Airbus A321XLR vs. North American F-100 Super Sabre

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Airbus A321XLR versus North American F-100 Super Sabre
44.51 m 146 ft 0 in length 16.46 m 54 ft 2 in
11.76 m 38 ft 7 in height 4.93 m 16 ft 2 in
35.8 m 117 ft 5 in wingspan 11.84 m 38 ft 1
CFM LEAP-1A and P&W PW1100G engines 1 Pratt & Whitney J57-P-21A
33,000 lbs (147 kN) thrust per engine 16,000 lb. thrust in afterburner
66,000 lbs (294 kN) total thrust 16,000 lb. (afterburner)
101,000 kg 222,700 lb MTOW 17,609 kg 38,800 lb
4,700 nmi 8,704 km range 2,673 km 1,444 nm
963km/h 598mph cruise speed 587 mph 945 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.