Lockheed U-2 vs. North American F-100 Super Sabre
... or view the full comparison list
here.
| Lockheed U-2 |
versus |
North American F-100 Super Sabre |
| 19.2 m |
63 ft 0 in |
length |
16.46 m |
54 ft 2 in |
| 4.8 m |
15 ft 9 in |
height |
4.93 m |
16 ft 2 in |
| 32 m |
105 ft |
wingspan |
11.84 m |
38 ft 1 |
| 1 × General Electric F118-101 |
engines |
1 Pratt & Whitney J57-P-21A |
| 17,000 lbf (76 kN) |
thrust per engine |
16,000 lb. thrust in afterburner |
| 17,000 lbf (76 kN) |
total thrust |
16,000 lb. (afterburner) |
| 18,144 kg |
40,000 lb |
MTOW |
17,609 kg |
38,800 lb |
| 6,090 nm |
11,278 km |
range |
2,673 km |
1,444 nm |
| 475 mph |
764 km/h |
cruise speed |
587 mph |
945 km/h |
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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.
