McDonnell-Douglas DC-10-30 vs. Lockheed Martin F-35 Lightning II
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McDonnell-Douglas DC-10-30 |
versus |
Lockheed Martin F-35 Lightning II |
55.35 m |
181 ft 8 in |
length |
15.67 m |
51 ft 4 in |
17.8 m |
58 ft 5 in |
height |
4.33 m |
14 ft 2 in |
50.39 m |
165 ft 4 in |
wingspan |
10.7 m |
35 ft 1 in |
3x GE CF6-50C Turbofan |
engines |
Pratt & Whitney F135 and GE Rolls-Royce Fighter Engine Team F136 |
54,000 lbf |
thrust per engine |
40,000 lb |
162,000 lbf |
total thrust |
40,000 lb |
251,744 kg |
555,000 lb |
MTOW |
31,800 kg |
70,000 lb |
9,630 km |
5,200 nm |
range |
1,380 mi |
1,200 nm |
507 knots |
939 km/h |
cruise speed |
520 kt |
302 mph |
Up to 380 passengers |
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.