Grumman OV-1 Mohawk vs. Mil Mi-26

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Grumman OV-1 Mohawk versus Mil Mi-26
12.52 m 41 ft 1 in length 40.03 m 131.3 ft
3.89 m 12 ft 9 in height 8.15 m 26.7 ft
14.63 m 48 ft wingspan
2 x Lycoming T53 turboprop engines engines 2 x Lotarev D-136 turboshaft engines
Approximately 1,100 hp each thrust per engine 8,380 kW
Approximately 2,200 hp total total thrust 16,760 kW
14,950 lb 6,781 kg MTOW 56,000 kg 123,459 lb
1,690 km 913 nm range 800 km 432 nm
230 mph 370 km/h cruise speed 255 km/h 158 mph
Pilot and observer 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.