An-26 Curl vs C-160 Transall
Overview
The An-26 Curl and the C-160 Transall are both Military Transport Aircraft, manufactured by Antonov and Transall respectively.
Top speed is 540 km/h for the An-26 Curl vs 513 km/h for the C-160 Transall. The An-26 Curl has an operational range of 1,100 km vs 1,853 km for the C-160 Transall. The C-160 Transall operates at altitudes up to 8,230 m compared to 7,500 m for the An-26 Curl. At 51,000 kg MTOW, the C-160 Transall is 2.1x the An-26 Curl's 24,000 kg.
The An-26 Curl has been produced in 1,403 units vs 214 for the C-160 Transall. Unit cost is $22M for the An-26 Curl vs $12M for the C-160 Transall. The C-160 Transall first flew 6 years before the An-26 Curl (1963 vs 1969).
| Soviet twin-engined transport aircraft, widely utilized in both civilian and military roles since the 1960s. | |
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| Origin country | 🇨🇳 Ex-USSR |
| Category | Military Transport Aircraft |
| Manufacturer | Antonov |
| First flight | 21 May 1969 |
| Year introduced | 1969 |
| Number produced | 1403 units |
| Average unit price | $22 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 | 75.0 m² ◉ |
| Wingspan | 29.2 m â—‰ |
| Height | 8.3 m â—‰ |
| Length | 23.8 m â—‰ |
| Maximum speed | 540 km/h â—‰ |
| Operational range | 1,100 km â—‰ |
| Service ceiling | 7,500 m â—‰ |
| Max. takeoff weight | 24,000 kg â—‰ |
| Empty weight | 15,000 kg â—‰ |
| Total thrust | 2 x 450 kgf 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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