Comparison of Douglas A-1 Skyraider and Martin 187 Baltimore [S]ave
| Attribute |  Douglas A-1 Skyraider × |  Martin 187 Baltimore × |
|---|---|---|
| General | ||
| Manufacturer | Douglas Aircraft Co. | Glenn L. Martin Company |
| Model | Douglas A-1 Skyraider | Martin 187 Baltimore |
| Country | United States | United States |
| Manufactured from (year) | 1945 | 1941 |
| Manufactured to (year) | 1957 | 1944 |
| Type | Military Propellor Planes | Military Propellor Planes |
| Icao | A1 | - |
| Performance | ||
| Engine | 1x Wright R-3350-26WA Duplex-Cyclone | 2x Wright GR-2600-A5B |
| Power, hp (hp) | 2,700 | 1,700 |
| Max cruise speed (km/h) | 519 | 546 |
| Approach speed (km/h) | - | 189 |
| Travel range (km) | 2,437 | 1,574 |
| Service ceiling (m) | 8,687 | 7,315 |
| Rate of climb (m/sec) | 14.48 | 6.33 |
| Take off distance (m) | 400 | - |
| Landing distance (m) | 800 | - |
| Weights | ||
| Max take off weight (kg) | 11,340 | 10,900 |
| Max payload (kg) | 3,800 | 1,100 |
| Fuel tank capacity (l) | 1,438 | 1,855 |
| Dimensions | ||
| Seats | 1 | 4 |
| Exterior length (m) | 11.9 | 14.8 |
| Tail height (m) | 4.78 | 5.4 |
| Fuselage diameter (m) | 1.5 | 1.1 |
| Wing span (m) | 15.24 | 18.7 |
| Wing tips | No Winglets | No Winglets |
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