Attribute | Grumman F7F Tigercat × | Douglas DC-1 × |
---|---|---|
General | ||
Manufacturer | Grumman | Douglas Aircraft Co. |
Model | Grumman F7F Tigercat | Douglas DC-1 |
Country | United States | United States |
Manufactured from (year) | 1943 | 1933 |
Manufactured to (year) | 1946 | 1933 |
Type | Military Propellor Planes | Passenger Turbo Props |
Icao | F7F | DC1 |
Performance | ||
Engine | 2x Pratt & Whitney R-2800-34W Double Wasp | 2x Wright SGR-1820F3 Cyclone |
Power, hp (hp) | 2,100 | 710 |
Max cruise speed (km/h) | 741 | 333 |
Approach speed (km/h) | 144 | - |
Travel range (km) | 1,935 | 1,611 |
Service ceiling (m) | 12,314 | 7,010 |
Rate of climb (m/sec) | 23.01 | 5.08 |
Take off distance (m) | 240 | - |
Landing distance (m) | 270 | - |
Weights | ||
Max take off weight (kg) | 11,670 | 7,938 |
Max payload (kg) | 2,000 | 1,800 |
Fuel tank capacity (l) | 2,748 | 3,028 |
Dimensions | ||
Seats | 2 | 14 |
Exterior length (m) | 13.84 | 18.3 |
Tail height (m) | 5.05 | - |
Fuselage diameter (m) | 1 | 2 |
Wing span (m) | 15.7 | 25.9 |
Wing tips | No Winglets | No Winglets |