Airbus A321XLR vs. Lockheed C-69 Constellation

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Airbus A321XLR versus Lockheed C-69 Constellation
44.51 m 146 ft 0 in length 29.72 m 97 ft 6 in
11.76 m 38 ft 7 in height 6.02 m 19 ft 9 in
35.8 m 117 ft 5 in wingspan 37.49 m 123 ft
CFM LEAP-1A and P&W PW1100G engines 4 x Wright R-3350 Duplex-Cyclone radial engines
33,000 lbs (147 kN) thrust per engine 2,200 to 3,700 horsepower (1,640 to 2,760 kW)
66,000 lbs (294 kN) total thrust 8,800 to 14,800 horsepower
101,000 kg 222,700 lb MTOW 44,453 kg 98,000 lb
4,700 nmi 8,704 km range 5,200 km 2,808 nm
963km/h 598mph cruise speed 507 km/h 315 mph
180-220 seats (typical 2-class seating) capacity Up to 109 passengers
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.