Airbus A321XLR vs. Lockheed U-2

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Airbus A321XLR 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 LEAP-1A and P&W PW1100G engines 1 × General Electric F118-101
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)
101,000 kg 222,700 lb MTOW 18,144 kg 40,000 lb
4,700 nmi 8,704 km range 6,090 nm 11,278 km
963km/h 598mph cruise speed 475 mph 764 km/h
180-220 seats (typical 2-class seating) 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.