus North American B-25 Mitchell
61.66 m 202 ft 4 in length 16.15 m 53 ft 0 in
11.4 m 37 ft 5 in height 5 m 16 ft 4 in
25.56 m 83 ft 1 wingspan 20.58 m 67 ft 6 in
4 Rolls Royce/Snecma Olympus 593 turbo jet engines engines 2 x Wright R-2600-92 Twin Cyclone
18.7 tons (180 kN) thrust per engine 1,700 horsepower
74.8 tons (720 kN) total thrust 3,400 horsepower
185,000 kg 408,000 lb MTOW 7,484 kg 16,500 lb
6,580 km 3,554 nm range 1,350 mi 1,175 nm
Mach 2.04 2,179 km/h cruise speed 233 MPH 375 km/h
92–120 passengers 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.