Lockheed U-2 vs. Short 360
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Lockheed U-2 |
versus |
Short 360 |
19.2 m |
63 ft 0 in |
length |
17.74 m |
58 ft 2 in |
4.8 m |
15 ft 9 in |
height |
6.8 m |
22 ft 4 in |
32 m |
105 ft |
wingspan |
22.72 m |
74 ft 6 in |
1 × General Electric F118-101 |
engines |
2 x Pratt & Whitney Canada PT6A-65R |
17,000 lbf (76 kN) |
thrust per engine |
2,430 lbs |
17,000 lbf (76 kN) |
total thrust |
4,860 lbs |
18,144 kg |
40,000 lb |
MTOW |
28,400 lb |
12,882 kg |
6,090 nm |
11,278 km |
range |
820 nm |
1,519 km |
475 mph |
764 km/h |
cruise speed |
220 kts |
137 mph |
|
capacity |
36 |
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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.