Attribute | Grumman F11F Tiger × | Grumman F9F-6 Cougar × |
---|---|---|
General | ||
Manufacturer | Grumman | Grumman |
Model | Grumman F11F Tiger | Grumman F9F-6 Cougar |
Country | United States | United States |
Manufactured from (year) | 1954 | 1951 |
Manufactured to (year) | 1959 | 1960 |
Type | Fighter Jets | Fighter Jets |
Icao | F11F | F9F6 |
Performance | ||
Engine | 1x Wright J65-W-18 afterburning turbojet | 1x Pratt & Whitney J48-P-8 |
Power, lbf (lbf) | 10,500 | 7,250 |
Avionics | AN/ARC-27A UHF COMMS, AN/ARA-25 UHF, AN/ARR-40 UHF, AN/ARN-14E VHF Nav etc. | AN/APG-30, AN/ARC-27, AN/APN-1 etc. |
Max cruise speed (km/h) | 1,213 | 1,052 |
Approach speed (km/h) | - | 172 |
Travel range (km) | 2,056 | 1,695 |
Service ceiling (m) | 12,771 | 13,564 |
Rate of climb (m/sec) | 82.8 | 34.29 |
Take off distance (m) | - | 640 |
Landing distance (m) | - | 415 |
Weights | ||
Max take off weight (kg) | 10,641 | 9,525 |
Max landing weight (kg) | 9,541 | 7,167 |
Max payload (kg) | 1,360 | 1,400 |
Fuel tank capacity (l) | 3,872 | 3,479 |
Dimensions | ||
Seats | 1 | 1 |
Exterior length (m) | 13.98 | 12.47 |
Tail height (m) | 4.03 | 3.75 |
Fuselage diameter (m) | 0.7 | 1.5 |
Wing span (m) | 9.64 | 10.52 |
Wing tips | No Winglets | No Winglets |