McDonnell Douglas F-4 Phantom II vs. Airbus A380-800F

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McDonnell Douglas F-4 Phantom II versus Airbus A380-800F
19.2 m 63 ft 0 in length 72.73 m 238 ft 7 in
5.03 m 16 ft 6 in height 24.09 m 79 ft
11.72 m 38 ft 5 in wingspan 79.75 m 261 ft 8 in
Two General Electric J79s engines 4 x Engine Alliance GP7200 turbofan engines
17,900 lbs thrust per engine 70,000 to 80,000 pounds of thrust (311 to 356 kilonewtons)
35,800 lbs total thrust 280,000 to 320,000 pounds
27,965 kg 61,700 lb MTOW 590,000 kg 1,300,733 lb
3,031 km 1,636 nm range 14,800 km 7,992 nm
Mach 2.2 2,717 km/h cruise speed 903 km/h 561 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.