McDonnell Douglas F-4 Phantom II vs. Mil Mi-26

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McDonnell Douglas F-4 Phantom II versus Mil Mi-26
19.2 m 63 ft 0 in length 40.03 m 131.3 ft
5.03 m 16 ft 6 in height 8.15 m 26.7 ft
11.72 m 38 ft 5 in wingspan
Two General Electric J79s engines 2 x Lotarev D-136 turboshaft engines
17,900 lbs thrust per engine 8,380 kW
35,800 lbs total thrust 16,760 kW
27,965 kg 61,700 lb MTOW 56,000 kg 123,459 lb
3,031 km 1,636 nm range 800 km 432 nm
Mach 2.2 2,717 km/h cruise speed 255 km/h 158 mph
Up to 16,000 lbs of externally carried ordnance 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.