| Attribute | Value |
|---|---|
| General | |
| Manufacturer | Grumman |
| Model | Grumman F9F-6 Cougar |
| Country | United States |
| Manufactured from | 1951 year |
| Manufactured to | 1960 year |
| Type | Fighter Jets |
| Icao | F9F6 |
| Performance | |
| Engine | 1x Pratt & Whitney J48-P-8 |
| Power, hp | Add |
| Power, lbf | 7,250 lbf |
| Avionics | AN/APG-30, AN/ARC-27, AN/APN-1 etc. |
| Max cruise speed | 1,052 km/h |
| Approach speed | 172 km/h |
| Travel range | 1,695 km |
| Fuel economy | Add |
| Service ceiling | 13,564 m |
| Rate of climb | 34.29 m/sec |
| Take off distance | 640 m |
| Landing distance | 415 m |
| Weights | |
| Max take off weight | 9,525 kg |
| Max landing weight | 7,167 kg |
| Max payload | 1,400 kg |
| Fuel tank capacity | 3,479 l |
| Baggage volume | Add |
| Dimensions | |
| Seats | 1 |
| Seats - business class | Add |
| Seats - first class | Add |
| Cabin height | Add |
| Cabin width | Add |
| Cabin length | Add |
| Exterior length | 12.47 m |
| Tail height | 3.75 m |
| Fuselage diameter | 1.5 m |
| Wing span | 10.52 m |
| Wing tips | No Winglets |