Lockheed U-2 vs. Praetor 600

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Lockheed U-2 versus Praetor 600
19.2 m 63 ft 0 in length 17.02 m 55 ft 10 in
4.8 m 15 ft 9 in height 6.2 m 20 ft 4 in
32 m 105 ft wingspan 20.97 m 68 ft 9 in
1 × General Electric F118-101 engines 2 Honeywell HTF7500E
17,000 lbf (76 kN) thrust per engine 7,036 lbf
17,000 lbf (76 kN) total thrust 14,072 lbf
18,144 kg 40,000 lb MTOW 31,750 lb 14,397 kg
6,090 nm 11,278 km range 4,018 nm 7,435 km
475 mph 764 km/h cruise speed 466 kts 290 mph
capacity 12
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.