Lockheed Martin F-35 Lightning II vs. Airbus A380-800F

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Lockheed Martin F-35 Lightning II versus Airbus A380-800F
15.67 m 51 ft 4 in length 72.73 m 238 ft 7 in
4.33 m 14 ft 2 in height 24.09 m 79 ft
10.7 m 35 ft 1 in wingspan 79.75 m 261 ft 8 in
Pratt & Whitney F135 and GE Rolls-Royce Fighter Engine Team F136 engines 4 x Engine Alliance GP7200 turbofan engines
40,000 lb thrust per engine 70,000 to 80,000 pounds of thrust (311 to 356 kilonewtons)
40,000 lb total thrust 280,000 to 320,000 pounds
31,800 kg 70,000 lb MTOW 590,000 kg 1,300,733 lb
1,380 mi 1,200 nm range 14,800 km 7,992 nm
520 kt 302 mph cruise speed 903 km/h 561 mph
18,000 pounds of total ordinance 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.