C-17 Globemaster III vs Kawasaki C-2
Overview
The C-17 Globemaster III and the Kawasaki C-2 are both Military Transport Aircraft, manufactured by McDonnell Douglas and Kawasaki Aerospace respectively.
Top speed is 930 km/h for the C-17 Globemaster III vs 920 km/h for the Kawasaki C-2. The C-17 Globemaster III has an operational range of 4,480 km vs 7,600 km for the Kawasaki C-2. The C-17 Globemaster III operates at altitudes up to 13,715 m compared to 13,100 m for the Kawasaki C-2.
The C-17 Globemaster III has been produced in 279 units vs 14 for the Kawasaki C-2. Unit cost is $340M for the C-17 Globemaster III vs $74.02M for the Kawasaki C-2. The C-17 Globemaster III first flew 19 years before the Kawasaki C-2 (1991 vs 2010).
| 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 |
| Japanese mid-size, twin-turbofan military transport aircraft, developed in the early 21st century and entered service in 2016, used for long-range, high-speed tactical and strategic airlift operations. | |
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| Origin country | π―π΅ Japan |
| Category | Military Transport Aircraft |
| Manufacturer | Kawasaki Aerospace |
| First flight | 26 January 2010 |
| Year introduced | 2016 |
| Number produced | 14 units |
| Average unit price | $74.0 million |
| 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 |
| Wing area | -- mΒ² |
| Wingspan | 44.4 m β |
| Height | 14.2 m β |
| Length | 43.9 m β |
| Maximum speed | 920 km/h β |
| Operational range | 7,600 km β |
| Service ceiling | 13,100 m β |
| Max. takeoff weight | 141,400 kg β |
| Empty weight | 69,000 kg β |
| Total thrust | 2 x 133 kN β |
Performance Radar Chart
Detailed Comparison
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