A400M Atlas vs C-160 Transall
Overview
The A400M Atlas and the C-160 Transall are both Military Transport Aircraft, manufactured by Airbus and Transall respectively.
Top speed is 780 km/h for the A400M Atlas vs 513 km/h for the C-160 Transall. The A400M Atlas has an operational range of 3,300 km vs 1,853 km for the C-160 Transall. The A400M Atlas operates at altitudes up to 12,500 m compared to 8,230 m for the C-160 Transall. At 141,000 kg MTOW, the A400M Atlas is 2.8x the C-160 Transall's 51,000 kg.
The A400M Atlas has been produced in 174 units vs 214 for the C-160 Transall. Unit cost is $152M for the A400M Atlas vs $12M for the C-160 Transall. The C-160 Transall first flew 46 years before the A400M Atlas (1963 vs 2009).
| European military transport aircraft, notable for strategic deployments in operations worldwide since the 2000s. | |
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| Origin country | 🇪🇺 Europe |
| Category | Military Transport Aircraft |
| Manufacturer | Airbus |
| First flight | 11 December 2009 |
| Year introduced | 2013 |
| Number produced | 174 units |
| Average unit price | $152 million |
| German-French transport plane, employed globally since the Cold War, essential for humanitarian aid, military logistical support, and troop transport. | |
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| Origin country | 🇩🇪 Germany 🇫🇷 France |
| Category | Military Transport Aircraft |
| Manufacturer | Transall |
| First flight | 25 February 1963 |
| Year introduced | 1967 |
| Number produced | 214 units |
| Average unit price | $12 million |
| Wing area | 221.5 m² ◉ |
| Wingspan | 42.4 m â—‰ |
| Height | 14.7 m â—‰ |
| Length | 45.1 m â—‰ |
| Maximum speed | 780 km/h â—‰ |
| Operational range | 3,300 km â—‰ |
| Service ceiling | 12,500 m â—‰ |
| Max. takeoff weight | 141,000 kg â—‰ |
| Empty weight | 66,500 kg â—‰ |
| Total thrust | 4 x 2,051 kW â—‰ |
| Wing area | 160.0 m² ◉ |
| Wingspan | 40.0 m â—‰ |
| Height | 11.7 m â—‰ |
| Length | 32.4 m â—‰ |
| Maximum speed | 513 km/h â—‰ |
| Operational range | 1,853 km â—‰ |
| Service ceiling | 8,230 m â—‰ |
| Max. takeoff weight | 51,000 kg â—‰ |
| Empty weight | 29,000 kg â—‰ |
| Total thrust | 2 x 2,275 kW â—‰ |
Performance Radar Chart
Detailed Comparison
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