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