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 |
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rotor diameter |
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rate of climb |
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Please note that these values are indicative and actual values can vary based on specific engine models and configurations.