Douglas DC-8-61 vs. Lockheed U-2

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Douglas DC-8-61 versus Lockheed U-2
57.0 m 187 ft 0 in length 19.2 m 63 ft 0 in
13.1 m 43 ft height 4.8 m 15 ft 9 in
45.24 m 148 ft 5 in wingspan 32 m 105 ft
4x P&W JT3D-3B Turbofan engines 1 × General Electric F118-101
18,000 pound-force thrust per engine 17,000 lbf (76 kN)
72,000 pound-force total thrust 17,000 lbf (76 kN)
147,400 kg 325,000 lb MTOW 18,144 kg 40,000 lb
3,200 nm 5,926 km range 6,090 nm 11,278 km
483 knots 282 mph cruise speed 475 mph 764 km/h
180 to 220 passengers in a mixed-class seating 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.