Lockheed U-2 vs. de Havilland Canada DHC-3 Otter
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here.
| Lockheed U-2 |
versus |
de Havilland Canada DHC-3 Otter |
| 19.2 m |
63 ft 0 in |
length |
10.52 m |
34 ft 6 in |
| 4.8 m |
15 ft 9 in |
height |
3.84 m |
12 ft 7 in |
| 32 m |
105 ft |
wingspan |
17.68 m |
58 ft |
| 1 × General Electric F118-101 |
engines |
1 x Pratt & Whitney R-1340 radial engine |
| 17,000 lbf (76 kN) |
thrust per engine |
400 to 600 horsepower (298 to 447 kW) |
| 17,000 lbf (76 kN) |
total thrust |
400 to 600 horsepower (298 to 447 kW) |
| 18,144 kg |
40,000 lb |
MTOW |
5,670 kg |
12,500 lb |
| 6,090 nm |
11,278 km |
range |
1,296 km |
700 nm |
| 475 mph |
764 km/h |
cruise speed |
215 km/h |
134 mph |
|
capacity |
10-11 passengers |
|
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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.
