Comparison of North American F-100 Super Sabre and Vought F8U Crusader [S]ave
| Attribute |  North American F-100 Super Sabre × |  Vought F8U Crusader × |
|---|---|---|
| General | ||
| Manufacturer | North American Aviation NAA | Vought |
| Model | North American F-100 Super Sabre | Vought F8U Crusader |
| Country | United States | United States |
| Manufactured from (year) | 1953 | 1957 |
| Manufactured to (year) | 1959 | 1964 |
| Type | Fighter Jets | Fighter Jets |
| Icao | F100 | F8 |
| Performance | ||
| Engine | 1x Pratt & Whitney J57-P-21/21A | 1x Pratt & Whitney J57-P-20A |
| Power, lbf (lbf) | 16,000 | 18,000 |
| Avionics | Minneapolis-Honeywell MB-3, AN/AJB-1B, AN/APR-26 | Magnavox AN/APQ-84 or AN/APQ-94 Fire-control radar |
| Max cruise speed (km/h) | 1,487 | 1,861 |
| Approach speed (km/h) | 300 | - |
| Travel range (km) | 3,211 | 2,259 |
| Service ceiling (m) | 15,240 | 17,983 |
| Rate of climb (m/sec) | 113.79 | 96.52 |
| Weights | ||
| Max take off weight (kg) | 15,800 | 15,422 |
| Max landing weight (kg) | 15,606 | 13,154 |
| Max payload (kg) | 3,190 | 2,450 |
| Fuel tank capacity (l) | 9,887 | 5,016 |
| Dimensions | ||
| Seats | 1 | 1 |
| Exterior length (m) | 15 | 16.6 |
| Tail height (m) | 4.95 | 4.8 |
| Fuselage diameter (m) | 1.6 | 1.1 |
| Wing span (m) | 11.8 | 10.87 |
| Wing tips | No Winglets | No Winglets |
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