Lockheed U-2 vs. Cessna 172
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Lockheed U-2 |
versus |
Cessna 172 |
19.2 m |
63 ft 0 in |
length |
8.28 m |
27 ft 2 in |
4.8 m |
15 ft 9 in |
height |
2.72 m |
8 ft 11 in |
32 m |
105 ft |
wingspan |
11 m |
36 ft 1 in |
1 × General Electric F118-101 |
engines |
1 x Lycoming IO-360-L2A flat-4 piston engine |
17,000 lbf (76 kN) |
thrust per engine |
180 to 200 horsepower (134 to 149 kW) |
17,000 lbf (76 kN) |
total thrust |
180 to 200 horsepower (134 to 149 kW) |
18,144 kg |
40,000 lb |
MTOW |
1,040 kg |
2,293 lb |
6,090 nm |
11,278 km |
range |
1,056 km |
570 nm |
475 mph |
764 km/h |
cruise speed |
226 km/h |
140 mph |
|
capacity |
4 |
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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.