Lockheed Martin F-35 Lightning II vs. Mil Mi-26

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Lockheed Martin F-35 Lightning II versus Mil Mi-26
15.67 m 51 ft 4 in length 40.03 m 131.3 ft
4.33 m 14 ft 2 in height 8.15 m 26.7 ft
10.7 m 35 ft 1 in wingspan
Pratt & Whitney F135 and GE Rolls-Royce Fighter Engine Team F136 engines 2 x Lotarev D-136 turboshaft engines
40,000 lb thrust per engine 8,380 kW
40,000 lb total thrust 16,760 kW
31,800 kg 70,000 lb MTOW 56,000 kg 123,459 lb
1,380 mi 1,200 nm range 800 km 432 nm
520 kt 302 mph cruise speed 255 km/h 158 mph
18,000 pounds of total ordinance 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.