Lockheed U-2 vs. North American B-25 Mitchell
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Lockheed U-2 |
versus |
North American B-25 Mitchell |
19.2 m |
63 ft 0 in |
length |
16.15 m |
53 ft 0 in |
4.8 m |
15 ft 9 in |
height |
5 m |
16 ft 4 in |
32 m |
105 ft |
wingspan |
20.58 m |
67 ft 6 in |
1 × General Electric F118-101 |
engines |
2 x Wright R-2600-92 Twin Cyclone |
17,000 lbf (76 kN) |
thrust per engine |
1,700 horsepower |
17,000 lbf (76 kN) |
total thrust |
3,400 horsepower |
18,144 kg |
40,000 lb |
MTOW |
7,484 kg |
16,500 lb |
6,090 nm |
11,278 km |
range |
1,350 mi |
1,175 nm |
475 mph |
764 km/h |
cruise speed |
233 MPH |
375 km/h |
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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.