Lockheed U-2 vs. Beechcraft King Air 360
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Lockheed U-2 |
versus |
Beechcraft King Air 360 |
19.2 m |
63 ft 0 in |
length |
13.39 m |
43 ft 11 in |
4.8 m |
15 ft 9 in |
height |
4.35 m |
14 ft 3 in |
32 m |
105 ft |
wingspan |
17.38 m |
57 ft 1 in |
1 × General Electric F118-101 |
engines |
2 x Pratt & Whitney Canada PT6A turboprop |
17,000 lbf (76 kN) |
thrust per engine |
1050 lbs |
17,000 lbf (76 kN) |
total thrust |
2100 lbs |
18,144 kg |
40,000 lb |
MTOW |
14,000 lb |
6,350 kg |
6,090 nm |
11,278 km |
range |
1,720 nm |
3,185 km |
475 mph |
764 km/h |
cruise speed |
310 kts |
193 mph |
|
capacity |
9 |
|
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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.