Lockheed U-2 vs. Mil Mi-26

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Lockheed U-2 versus Mil Mi-26
19.2 m 63 ft 0 in length 40.03 m 131.3 ft
4.8 m 15 ft 9 in height 8.15 m 26.7 ft
32 m 105 ft wingspan
1 × General Electric F118-101 engines 2 x Lotarev D-136 turboshaft engines
17,000 lbf (76 kN) thrust per engine 8,380 kW
17,000 lbf (76 kN) total thrust 16,760 kW
18,144 kg 40,000 lb MTOW 56,000 kg 123,459 lb
6,090 nm 11,278 km range 800 km 432 nm
475 mph 764 km/h cruise speed 255 km/h 158 mph
capacity Up to 90 passengers
rotor diameter 32.00 m 105 ft 0 in
rate of climb 8 m/s 1,574 ft/min
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.