McDonnell Douglas F-4 Phantom II vs. Antonov An-225 Mriya

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McDonnell Douglas F-4 Phantom II versus Antonov An-225 Mriya
19.2 m 63 ft 0 in length 84.0 m 275 ft 7 in
5.03 m 16 ft 6 in height 18.1 m 59 ft 5 in
11.72 m 38 ft 5 in wingspan 88.4 m 290 ft 2 in
Two General Electric J79s engines 6 x Ivchenko Progress D-18T turbofan engines
17,900 lbs thrust per engine Approximately 23,400 kgf per engine
35,800 lbs total thrust Approximately 140,400 kgf total
27,965 kg 61,700 lb MTOW 640,000 kg 1,411,200 lb
3,031 km 1,636 nm range 15,400 km 8,315 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 based on configuration
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.