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

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Airbus A300-600 versus Lockheed Martin F-35 Lightning II
54.10 m 177 ft 6 in length 15.67 m 51 ft 4 in
16.5 m 54 ft 2 in height 4.33 m 14 ft 2 in
44.84 m 147 ft 1 in wingspan 10.7 m 35 ft 1 in
2 x turbofan engines, either Pratt & Whitney PW 4000 or General Electric GE CF6-80C2A1 engines Pratt & Whitney F135 and GE Rolls-Royce Fighter Engine Team F136
56,000lb to 61,500lb thrust per engine 40,000 lb
112,000–123,000 lb total thrust 40,000 lb
171,700 kg 378,600 lb MTOW 31,800 kg 70,000 lb
7,500 km 4,052 nm range 1,380 mi 1,200 nm
897 km/h 557 mph cruise speed 520 kt 302 mph
210-250 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.