McDonnell Douglas F-4 Phantom II vs. North American P-51 Mustang
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McDonnell Douglas F-4 Phantom II |
versus |
North American P-51 Mustang |
19.2 m |
63 ft 0 in |
length |
9.83 m |
32 ft 3 in |
5.03 m |
16 ft 6 in |
height |
4.08 m |
13 ft 5 in |
11.72 m |
38 ft 5 in |
wingspan |
11.28 m |
37 ft |
Two General Electric J79s |
engines |
Packard Rolls Royce Merlin V-1650-7 |
17,900 lbs |
thrust per engine |
1,490 horsepower at 3,000 rpm and 1,720 horsepower at war emergency power (WEP) |
35,800 lbs |
total thrust |
1,490 horsepower at 3,000 rpm and 1,720 horsepower at war emergency power (WEP) |
27,965 kg |
61,700 lb |
MTOW |
5,489 kg |
12,100 lb |
3,031 km |
1,636 nm |
range |
2,200 km |
1,188 nm |
Mach 2.2 |
2,717 km/h |
cruise speed |
325 mph |
525 km/h |
Up to 16,000 lbs of externally carried ordnance |
capacity |
2,000 pounds of bombs, or ten 5-inch rockets |
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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.