McDonnell-Douglas DC-9-30 vs. Lockheed U-2

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McDonnell-Douglas DC-9-30 versus Lockheed U-2
36.36 m 119 ft 3 in length 19.2 m 63 ft 0 in
8.5 m 27 ft 11 in height 4.8 m 15 ft 9 in
28.44 m 93 ft 4 in wingspan 32 m 105 ft
2x Pratt & Whitney JT8D engines 1 × General Electric F118-101
15,000 pound-force thrust per engine 17,000 lbf (76 kN)
30,000 pound-force (2 engines) total thrust 17,000 lbf (76 kN)
54,885 kg 121,000 lb MTOW 18,144 kg 40,000 lb
2,632 km 1,422 nm range 6,090 nm 11,278 km
898 km/h 558 mph cruise speed 475 mph 764 km/h
Up to 139 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.