Airbus A330-200 vs. Lockheed Martin F-35 Lightning II

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Airbus A330-200 versus Lockheed Martin F-35 Lightning II
58.82 m 193 ft 0 in length 15.67 m 51 ft 4 in
17.39 m 57 ft 1 in height 4.33 m 14 ft 2 in
64 m 210 ft wingspan 10.7 m 35 ft 1 in
2 Turbofans engines Pratt & Whitney F135 and GE Rolls-Royce Fighter Engine Team F136
GE CF6-80E1A3: 304.7 kN / 68500 lbf, PW4170: 311.4 kN / 70000 lbf, RR Trent 772C-60: 316.3 kN / 71100 lbf thrust per engine 40,000 lb
Depends on the engine variant total thrust 40,000 lb
251,000 kg 553,400 lb MTOW 31,800 kg 70,000 lb
15,094 km 8,150 nm range 1,380 mi 1,200 nm
531 mph 855 km/h cruise speed 520 kt 302 mph
220-260 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.