Comparison of Curtiss P-40 Warhawk and Vought SB2U Vindicator [S]ave
| Attribute |  Curtiss P-40 Warhawk × |  Vought SB2U Vindicator × |
|---|---|---|
| General | ||
| Manufacturer | Curtiss | Vought |
| Model | Curtiss P-40 Warhawk | Vought SB2U Vindicator |
| Country | United States | United States |
| Manufactured from (year) | 1939 | 1936 |
| Manufactured to (year) | 1944 | 1941 |
| Type | Military Propellor Planes | Military Propellor Planes |
| Icao | P40 | SB2U |
| Performance | ||
| Engine | 1x Allison V-1710-39 | 1x Pratt & Whitney R-1535-02 Twin Wasp Jr |
| Power, hp (hp) | 1,240 | 825 |
| Max cruise speed (km/h) | 589 | 391 |
| Approach speed (km/h) | 154 | 115 |
| Travel range (km) | 1,152 | 1,796 |
| Service ceiling (m) | 8,839 | 8,382 |
| Rate of climb (m/sec) | 10.67 | 5.44 |
| Weights | ||
| Max take off weight (kg) | 4,173 | 4,273 |
| Max landing weight (kg) | 3,862 | 3,390 |
| Max payload (kg) | 910 | 680 |
| Fuel tank capacity (l) | 594 | 1,401 |
| Dimensions | ||
| Seats | 1 | 2 |
| Exterior length (m) | 10.15 | 10.36 |
| Tail height (m) | 3.77 | 4.34 |
| Fuselage diameter (m) | 1 | 1.1 |
| Wing span (m) | 11.36 | 12.8 |
| Wing tips | No Winglets | No Winglets |
Help · Contact us · Disclaimer · Contributors · Developers · Donate