Lockheed U-2 vs. North American T-6 Texan

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Lockheed U-2 versus North American T-6 Texan
19.2 m 63 ft 0 in length 9.0 m 29 ft 6 in
4.8 m 15 ft 9 in height 3.56 m 11 ft 8 in
32 m 105 ft wingspan 12.8 m 42 ft
1 × General Electric F118-101 engines 1 x Pratt & Whitney R-1340-AN-1 radial engine
17,000 lbf (76 kN) thrust per engine Approximately 600 hp
17,000 lbf (76 kN) total thrust Approximately 600 hp
18,144 kg 40,000 lb MTOW 5,617 lb 2,548 kg
6,090 nm 11,278 km range 1,175 km 634 nm
475 mph 764 km/h cruise speed 145 mph 233 km/h
capacity Pilot and one passenger
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.