McDonnell-Douglas MD-11 vs. Concorde

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McDonnell-Douglas MD-11 versus Concorde
61.20 m 200 ft 10 in length 61.66 m 202 ft 4 in
17.6 m 57 ft 9 in height 11.4 m 37 ft 5 in
51.6 m 169 ft 4 in wingspan 25.56 m 83 ft 1
3 (General Electric CF6-80C2D1F or Pratt & Whitney PW4460 or PW4462) engines 4 Rolls Royce/Snecma Olympus 593 turbo jet engines
273.1 kN (GE CF6-80C2D1F) or 266.9 kN (PW4460) thrust per engine 18.7 tons (180 kN)
819.3 kN (GE CF6-80C2D1F) or 800.7 kN (PW4460) total thrust 74.8 tons (720 kN)
285,990 kg 630,400 lb MTOW 185,000 kg 408,000 lb
13,231 km 7,147 nm range 6,580 km 3,554 nm
961 km/h 597 mph cruise speed Mach 2.04 2,179 km/h
Max 410 passengers capacity 92–120 passengers
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.