McDonnell-Douglas MD-11 vs. Lockheed U-2

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McDonnell-Douglas MD-11 versus Lockheed U-2
61.20 m 200 ft 10 in length 19.2 m 63 ft 0 in
17.6 m 57 ft 9 in height 4.8 m 15 ft 9 in
51.6 m 169 ft 4 in wingspan 32 m 105 ft
3 (General Electric CF6-80C2D1F or Pratt & Whitney PW4460 or PW4462) engines 1 × General Electric F118-101
273.1 kN (GE CF6-80C2D1F) or 266.9 kN (PW4460) thrust per engine 17,000 lbf (76 kN)
819.3 kN (GE CF6-80C2D1F) or 800.7 kN (PW4460) total thrust 17,000 lbf (76 kN)
285,990 kg 630,400 lb MTOW 18,144 kg 40,000 lb
13,231 km 7,147 nm range 6,090 nm 11,278 km
961 km/h 597 mph cruise speed 475 mph 764 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.