Airbus A350-800 vs. McDonnell Douglas F-4 Phantom II
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Airbus A350-800 |
versus |
McDonnell Douglas F-4 Phantom II |
60.54 m |
198 ft 7 in |
length |
19.2 m |
63 ft 0 in |
17.05 m |
55 ft 11 in |
height |
5.03 m |
16 ft 6 in |
64.7 m |
212 ft 5 in |
wingspan |
11.72 m |
38 ft 5 in |
2 Turbofans (wing mounted) |
engines |
Two General Electric J79s |
75,760 lb |
thrust per engine |
17,900 lbs |
151,520 lb |
total thrust |
35,800 lbs |
283,000 kg |
623,900 lb |
MTOW |
27,965 kg |
61,700 lb |
11,708 km |
6,319 nm |
range |
3,031 km |
1,636 nm |
552 mph |
888 km/h |
cruise speed |
Mach 2.2 |
2,717 km/h |
Typically carries 300 to 350 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.