Lockheed U-2 vs. Polikarpov I-16
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Lockheed U-2 |
versus |
Polikarpov I-16 |
19.2 m |
63 ft 0 in |
length |
6.13 m |
20 ft 1 in |
4.8 m |
15 ft 9 in |
height |
3.25 m |
10 ft 8 in |
32 m |
105 ft |
wingspan |
9 m |
29 ft 6 in |
1 × General Electric F118-101 |
engines |
1x Shvetsov M-25 radial engine |
17,000 lbf (76 kN) |
thrust per engine |
1000 hp |
17,000 lbf (76 kN) |
total thrust |
1000 hp |
18,144 kg |
40,000 lb |
MTOW |
2,060 kg |
4,540 lb |
6,090 nm |
11,278 km |
range |
248 mi |
216 nm |
475 mph |
764 km/h |
cruise speed |
180 mph |
290 km/h |
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capacity |
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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.