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 |