Lockheed U-2 vs. PZL TS-11 Iskra
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Lockheed U-2 |
versus |
PZL TS-11 Iskra |
19.2 m |
63 ft 0 in |
length |
11.15 m |
36 ft 7 in |
4.8 m |
15 ft 9 in |
height |
3.5 m |
11 ft 6 in |
32 m |
105 ft |
wingspan |
10.06 m |
33 ft |
1 × General Electric F118-101 |
engines |
1 (WSK PZL Rzeszow SO-3W) |
17,000 lbf (76 kN) |
thrust per engine |
10.8 kN |
17,000 lbf (76 kN) |
total thrust |
10.8 kN |
18,144 kg |
40,000 lb |
MTOW |
3,840 kg |
8,466 lb |
6,090 nm |
11,278 km |
range |
1,250 km |
675 nm |
475 mph |
764 km/h |
cruise speed |
770 km/h |
478 mph |
|
capacity |
2 |
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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.