Airbus A321XLR vs. Lockheed Martin F-35 Lightning II

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Airbus A321XLR versus Lockheed Martin F-35 Lightning II
44.51 m 146 ft 0 in length 15.67 m 51 ft 4 in
11.76 m 38 ft 7 in height 4.33 m 14 ft 2 in
35.8 m 117 ft 5 in wingspan 10.7 m 35 ft 1 in
CFM LEAP-1A and P&W PW1100G engines Pratt & Whitney F135 and GE Rolls-Royce Fighter Engine Team F136
33,000 lbs (147 kN) thrust per engine 40,000 lb
66,000 lbs (294 kN) total thrust 40,000 lb
101,000 kg 222,700 lb MTOW 31,800 kg 70,000 lb
4,700 nmi 8,704 km range 1,380 mi 1,200 nm
963km/h 598mph cruise speed 520 kt 302 mph
180-220 seats (typical 2-class seating) capacity 18,000 pounds of total ordinance
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.