C-17 Globemaster III vs DC-3
Overview
The C-17 Globemaster III and the DC-3 are both Military Transport Aircraft, manufactured by McDonnell Douglas and Douglas respectively.
The C-17 Globemaster III reaches 930 km/h β 2.3x the DC-3's 413 km/h. The C-17 Globemaster III has an operational range of 4,480 km vs 2,540 km for the DC-3. The C-17 Globemaster III operates at altitudes up to 13,715 m compared to 7,071 m for the DC-3. At 259,460 kg MTOW, the C-17 Globemaster III is 20:1 the DC-3's 13,154 kg.
The C-17 Globemaster III has been produced in 279 units vs 10,174 for the DC-3. Unit cost is $340M for the C-17 Globemaster III vs $0.08M for the DC-3. The DC-3 first flew 50 years before the C-17 Globemaster III (1941 vs 1991).
| 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 |
| American commercial airliner, renowned for significant contributions to World War II airlift operations, frequently used for cargo and passenger transport. | |
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| Origin country | πΊπΈ United States |
| Category | Military Transport Aircraft |
| Manufacturer | Douglas |
| First flight | 23 December 1941 |
| Year introduced | 1936 |
| Number produced | 10174 units |
| Average unit price | $80K |
| 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 |
| Wing area | 91.7 mΒ² β |
| Wingspan | 29.0 m β |
| Height | 5.6 m β |
| Length | 22.7 m β |
| Maximum speed | 413 km/h β |
| Operational range | 2,540 km β |
| Service ceiling | 7,071 m β |
| Max. takeoff weight | 13,154 kg β |
| Empty weight | 6,450 kg β |
| Total thrust | 3 x 292 kW β |
Performance Radar Chart
Detailed Comparison
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