Lockheed Martin F-35 Lightning II vs. North American F-100 Super Sabre
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Lockheed Martin F-35 Lightning II |
versus |
North American F-100 Super Sabre |
15.67 m |
51 ft 4 in |
length |
16.46 m |
54 ft 2 in |
4.33 m |
14 ft 2 in |
height |
4.93 m |
16 ft 2 in |
10.7 m |
35 ft 1 in |
wingspan |
11.84 m |
38 ft 1 |
Pratt & Whitney F135 and GE Rolls-Royce Fighter Engine Team F136 |
engines |
1 Pratt & Whitney J57-P-21A |
40,000 lb |
thrust per engine |
16,000 lb. thrust in afterburner |
40,000 lb |
total thrust |
16,000 lb. (afterburner) |
31,800 kg |
70,000 lb |
MTOW |
17,609 kg |
38,800 lb |
1,380 mi |
1,200 nm |
range |
2,673 km |
1,444 nm |
520 kt |
302 mph |
cruise speed |
587 mph |
945 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.