Lockheed P-2 Neptune vs. Mil Mi-26

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Lockheed P-2 Neptune versus Mil Mi-26
30.17 m 99 ft 0 in length 40.03 m 131.3 ft
10.15 m 33 ft 4 in height 8.15 m 26.7 ft
33.53 m 110 ft wingspan
2 x Wright R-3350 radial engines engines 2 x Lotarev D-136 turboshaft engines
Approximately 3,700 hp thrust per engine 8,380 kW
Approximately 7,400 hp total thrust 16,760 kW
27,216 kg 60,000 lb MTOW 56,000 kg 123,459 lb
7,885 km 4,259 nm range 800 km 432 nm
300 mph 483 km/h cruise speed 255 km/h 158 mph
based on configuration 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.