| Attribute | Tupolev Tu-114 × | Douglas C-74 Globemaster × |
|---|---|---|
| General | ||
| Manufacturer | Tupolev | Douglas Aircraft Co. |
| Model | Tupolev Tu-114 | Douglas C-74 Globemaster |
| Country | Russia | United States |
| Manufactured from (year) | 1958 | 1945 |
| Manufactured to (year) | 1963 | 1947 |
| Type | Passenger Turbo Props | Military Transport Planes |
| Icao | TU114 | C74 |
| Performance | ||
| Engine | 4x Kuznetsov NK-12MV | 4x Pratt & Whitney R-4360-69 Wasp Major |
| Power, hp (hp) | 14,795 | 3,250 |
| Max cruise speed (km/h) | 880 | 528 |
| Travel range (km) | 8,945 | 5,556 |
| Service ceiling (m) | 11,887 | 6,492 |
| Rate of climb (m/sec) | 10.16 | 13.23 |
| Take off distance (m) | 2,500 | - |
| Landing distance (m) | 1,400 | - |
| Weights | ||
| Max take off weight (kg) | 171,000 | 78,000 |
| Max payload (kg) | 20,000 | 21,840 |
| Fuel tank capacity (l) | 72,983 | 41,639 |
| Dimensions | ||
| Seats | 23 | 13 |
| Exterior length (m) | 54.1 | 37.8 |
| Tail height (m) | 15.44 | 13.34 |
| Fuselage diameter (m) | 3.3 | 4.1 |
| Wing span (m) | 51.1 | 52.8 |
| Wing tips | No Winglets | No Winglets |