Lockheed U-2 vs. Short C-23 Sherpa
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Lockheed U-2 |
versus |
Short C-23 Sherpa |
19.2 m |
63 ft 0 in |
length |
17.68 m |
58 ft 0 in |
4.8 m |
15 ft 9 in |
height |
6.55 m |
21 ft 6 in |
32 m |
105 ft |
wingspan |
22.76 m |
74 ft 8 in |
1 × General Electric F118-101 |
engines |
2 x Pratt & Whitney Canada PT6A-45R turboprop engines |
17,000 lbf (76 kN) |
thrust per engine |
Approximately 1,200 hp per engine |
17,000 lbf (76 kN) |
total thrust |
Approximately 2,400 hp total |
18,144 kg |
40,000 lb |
MTOW |
7,484 kg |
16,500 lb |
6,090 nm |
11,278 km |
range |
1,048 km |
566 nm |
475 mph |
764 km/h |
cruise speed |
425 km/h |
264 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.