McDonnell Douglas F-4 Phantom II vs. Antonov An-124 Ruslan

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McDonnell Douglas F-4 Phantom II versus Antonov An-124 Ruslan
19.2 m 63 ft 0 in length 69.10 m 226 ft 9 in
5.03 m 16 ft 6 in height 20.78 m 68 ft 2 in
11.72 m 38 ft 5 in wingspan 73.3 m 240 ft 6 in
Two General Electric J79s engines 4 x Ivchenko Progress D-18T turbofan engines
17,900 lbs thrust per engine Approximately 51,590 lbf
35,800 lbs total thrust Approximately 206,360 lbf
27,965 kg 61,700 lb MTOW 405,000 kg 893,000 lb
3,031 km 1,636 nm range 3,700 km 1,998 nm
Mach 2.2 2,717 km/h cruise speed 800 km/h 497 mph
Up to 16,000 lbs of externally carried ordnance capacity
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.