Attribute | ![]() Vought F8U Crusader × | ![]() Grumman F11F Tiger × |
---|---|---|
General | ||
Manufacturer | Vought | Grumman |
Model | Vought F8U Crusader | Grumman F11F Tiger |
Country | United States | United States |
Manufactured from (year) | 1957 | 1954 |
Manufactured to (year) | 1964 | 1959 |
Type | Fighter Jets | Fighter Jets |
Icao | F8 | F11F |
Performance | ||
Engine | 1x Pratt & Whitney J57-P-20A | 1x Wright J65-W-18 afterburning turbojet |
Power, lbf (lbf) | 18,000 | 10,500 |
Avionics | Magnavox AN/APQ-84 or AN/APQ-94 Fire-control radar | AN/ARC-27A UHF COMMS, AN/ARA-25 UHF, AN/ARR-40 UHF, AN/ARN-14E VHF Nav etc. |
Max cruise speed (km/h) | 1,861 | 1,213 |
Travel range (km) | 2,259 | 2,056 |
Service ceiling (m) | 17,983 | 12,771 |
Rate of climb (m/sec) | 96.52 | 82.8 |
Weights | ||
Max take off weight (kg) | 15,422 | 10,641 |
Max landing weight (kg) | 13,154 | 9,541 |
Max payload (kg) | 2,450 | 1,360 |
Fuel tank capacity (l) | 5,016 | 3,872 |
Dimensions | ||
Seats | 1 | 1 |
Exterior length (m) | 16.6 | 13.98 |
Tail height (m) | 4.8 | 4.03 |
Fuselage diameter (m) | 1.1 | 0.7 |
Wing span (m) | 10.87 | 9.64 |
Wing tips | No Winglets | No Winglets |