Lockheed Martin F-35 Lightning II vs. Beechcraft King Air 260
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Lockheed Martin F-35 Lightning II |
versus |
Beechcraft King Air 260 |
15.67 m |
51 ft 4 in |
length |
13.41 m |
43 ft 11 in |
4.33 m |
14 ft 2 in |
height |
4.57 m |
15 ft |
10.7 m |
35 ft 1 in |
wingspan |
17.39 m |
57 ft 1 in |
Pratt & Whitney F135 and GE Rolls-Royce Fighter Engine Team F136 |
engines |
2 x Pratt & Whitney Canada PT6A turboprop |
40,000 lb |
thrust per engine |
1050 lbs |
40,000 lb |
total thrust |
2100 lbs |
31,800 kg |
70,000 lb |
MTOW |
12,500 lb |
5,670 kg |
1,380 mi |
1,200 nm |
range |
1,720 nm |
3,185 km |
520 kt |
302 mph |
cruise speed |
310 kts |
193 mph |
18,000 pounds of total ordinance |
capacity |
9 |
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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.