McDonnell Douglas F-4 Phantom II vs. Douglas C-54 Skymaster
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McDonnell Douglas F-4 Phantom II |
versus |
Douglas C-54 Skymaster |
19.2 m |
63 ft 0 in |
length |
28.60 m |
93 ft 10 in |
5.03 m |
16 ft 6 in |
height |
8.38 m |
27 ft 6 in |
11.72 m |
38 ft 5 in |
wingspan |
35.81 m |
117 ft 6 in |
Two General Electric J79s |
engines |
4 x Pratt & Whitney R-2000 Twin Wasp radial engines |
17,900 lbs |
thrust per engine |
1,200 to 1,450 horsepower (895 to 1,080 kW) |
35,800 lbs |
total thrust |
4,800 to 5,800 horsepower |
27,965 kg |
61,700 lb |
MTOW |
29,484 kg |
65,000 lb |
3,031 km |
1,636 nm |
range |
6,500 km |
3,510 nm |
Mach 2.2 |
2,717 km/h |
cruise speed |
340 km/h |
211 mph |
Up to 16,000 lbs of externally carried ordnance |
capacity |
Up to 50 passengers or 28,500 lb cargo |
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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.