Avro Shackleton vs. Lockheed U-2

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Avro Shackleton versus Lockheed U-2
26.6 m 87 ft 4 in length 19.2 m 63 ft 0 in
6.22 m 20 ft 5 in height 4.8 m 15 ft 9 in
36.58 m 120 ft wingspan 32 m 105 ft
4 x Rolls-Royce Griffon 57 engines 1 × General Electric F118-101
1,960 horsepower thrust per engine 17,000 lbf (76 kN)
7,840 horsepower total thrust 17,000 lbf (76 kN)
39,009 kg 86,000 lb MTOW 18,144 kg 40,000 lb
3,621 km 1,955 nm range 6,090 nm 11,278 km
262 kts 163 mph cruise speed 475 mph 764 km/h
10,000lb of bombs, torpedoes or mines 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.