Airbus A321LR vs. Lockheed U-2

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Airbus A321LR versus Lockheed U-2
44.51 m 146 ft 0 in length 19.2 m 63 ft 0 in
11.76 m 38 ft 7 in height 4.8 m 15 ft 9 in
35.8 m 117 ft 5 in wingspan 32 m 105 ft
CFM International’s LEAP-1A or Pratt & Whitney’s PurePower PW1100G-JM engines 1 × General Electric F118-101
Over 33,000 lbs (147 kN) thrust per engine 17,000 lbf (76 kN)
66,000 lbs (294 kN) total thrust 17,000 lbf (76 kN)
97,000 kg 213,800 lb MTOW 18,144 kg 40,000 lb
7,400 km 4,000 nm range 6,090 nm 11,278 km
832 km/h 517 mph cruise speed 475 mph 764 km/h
180-220 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.