Avro 652 Anson vs. Lockheed U-2

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Avro 652 Anson versus Lockheed U-2
12.88 m 42 ft 3 in length 19.2 m 63 ft 0 in
2.9 m 9 ft 6 in height 4.8 m 15 ft 9 in
17.22 m 56 ft 6 in wingspan 32 m 105 ft
2 × Armstrong Siddeley Cheetah VI engines 1 × General Electric F118-101
290 hp (220 kW) thrust per engine 17,000 lbf (76 kN)
580 hp (440 kW) total thrust 17,000 lbf (76 kN)
7,500 lb 3,402 kg MTOW 18,144 kg 40,000 lb
1,267 km 684 nm range 6,090 nm 11,278 km
165 mph 266 km/h cruise speed 475 mph 764 km/h
4 passengers 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.