Lockheed U-2 vs. Aero Commander 500S
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Lockheed U-2 |
versus |
Aero Commander 500S |
19.2 m |
63 ft 0 in |
length |
10.46 m |
34 ft 4 in |
4.8 m |
15 ft 9 in |
height |
3.63 m |
11 ft 11 in |
32 m |
105 ft |
wingspan |
13.52 m |
44 ft 4 in |
1 × General Electric F118-101 |
engines |
2 x Lycoming IO-540 |
17,000 lbf (76 kN) |
thrust per engine |
380 lbs |
17,000 lbf (76 kN) |
total thrust |
760 lbs |
18,144 kg |
40,000 lb |
MTOW |
11,500 lb |
5,216 kg |
6,090 nm |
11,278 km |
range |
1,350 nm |
2,500 km |
475 mph |
764 km/h |
cruise speed |
230 kts |
143 mph |
|
capacity |
Up to 4 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.