Lockheed U-2 vs. de Havilland Canada DHC-6 Twin Otter
... or view the full comparison list
here.
| Lockheed U-2 |
versus |
de Havilland Canada DHC-6 Twin Otter |
| 19.2 m |
63 ft 0 in |
length |
15.32 m |
50 ft 3 in |
| 4.8 m |
15 ft 9 in |
height |
5.94 m |
19 ft 6 in |
| 32 m |
105 ft |
wingspan |
19.81 m |
65 ft |
| 1 × General Electric F118-101 |
engines |
2 x Pratt & Whitney Canada PT6A-27 turboprop engines |
| 17,000 lbf (76 kN) |
thrust per engine |
550 to 750 shaft horsepower (410 to 560 kW) |
| 17,000 lbf (76 kN) |
total thrust |
1100 to 1500 shaft horsepower |
| 18,144 kg |
40,000 lb |
MTOW |
5,670 kg |
12,500 lb |
| 6,090 nm |
11,278 km |
range |
1,389 km |
750 nm |
| 475 mph |
764 km/h |
cruise speed |
280 km/h |
174 mph |
|
capacity |
19 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.
