737 vs C-17 Globemaster III
Overview
The 737 and the C-17 Globemaster III are both Military Transport Aircraft, manufactured by Boeing and McDonnell Douglas respectively.
Top speed is 904 km/h for the 737 vs 930 km/h for the C-17 Globemaster III. The 737 has an operational range of 4,800 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 11,278 m for the 737. At 259,460 kg MTOW, the C-17 Globemaster III is 5.0x the 737's 52,163 kg.
The 737 has been produced in 11,535 units vs 279 for the C-17 Globemaster III. Unit cost is $115M for the 737 vs $340M for the C-17 Globemaster III. The 737 first flew 24 years before the C-17 Globemaster III (1967 vs 1991).
| American twin-engine narrow-body jet airliner, popularly deployed for commercial aviation since the late 1960s. | |
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| Origin country | πΊπΈ United States |
| Category | Military Transport Aircraft |
| Manufacturer | Boeing |
| First flight | 9 April 1967 |
| Year introduced | 1968 |
| Number produced | 11535 units |
| Average unit price | $115 million |
| 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 | 91.0 mΒ² β |
| Wingspan | 28.0 m β |
| Height | 11.0 m β |
| Length | 30.0 m β |
| Maximum speed | 904 km/h β |
| Operational range | 4,800 km β |
| Service ceiling | 11,278 m β |
| Max. takeoff weight | 52,163 kg β |
| Empty weight | 29,071 kg β |
| Total thrust | 2 x 3,289 kgf 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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