C-160 Transall vs C-295 Persuader
Overview
The C-160 Transall and the C-295 Persuader are both Military Transport Aircraft, manufactured by Transall and Airbus respectively.
Top speed is 513 km/h for the C-160 Transall vs 576 km/h for the C-295 Persuader. The C-160 Transall has an operational range of 1,853 km vs 5,750 km for the C-295 Persuader. The C-160 Transall operates at altitudes up to 8,230 m compared to 7,620 m for the C-295 Persuader. At 51,000 kg MTOW, the C-160 Transall is 2.2x the C-295 Persuader's 23,200 kg.
The C-160 Transall has been produced in 214 units vs 209 for the C-295 Persuader. Unit cost is $12M for the C-160 Transall vs $78M for the C-295 Persuader. The C-160 Transall first flew 34 years before the C-295 Persuader (1963 vs 1997).
| 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 |
| Spanish tactical military transport aircraft, utilized globally in maritime patrol, surveillance, and humanitarian relief missions since the late 20th century. | |
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| Origin country | 🇪🇸 Spain 🇮🇩 Indonesia |
| Category | Military Transport Aircraft |
| Manufacturer | Airbus |
| First flight | 28 November 1997 |
| Year introduced | 2001 |
| Number produced | 209 units |
| Average unit price | $78 million |
| 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—‰ |
| Wing area | 59.0 m² ◉ |
| Wingspan | 25.8 m â—‰ |
| Height | 8.6 m â—‰ |
| Length | 24.5 m â—‰ |
| Maximum speed | 576 km/h â—‰ |
| Operational range | 5,750 km â—‰ |
| Service ceiling | 7,620 m â—‰ |
| Max. takeoff weight | 23,200 kg â—‰ |
| Empty weight | 9,250 kg â—‰ |
| Total thrust | 2 x 986 kW â—‰ |
Performance Radar Chart
Detailed Comparison
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