Lockheed U-2 vs. North American B-25 Mitchell

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Lockheed U-2 versus North American B-25 Mitchell
19.2 m 63 ft 0 in length 16.15 m 53 ft 0 in
4.8 m 15 ft 9 in height 5 m 16 ft 4 in
32 m 105 ft wingspan 20.58 m 67 ft 6 in
1 × General Electric F118-101 engines 2 x Wright R-2600-92 Twin Cyclone
17,000 lbf (76 kN) thrust per engine 1,700 horsepower
17,000 lbf (76 kN) total thrust 3,400 horsepower
18,144 kg 40,000 lb MTOW 7,484 kg 16,500 lb
6,090 nm 11,278 km range 1,350 mi 1,175 nm
475 mph 764 km/h cruise speed 233 MPH 375 km/h
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.