Lockheed U-2 vs. North American BT-9

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Lockheed U-2 versus North American BT-9
19.2 m 63 ft 0 in length 8.79 m 28 ft 10 in
4.8 m 15 ft 9 in height 2.82 m 9 ft 3 in
32 m 105 ft wingspan 10.97 m 36 ft
1 × General Electric F118-101 engines 1 x Wright R-975-3 radial engine
17,000 lbf (76 kN) thrust per engine Approximately 440 hp
17,000 lbf (76 kN) total thrust Approximately 440 hp
18,144 kg 40,000 lb MTOW 4,300 lb 1,950 kg
6,090 nm 11,278 km range 917 km 495 nm
475 mph 764 km/h cruise speed 150 mph 241 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.