McDonnell-Douglas DC-10-30 vs. Lockheed U-2

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McDonnell-Douglas DC-10-30 versus Lockheed U-2
55.35 m 181 ft 8 in length 19.2 m 63 ft 0 in
17.8 m 58 ft 5 in height 4.8 m 15 ft 9 in
50.39 m 165 ft 4 in wingspan 32 m 105 ft
3x GE CF6-50C Turbofan engines 1 × General Electric F118-101
54,000 lbf thrust per engine 17,000 lbf (76 kN)
162,000 lbf total thrust 17,000 lbf (76 kN)
251,744 kg 555,000 lb MTOW 18,144 kg 40,000 lb
9,630 km 5,200 nm range 6,090 nm 11,278 km
507 knots 939 km/h cruise speed 475 mph 764 km/h
Up to 380 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.