Airbus A340-200 vs. Lockheed Martin F-35 Lightning II
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Airbus A340-200 |
versus |
Lockheed Martin F-35 Lightning II |
59.4 m |
194 ft 11 in |
length |
15.67 m |
51 ft 4 in |
16.8 m |
55 ft 1 in |
height |
4.33 m |
14 ft 2 in |
60.3 m |
197 ft 9 in |
wingspan |
10.7 m |
35 ft 1 in |
4 x CFM International CFM56-5C4 |
engines |
Pratt & Whitney F135 and GE Rolls-Royce Fighter Engine Team F136 |
34,000 lbf |
thrust per engine |
40,000 lb |
136,000 lbf |
total thrust |
40,000 lb |
275,000 kg |
606,300 lb |
MTOW |
31,800 kg |
70,000 lb |
12,400 km |
6,699 nm |
range |
1,380 mi |
1,200 nm |
880 km/h |
547 mph |
cruise speed |
520 kt |
302 mph |
Typical seating 3-class 210-250 |
capacity |
18,000 pounds of total ordinance |
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rotor diameter |
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rate of climb |
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Please note that these values are indicative and actual values can vary based on specific engine models and configurations.