McDonnell-Douglas MD-11 vs. North American B-25 Mitchell

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McDonnell-Douglas MD-11 versus North American B-25 Mitchell
61.20 m 200 ft 10 in length 16.15 m 53 ft 0 in
17.6 m 57 ft 9 in height 5 m 16 ft 4 in
51.6 m 169 ft 4 in wingspan 20.58 m 67 ft 6 in
3 (General Electric CF6-80C2D1F or Pratt & Whitney PW4460 or PW4462) engines 2 x Wright R-2600-92 Twin Cyclone
273.1 kN (GE CF6-80C2D1F) or 266.9 kN (PW4460) thrust per engine 1,700 horsepower
819.3 kN (GE CF6-80C2D1F) or 800.7 kN (PW4460) total thrust 3,400 horsepower
285,990 kg 630,400 lb MTOW 7,484 kg 16,500 lb
13,231 km 7,147 nm range 1,350 mi 1,175 nm
961 km/h 597 mph cruise speed 233 MPH 375 km/h
Max 410 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.