Comparison of Grumman F9F-6 Cougar and Lockheed P-80 Shooting Star [S]ave
| Attribute |  Grumman F9F-6 Cougar × |  Lockheed P-80 Shooting Star × |
|---|---|---|
| General | ||
| Manufacturer | Grumman | Lockheed Martin Aeronautics |
| Model | Grumman F9F-6 Cougar | Lockheed P-80 Shooting Star |
| Country | United States | United States |
| Manufactured from (year) | 1951 | 1945 |
| Manufactured to (year) | 1960 | 1950 |
| Type | Fighter Jets | Fighter Jets |
| Icao | F9F6 | P80 |
| Performance | ||
| Engine | 1x Pratt & Whitney J48-P-8 | 1x Allison J33-A-35 |
| Power, lbf (lbf) | 7,250 | 4,600 |
| Avionics | AN/APG-30, AN/ARC-27, AN/APN-1 etc. | - |
| Max cruise speed (km/h) | 1,052 | 956 |
| Approach speed (km/h) | 172 | - |
| Travel range (km) | 1,695 | 2,222 |
| Service ceiling (m) | 13,564 | 14,265 |
| Rate of climb (m/sec) | 34.29 | 34.9 |
| Take off distance (m) | 640 | - |
| Landing distance (m) | 415 | - |
| Weights | ||
| Max take off weight (kg) | 9,525 | 7,257 |
| Max landing weight (kg) | 7,167 | 6,350 |
| Max payload (kg) | 1,400 | 1,000 |
| Fuel tank capacity (l) | 3,479 | 3,350 |
| Dimensions | ||
| Seats | 1 | 1 |
| Exterior length (m) | 12.47 | 10.5 |
| Tail height (m) | 3.75 | 3.45 |
| Fuselage diameter (m) | 1.5 | 1 |
| Wing span (m) | 10.52 | 11.83 |
| Wing tips | No Winglets | No Winglets |
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