Airbus A321-200 vs. Lockheed Martin F-35 Lightning II

versus
... or view the full comparison list here.
Airbus A321-200 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
2 GE CFM56-5B3 engines Pratt & Whitney F135 and GE Rolls-Royce Fighter Engine Team F136
31,600 lbs thrust per engine 40,000 lb
63,200 lbs total thrust 40,000 lb
89,000 kg 196,200 lb MTOW 31,800 kg 70,000 lb
4,000 nmi 7,408 km range 1,380 mi 1,200 nm
871 km/h 541 mph cruise speed 520 kt 302 mph
185 to 220 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.