Lockheed P-2 Neptune vs. Lockheed U-2
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Lockheed P-2 Neptune |
versus |
Lockheed U-2 |
30.17 m |
99 ft 0 in |
length |
19.2 m |
63 ft 0 in |
10.15 m |
33 ft 4 in |
height |
4.8 m |
15 ft 9 in |
33.53 m |
110 ft |
wingspan |
32 m |
105 ft |
2 x Wright R-3350 radial engines |
engines |
1 × General Electric F118-101 |
Approximately 3,700 hp |
thrust per engine |
17,000 lbf (76 kN) |
Approximately 7,400 hp |
total thrust |
17,000 lbf (76 kN) |
27,216 kg |
60,000 lb |
MTOW |
18,144 kg |
40,000 lb |
7,885 km |
4,259 nm |
range |
6,090 nm |
11,278 km |
300 mph |
483 km/h |
cruise speed |
475 mph |
764 km/h |
based on configuration |
capacity |
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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.