An-2 Colt vs C-17 Globemaster III
Overview
The An-2 Colt and the C-17 Globemaster III are both Military Transport Aircraft, manufactured by Antonov and McDonnell Douglas respectively.
The C-17 Globemaster III reaches 930 km/h β 3.6x the An-2 Colt's 258 km/h. The An-2 Colt has an operational range of 845 km vs 4,480 km for the C-17 Globemaster III. The C-17 Globemaster III operates at altitudes up to 13,715 m compared to 4,500 m for the An-2 Colt. At 259,460 kg MTOW, the C-17 Globemaster III is 48:1 the An-2 Colt's 5,440 kg.
The An-2 Colt has been produced in 18,000 units vs 279 for the C-17 Globemaster III. Unit cost is $0.1M for the An-2 Colt vs $340M for the C-17 Globemaster III. The An-2 Colt first flew 44 years before the C-17 Globemaster III (1947 vs 1991).
| Soviet single-engine biplane aircraft, mass-produced since 1947, remaining in service for military and civilian operations. | |
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| Origin country | π¨π³ Ex-USSR |
| Category | Military Transport Aircraft |
| Manufacturer | Antonov |
| First flight | 31 August 1947 |
| Year introduced | 1947 |
| Number produced | 18000 units |
| Average unit price | $100K |
| American military transport aircraft, extensively deployed in global conflict zones since the 1990s for strategic airlift missions. | |
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| Origin country | πΊπΈ United States |
| Category | Military Transport Aircraft |
| Manufacturer | McDonnell Douglas |
| First flight | 15 September 1991 |
| Year introduced | 1993 |
| Number produced | 279 units |
| Average unit price | $340 million |
| Wing area | 71.5 mΒ² β |
| Wingspan | 18.2 m β |
| Height | 4.1 m β |
| Length | 12.4 m β |
| Maximum speed | 258 km/h β |
| Operational range | 845 km β |
| Service ceiling | 4,500 m β |
| Max. takeoff weight | 5,440 kg β |
| Empty weight | 3,300 kg β |
| Total thrust | 1 x 750 kW β |
| Wing area | 353.0 mΒ² β |
| Wingspan | 51.8 m β |
| Height | 16.8 m β |
| Length | 53.0 m β |
| Maximum speed | 930 km/h β |
| Operational range | 4,480 km β |
| Service ceiling | 13,715 m β |
| Max. takeoff weight | 259,460 kg β |
| Empty weight | 122,000 kg β |
| Total thrust | 4 x 4,727 kgf β |
Performance Radar Chart
Detailed Comparison
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