Lockheed U-2 vs. Aero Commander 500B
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Lockheed U-2 |
versus |
Aero Commander 500B |
19.2 m |
63 ft 0 in |
length |
10.44 m |
34 ft 3 in |
4.8 m |
15 ft 9 in |
height |
3.23 m |
10 ft 7 in |
32 m |
105 ft |
wingspan |
15.02 m |
49 ft 3 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 |
5,100 lb |
2,313 kg |
6,090 nm |
11,278 km |
range |
1,100 nm |
2,037 km |
475 mph |
764 km/h |
cruise speed |
216 kts |
134 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.