| Attribute | Grumman F8F Bearcat × | Curtiss P-40 Warhawk × |
|---|---|---|
| General | ||
| Manufacturer | Grumman | Curtiss |
| Model | Grumman F8F Bearcat | Curtiss P-40 Warhawk |
| Country | United States | United States |
| Manufactured from (year) | 1943 | 1939 |
| Manufactured to (year) | 1949 | 1944 |
| Type | Military Propellor Planes | Military Propellor Planes |
| Icao | F8F | P40 |
| Performance | ||
| Engine | 1x Pratt & Whitney R-2800-30W Double Wasp | 1x Allison V-1710-39 |
| Power, hp (hp) | 2,250 | 1,240 |
| Avionics | AN/ARC-1, AN/ARR-2A, R-23/ARC-5 | - |
| Max cruise speed (km/h) | 732 | 589 |
| Approach speed (km/h) | 137 | 154 |
| Travel range (km) | 1,778 | 1,152 |
| Service ceiling (m) | 12,436 | 8,839 |
| Rate of climb (m/sec) | 22.68 | 10.67 |
| Take off distance (m) | 185 | - |
| Landing distance (m) | 250 | - |
| Weights | ||
| Max take off weight (kg) | 6,105 | 4,173 |
| Max landing weight (kg) | 5,941 | 3,862 |
| Max payload (kg) | 1,000 | 910 |
| Fuel tank capacity (l) | 2,025 | 594 |
| Dimensions | ||
| Seats | 1 | 1 |
| Exterior length (m) | 8.43 | 10.15 |
| Tail height (m) | 4.16 | 3.77 |
| Fuselage diameter (m) | 1.35 | 1 |
| Wing span (m) | 10.82 | 11.36 |
| Wing tips | No Winglets | No Winglets |