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

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Airbus A380-800 versus McDonnell Douglas F-4 Phantom II
72.72 m 238 ft 7 in length 19.2 m 63 ft 0 in
24.09 m 79 ft height 5.03 m 16 ft 6 in
79.75 m 261 ft 8 in wingspan 11.72 m 38 ft 5 in
4 engines Two General Electric J79s
70000lbs thrust per engine 17,900 lbs
280000lbs total thrust 35,800 lbs
560,000 kg 1,234,600 lb MTOW 27,965 kg 61,700 lb
14,800 km 8,000 nm range 3,031 km 1,636 nm
1,050 km/h 652 mph cruise speed Mach 2.2 2,717 km/h
525-853 passengers capacity Up to 16,000 lbs of externally carried ordnance
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.