Attribute | Lockheed EC-130H Compass Call × | Douglas C-124 Globemaster II × |
---|---|---|
General | ||
Manufacturer | Lockheed Martin Aeronautics | Douglas Aircraft Co. |
Model | Lockheed EC-130H Compass Call | Douglas C-124 Globemaster II |
Country | United States | United States |
Manufactured from (year) | 1982 | 1949 |
Manufactured to (year) | - | 1955 |
Type | Military Propellor Planes | Military Transport Planes |
Icao | C130 | C124 |
Performance | ||
Engine | 4x Allison T56-A-15 | 4x Pratt & Whitney R-4360-63A Wasp Major |
Power, hp (hp) | 4,590 | 3,800 |
Max cruise speed (km/h) | 593 | 489 |
Approach speed (km/h) | 185 | - |
Travel range (km) | 4,250 | 6,482 |
Service ceiling (m) | 7,620 | 7,010 |
Rate of climb (m/sec) | 9.3 | 3.86 |
Take off distance (m) | 1,433 | - |
Landing distance (m) | 2,550 | - |
Weights | ||
Max take off weight (kg) | 70,000 | 88,224 |
Max landing weight (kg) | 58,967 | 88,224 |
Max payload (kg) | 45,000 | 34,000 |
Fuel tank capacity (l) | 37,854 | 42,124 |
Dimensions | ||
Seats | 13 | 7 |
Cabin height (m) | 2.7 | - |
Cabin width (m) | 3.1 | - |
Cabin length (m) | 12.2 | 23 |
Exterior length (m) | 29.79 | 39.8 |
Tail height (m) | 11.66 | 14.74 |
Fuselage diameter (m) | 4.2 | 4.5 |
Wing span (m) | 40.41 | 53.06 |
Wing tips | No Winglets | No Winglets |