Lockheed U-2 vs. North American Rockwell OV-10 Bronco

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Lockheed U-2 versus North American Rockwell OV-10 Bronco
19.2 m 63 ft 0 in length 12.7 m 41 ft 7 in
4.8 m 15 ft 9 in height 4.62 m 15 ft 2 in
32 m 105 ft wingspan 12.19 m 40 ft
1 × General Electric F118-101 engines 2 x Garrett T76-G-420/421 turboprop engines
17,000 lbf (76 kN) thrust per engine Approximately 715 hp each
17,000 lbf (76 kN) total thrust Approximately 1,430 hp total
18,144 kg 40,000 lb MTOW 14,444 lb 6,553 kg
6,090 nm 11,278 km range 1,931 km 1,043 nm
475 mph 764 km/h cruise speed 244 mph 393 km/h
capacity Pilot and observer
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.