| Attribute | Martin 2-0-2 × | Vickers VC.1 Viking × |
|---|---|---|
| General | ||
| Manufacturer | Glenn L. Martin Company | Vickers-Armstrongs |
| Model | Martin 2-0-2 | Vickers VC.1 Viking |
| Country | United States | United Kingdom |
| Manufactured from (year) | 1946 | 1945 |
| Manufactured to (year) | 1948 | 1954 |
| Type | Passenger Turbo Props | Passenger Turbo Props |
| Icao | - | VC1 |
| Performance | ||
| Engine | 2x Pratt & Whitney R-2800 CA-18 Double Wasp | 2x Bristol Hercules 634 |
| Power, hp (hp) | 2,400 | 1,690 |
| Max cruise speed (km/h) | 500 | 424 |
| Approach speed (km/h) | 122 | - |
| Travel range (km) | 1,022 | 2,778 |
| Service ceiling (m) | 10,058 | 7,620 |
| Rate of climb (m/sec) | 11.18 | 7.62 |
| Take off distance (m) | 477 | 780 |
| Landing distance (m) | 520 | 1,200 |
| Weights | ||
| Max take off weight (kg) | 18,098 | 15,422 |
| Max payload (kg) | 4,200 | 2,500 |
| Fuel tank capacity (l) | 6,587 | 3,369 |
| Dimensions | ||
| Seats | 4 | 26 |
| Exterior length (m) | 21.74 | 19.86 |
| Tail height (m) | 8.66 | 5.97 |
| Fuselage diameter (m) | 2.8 | 2.6 |
| Wing span (m) | 28.42 | 27.2 |
| Wing tips | No Winglets | No Winglets |