Attribute | ![]() Airbus A400M × | ![]() Lockheed Martin C-130J Super Hercules × |
---|---|---|
General | ||
Manufacturer | Airbus | Lockheed Martin Aeronautics |
Model | Airbus A400M | Lockheed Martin C-130J Super Hercules |
Country | France | United States |
Manufactured from (year) | 2009 | 1996 |
Type | Military Propellor Planes | Military Transport Planes |
Icao | A400 | C130 |
Performance | ||
Engine | 4x 4 × EuroProp International TP400-D6 | 4x Rolls-Royce AE 2100D3 |
Power, hp (hp) | 11,000 | 4,700 |
Avionics | - | Lockheed C-130X AMP Avionics |
Max cruise speed (km/h) | 780 | 676 |
Approach speed (km/h) | 241 | 222 |
Travel range (km) | 8,890 | 4,426 |
Fuel economy (km/l) | 0.083 | 0.108 |
Service ceiling (m) | 12,192 | 10,058 |
Rate of climb (m/sec) | 15.24 | 9.3 |
Take off distance (m) | 980 | 1,573 |
Landing distance (m) | 770 | 792 |
Weights | ||
Max take off weight (kg) | 141,000 | 79,365 |
Max landing weight (kg) | 123,000 | 58,957 |
Max payload (kg) | 37,000 | 21,500 |
Fuel tank capacity (l) | 62,879 | 36,643 |
Baggage volume (m³) | 342 | 170 |
Dimensions | ||
Seats | 116 | 92 |
Cabin height (m) | 3.85 | 2.74 |
Cabin width (m) | 4 | 3.12 |
Cabin length (m) | 17.71 | 16.9 |
Exterior length (m) | 43.8 | 34.37 |
Tail height (m) | 14.7 | 11.84 |
Fuselage diameter (m) | 4.1 | 4.32 |
Wing span (m) | 42.4 | 40.4 |
Wing tips | No Winglets | No Winglets |