Airbus A350-1000 vs. McDonnell Douglas F-4 Phantom II
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Airbus A350-1000 |
versus |
McDonnell Douglas F-4 Phantom II |
73.79 m |
242 ft 1 in |
length |
19.2 m |
63 ft 0 in |
17.08 m |
56 ft |
height |
5.03 m |
16 ft 6 in |
64.75 m |
212 ft 5 in |
wingspan |
11.72 m |
38 ft 5 in |
2 Trent XWB-97 turbofan engines |
engines |
Two General Electric J79s |
97,000 lb |
thrust per engine |
17,900 lbs |
194,000 lb |
total thrust |
35,800 lbs |
319,000 kg |
703,300 lb |
MTOW |
27,965 kg |
61,700 lb |
16,100 km |
8,695 nm |
range |
3,031 km |
1,636 nm |
1,099 km/h |
683 mph |
cruise speed |
Mach 2.2 |
2,717 km/h |
350 to 410 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.