Comparison of North American P-51 Mustang and Vought SB2U Vindicator [S]ave
| Attribute |  North American P-51 Mustang × |  Vought SB2U Vindicator × |
|---|---|---|
| General | ||
| Manufacturer | North American Aviation NAA | Vought |
| Model | North American P-51 Mustang | Vought SB2U Vindicator |
| Country | United States | United States |
| Manufactured from (year) | 1940 | 1936 |
| Manufactured to (year) | 1945 | 1941 |
| Type | Military Propellor Planes | Military Propellor Planes |
| Icao | P51 | SB2U |
| Performance | ||
| Engine | 1x Packard (Rolls Royce) V-1650-7 Merlin | 1x Pratt & Whitney R-1535-02 Twin Wasp Jr |
| Power, hp (hp) | 1,720 | 825 |
| Max cruise speed (km/h) | 709 | 391 |
| Approach speed (km/h) | 161 | 115 |
| Travel range (km) | 2,656 | 1,796 |
| Service ceiling (m) | 12,771 | 8,382 |
| Rate of climb (m/sec) | 16.26 | 5.44 |
| Take off distance (m) | 366 | - |
| Landing distance (m) | 457 | - |
| Weights | ||
| Max take off weight (kg) | 5,490 | 4,273 |
| Max landing weight (kg) | 5,490 | 3,390 |
| Max payload (kg) | 910 | 680 |
| Fuel tank capacity (l) | 1,018 | 1,401 |
| Dimensions | ||
| Seats | 1 | 2 |
| Exterior length (m) | 9.8 | 10.36 |
| Tail height (m) | 4.08 | 4.34 |
| Fuselage diameter (m) | 0.9 | 1.1 |
| Wing span (m) | 11.28 | 12.8 |
| Wing tips | No Winglets | No Winglets |
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