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
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.