An-178 vs C-17 Globemaster III
Overview
The An-178 and the C-17 Globemaster III are both Military Transport Aircraft, manufactured by Antonov and McDonnell Douglas respectively.
Top speed is 990 km/h for the An-178 vs 930 km/h for the C-17 Globemaster III. The An-178 has an operational range of 3,680 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 12,000 m for the An-178. At 259,460 kg MTOW, the C-17 Globemaster III is 5.1x the An-178's 51,000 kg.
The An-178 has been produced in 1 units vs 279 for the C-17 Globemaster III. Unit cost is $35M for the An-178 vs $340M for the C-17 Globemaster III. The C-17 Globemaster III first flew 24 years before the An-178 (1991 vs 2015).
| Ukrainian transport aircraft, developed in the 21st century, notable for international commercial and military cargo roles. | |
|
|
| Origin country | πΊπ¦ Ukraine |
| Category | Military Transport Aircraft |
| Manufacturer | Antonov |
| First flight | 7 May 2015 |
| Year introduced | 2023 |
| Number produced | 1 units |
| Average unit price | $35 million |
| American military transport aircraft, extensively deployed in global conflict zones since the 1990s for strategic airlift missions. | |
|
|
| 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 | -- mΒ² |
| Wingspan | 30.6 m β |
| Height | 9.6 m β |
| Length | 32.2 m β |
| Maximum speed | 990 km/h β |
| Operational range | 3,680 km β |
| Service ceiling | 12,000 m β |
| Max. takeoff weight | 51,000 kg β |
| Empty weight | 18,350 kg β |
| Total thrust | 2 x 3,751 kgf β |
| Wing area | 353.0 mΒ² |
| 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
Generating comparison analysis...
Unable to generate comparison at this time.