McDonnell Douglas A-4 Skyhawk vs. Mil Mi-26

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McDonnell Douglas A-4 Skyhawk versus Mil Mi-26
12.19 m 40 ft 0 in length 40.03 m 131.3 ft
4.57 m 15 ft height 8.15 m 26.7 ft
8.08 m 26 ft 6 in wingspan
1x Pratt & Whitney J52-P-6A Jet engines 2 x Lotarev D-136 turboshaft engines
8,500 pound-force thrust per engine 8,380 kW
8,500 pound-force total thrust 16,760 kW
11,113 kg 24,500 lb MTOW 56,000 kg 123,459 lb
3,222 km 1,739 nm range 800 km 432 nm
586 kts 364 mph cruise speed 255 km/h 158 mph
Up to 9,155 pounds of weapons on 5 hardpoints 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.