Lockheed U-2 vs. North American P-51 Mustang
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Lockheed U-2 |
versus |
North American P-51 Mustang |
19.2 m |
63 ft 0 in |
length |
9.83 m |
32 ft 3 in |
4.8 m |
15 ft 9 in |
height |
4.08 m |
13 ft 5 in |
32 m |
105 ft |
wingspan |
11.28 m |
37 ft |
1 × General Electric F118-101 |
engines |
Packard Rolls Royce Merlin V-1650-7 |
17,000 lbf (76 kN) |
thrust per engine |
1,490 horsepower at 3,000 rpm and 1,720 horsepower at war emergency power (WEP) |
17,000 lbf (76 kN) |
total thrust |
1,490 horsepower at 3,000 rpm and 1,720 horsepower at war emergency power (WEP) |
18,144 kg |
40,000 lb |
MTOW |
5,489 kg |
12,100 lb |
6,090 nm |
11,278 km |
range |
2,200 km |
1,188 nm |
475 mph |
764 km/h |
cruise speed |
325 mph |
525 km/h |
|
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.