Airbus A321LR vs. Lockheed Martin F-35 Lightning II

versus
... or view the full comparison list here.
Airbus A321LR 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 International’s LEAP-1A or Pratt & Whitney’s PurePower PW1100G-JM engines Pratt & Whitney F135 and GE Rolls-Royce Fighter Engine Team F136
Over 33,000 lbs (147 kN) thrust per engine 40,000 lb
66,000 lbs (294 kN) total thrust 40,000 lb
97,000 kg 213,800 lb MTOW 31,800 kg 70,000 lb
7,400 km 4,000 nm range 1,380 mi 1,200 nm
832 km/h 517 mph cruise speed 520 kt 302 mph
180-220 passengers 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.