Airbus A340-600 vs. McDonnell Douglas F-4 Phantom II
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| Airbus A340-600 |
versus |
McDonnell Douglas F-4 Phantom II |
| 75.36 m |
247 ft 3 in |
length |
19.2 m |
63 ft 0 in |
| 17.93 m |
58 ft 10 in |
height |
5.03 m |
16 ft 6 in |
| 63.45 m |
208 ft 2 in |
wingspan |
11.72 m |
38 ft 5 in |
| 4 x Rolls-Royce Trent 556 |
engines |
Two General Electric J79s |
| 56,000 lbs |
thrust per engine |
17,900 lbs |
| 224,000 lbs |
total thrust |
35,800 lbs |
| 380,000 kg |
837,800 lb |
MTOW |
27,965 kg |
61,700 lb |
| 14,450 km |
7,804 nm |
range |
3,031 km |
1,636 nm |
| 890 km/h |
553 mph |
cruise speed |
Mach 2.2 |
2,717 km/h |
| 320-370 |
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.
