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