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 |