Lockheed U-2 vs. Soko G-2 Galeb

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Lockheed U-2 versus Soko G-2 Galeb
19.2 m 63 ft 0 in length 10.34 m 33 ft 11 in
4.8 m 15 ft 9 in height 3.28 m 10 ft 9 in
32 m 105 ft wingspan 11.62 m 38 ft 1 in
1 × General Electric F118-101 engines 1 x Armstrong Siddeley Viper II Mark 22/6 turbojet
17,000 lbf (76 kN) thrust per engine 2,500 lb
17,000 lbf (76 kN) total thrust 2,500 lb
18,144 kg 40,000 lb MTOW 4,300 kg 9,480 lb
6,090 nm 11,278 km range 1,242 km 671 nm
475 mph 764 km/h cruise speed 730 km/h 454 mph
capacity Fuel capacity: 1,120 ltr
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.