Comparison of Bell AH-1 SuperCobra and LTV XC-142 [S]ave
| Attribute |  LTV XC-142 × |  Bell AH-1 SuperCobra × |
|---|---|---|
| General | ||
| Manufacturer | Vought | Bell Helicopter |
| Model | LTV XC-142 | Bell AH-1 SuperCobra |
| Country | United States | United States |
| Manufactured from (year) | 1964 | 1966 |
| Manufactured to (year) | 1966 | - |
| Type | Tilt Rotors | Military Helicopters |
| Icao | XC142 | SUCO |
| Performance | ||
| Engine | 4x General Electric T64-GE-1 | 2x General Electric T700-GE-401 |
| Power, hp (hp) | 2,850 | 1,690 |
| Avionics | - | Northrop Grumman |
| Max cruise speed (km/h) | 695 | 352 |
| Travel range (km) | 6,112 | 587 |
| Service ceiling (m) | 7,620 | 4,572 |
| Rate of climb (m/sec) | 34.54 | 8.2 |
| Weights | ||
| Max take off weight (kg) | 20,185 | 6,690 |
| Max landing weight (kg) | 15,637 | 6,690 |
| Max payload (kg) | 4,000 | 2,065 |
| Fuel tank capacity (l) | 5,300 | 1,741 |
| Dimensions | ||
| Seats | 32 | 3 |
| Cabin height (m) | 2.1 | - |
| Cabin width (m) | 2.3 | - |
| Cabin length (m) | 9.1 | - |
| Exterior length (m) | 17.7 | 17.7 |
| Tail height (m) | 7.95 | 4.44 |
| Fuselage diameter (m) | 2.6 | 2.2 |
| Wing span (m) | 20.6 | 13.4 |
| Wing tips | No Winglets | No Winglets |
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