Lockheed U-2 vs. Lockheed Martin C-130J Super Hercules
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Lockheed U-2 |
versus |
Lockheed Martin C-130J Super Hercules |
19.2 m |
63 ft 0 in |
length |
34.37 m |
112 ft 9 in |
4.8 m |
15 ft 9 in |
height |
11.86 m |
38 ft 11 in |
32 m |
105 ft |
wingspan |
40.41 m |
132 ft 7 in |
1 × General Electric F118-101 |
engines |
4 x Rolls-Royce AE 2100D3 turboprop engines |
17,000 lbf (76 kN) |
thrust per engine |
Approximately 4,700 hp per engine |
17,000 lbf (76 kN) |
total thrust |
Approximately 18,800 hp total |
18,144 kg |
40,000 lb |
MTOW |
76,610 kg |
168,900 lb |
6,090 nm |
11,278 km |
range |
4,600 km |
2,485 nm |
475 mph |
764 km/h |
cruise speed |
660 km/h |
410 mph |
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capacity |
based on configuration |
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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.