Lockheed Martin F-35 Lightning II vs. North American B-25 Mitchell
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Lockheed Martin F-35 Lightning II |
versus |
North American B-25 Mitchell |
15.67 m |
51 ft 4 in |
length |
16.15 m |
53 ft 0 in |
4.33 m |
14 ft 2 in |
height |
5 m |
16 ft 4 in |
10.7 m |
35 ft 1 in |
wingspan |
20.58 m |
67 ft 6 in |
Pratt & Whitney F135 and GE Rolls-Royce Fighter Engine Team F136 |
engines |
2 x Wright R-2600-92 Twin Cyclone |
40,000 lb |
thrust per engine |
1,700 horsepower |
40,000 lb |
total thrust |
3,400 horsepower |
31,800 kg |
70,000 lb |
MTOW |
7,484 kg |
16,500 lb |
1,380 mi |
1,200 nm |
range |
1,350 mi |
1,175 nm |
520 kt |
302 mph |
cruise speed |
233 MPH |
375 km/h |
18,000 pounds of total ordinance |
capacity |
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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.