| Attribute | Grumman F7F Tigercat × | Martin B-10 × |
|---|---|---|
| General | ||
| Manufacturer | Grumman | Glenn L. Martin Company |
| Model | Grumman F7F Tigercat | Martin B-10 |
| Country | United States | United States |
| Manufactured from (year) | 1943 | 1933 |
| Manufactured to (year) | 1946 | 1940 |
| Type | Military Propellor Planes | Military Propellor Planes |
| Icao | F7F | B10 |
| Performance | ||
| Engine | 2x Pratt & Whitney R-2800-34W Double Wasp | 2x Wright R-1820-33 Cyclone |
| Power, hp (hp) | 2,100 | 775 |
| Max cruise speed (km/h) | 741 | 343 |
| Approach speed (km/h) | 144 | - |
| Travel range (km) | 1,935 | 2,000 |
| Service ceiling (m) | 12,314 | 7,376 |
| Rate of climb (m/sec) | 23.01 | 7.01 |
| Take off distance (m) | 240 | - |
| Landing distance (m) | 270 | - |
| Weights | ||
| Max take off weight (kg) | 11,670 | 7,440 |
| Max payload (kg) | 2,000 | 1,025 |
| Fuel tank capacity (l) | 2,748 | 2,801 |
| Dimensions | ||
| Seats | 2 | 3 |
| Exterior length (m) | 13.84 | 13.64 |
| Tail height (m) | 5.05 | 4.7 |
| Fuselage diameter (m) | 1 | 1.3 |
| Wing span (m) | 15.7 | 21.5 |
| Wing tips | No Winglets | No Winglets |