Lockheed Martin F-35 Lightning II vs. Airbus A300-600F

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Lockheed Martin F-35 Lightning II versus Airbus A300-600F
15.67 m 51 ft 4 in length 54.08 m 177 ft 5 in
4.33 m 14 ft 2 in height 17.05 m 55 ft 11 in
10.7 m 35 ft 1 in wingspan 44.84 m 147 ft 1 in
Pratt & Whitney F135 and GE Rolls-Royce Fighter Engine Team F136 engines 2 x General Electric CF6-80C2A5 turbofan engines
40,000 lb thrust per engine Approximately 59,000 lbf per engine
40,000 lb total thrust Approximately 118,000 lbf total
31,800 kg 70,000 lb MTOW 170,000 kg 374,786 lb
1,380 mi 1,200 nm range 4,830 km 2,608 nm
520 kt 302 mph cruise speed 860 km/h 534 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.