Airbus A310-300 vs. Lockheed Martin F-35 Lightning II

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Airbus A310-300 versus Lockheed Martin F-35 Lightning II
46.66 m 153 ft 1 in length 15.67 m 51 ft 4 in
15.8 m 51 ft 10 in height 4.33 m 14 ft 2 in
43.9 m 144 ft wingspan 10.7 m 35 ft 1 in
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines Pratt & Whitney F135 and GE Rolls-Royce Fighter Engine Team F136
52,000 lb thrust per engine 40,000 lb
104,000 lb total thrust 40,000 lb
148,768 kg 328,000 lb MTOW 31,800 kg 70,000 lb
8,050 km 4,348 nm range 1,380 mi 1,200 nm
482 knots 279 mph cruise speed 520 kt 302 mph
190-230 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.