Grumman OV-1 Mohawk vs. Lockheed U-2

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Grumman OV-1 Mohawk versus Lockheed U-2
12.52 m 41 ft 1 in length 19.2 m 63 ft 0 in
3.89 m 12 ft 9 in height 4.8 m 15 ft 9 in
14.63 m 48 ft wingspan 32 m 105 ft
2 x Lycoming T53 turboprop engines engines 1 × General Electric F118-101
Approximately 1,100 hp each thrust per engine 17,000 lbf (76 kN)
Approximately 2,200 hp total total thrust 17,000 lbf (76 kN)
14,950 lb 6,781 kg MTOW 18,144 kg 40,000 lb
1,690 km 913 nm range 6,090 nm 11,278 km
230 mph 370 km/h cruise speed 475 mph 764 km/h
Pilot and observer capacity
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.