Attribute | ![]() North American P-51 Mustang × | ![]() Curtiss P-40 Warhawk × |
---|---|---|
General | ||
Manufacturer | North American Aviation NAA | Curtiss |
Model | North American P-51 Mustang | Curtiss P-40 Warhawk |
Country | United States | United States |
Manufactured from (year) | 1940 | 1939 |
Manufactured to (year) | 1945 | 1944 |
Type | Military Propellor Planes | Military Propellor Planes |
Icao | P51 | P40 |
Performance | ||
Engine | 1x Packard (Rolls Royce) V-1650-7 Merlin | 1x Allison V-1710-39 |
Power, hp (hp) | 1,720 | 1,240 |
Max cruise speed (km/h) | 709 | 589 |
Approach speed (km/h) | 161 | 154 |
Travel range (km) | 2,656 | 1,152 |
Service ceiling (m) | 12,771 | 8,839 |
Rate of climb (m/sec) | 16.26 | 10.67 |
Take off distance (m) | 366 | - |
Landing distance (m) | 457 | - |
Weights | ||
Max take off weight (kg) | 5,490 | 4,173 |
Max landing weight (kg) | 5,490 | 3,862 |
Max payload (kg) | 910 | 910 |
Fuel tank capacity (l) | 1,018 | 594 |
Dimensions | ||
Seats | 1 | 1 |
Exterior length (m) | 9.8 | 10.15 |
Tail height (m) | 4.08 | 3.77 |
Fuselage diameter (m) | 0.9 | 1 |
Wing span (m) | 11.28 | 11.36 |
Wing tips | No Winglets | No Winglets |