Attribute | North American F-100 Super Sabre × | Grumman F11F Tiger × |
---|---|---|
General | ||
Manufacturer | North American Aviation NAA | Grumman |
Model | North American F-100 Super Sabre | Grumman F11F Tiger |
Country | United States | United States |
Manufactured from (year) | 1953 | 1954 |
Manufactured to (year) | 1959 | 1959 |
Type | Fighter Jets | Fighter Jets |
Icao | F100 | F11F |
Performance | ||
Engine | 1x Pratt & Whitney J57-P-21/21A | 1x Wright J65-W-18 afterburning turbojet |
Power, lbf (lbf) | 16,000 | 10,500 |
Avionics | Minneapolis-Honeywell MB-3, AN/AJB-1B, AN/APR-26 | AN/ARC-27A UHF COMMS, AN/ARA-25 UHF, AN/ARR-40 UHF, AN/ARN-14E VHF Nav etc. |
Max cruise speed (km/h) | 1,487 | 1,213 |
Approach speed (km/h) | 300 | - |
Travel range (km) | 3,211 | 2,056 |
Service ceiling (m) | 15,240 | 12,771 |
Rate of climb (m/sec) | 113.79 | 82.8 |
Weights | ||
Max take off weight (kg) | 15,800 | 10,641 |
Max landing weight (kg) | 15,606 | 9,541 |
Max payload (kg) | 3,190 | 1,360 |
Fuel tank capacity (l) | 9,887 | 3,872 |
Dimensions | ||
Seats | 1 | 1 |
Exterior length (m) | 15 | 13.98 |
Tail height (m) | 4.95 | 4.03 |
Fuselage diameter (m) | 1.6 | 0.7 |
Wing span (m) | 11.8 | 9.64 |
Wing tips | No Winglets | No Winglets |