DHC-5 Buffalo vs V-22 Osprey
Overview
The DHC-5 Buffalo and the V-22 Osprey are both Military Transport Aircraft, manufactured by De Havilland Canada and Bell/Boeing respectively.
Top speed is 467 km/h for the DHC-5 Buffalo vs 565 km/h for the V-22 Osprey. The DHC-5 Buffalo has an operational range of 1,100 km vs 1,628 km for the V-22 Osprey. The DHC-5 Buffalo operates at altitudes up to 9,449 m compared to 7,925 m for the V-22 Osprey. At 60,500 kg MTOW, the V-22 Osprey is 2.7x the DHC-5 Buffalo's 22,317 kg.
The DHC-5 Buffalo has been produced in 122 units vs 400 for the V-22 Osprey. Unit cost is $25M for the DHC-5 Buffalo vs $72M for the V-22 Osprey. The DHC-5 Buffalo first flew 25 years before the V-22 Osprey (1964 vs 1989).
| Canadian tactical transport aircraft, primarily utilized during the 1960s, notably deployed for civilian and military air-drop operations. | |
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| Origin country | π¨π¦ Canada |
| Category | Military Transport Aircraft |
| Manufacturer | De Havilland Canada |
| First flight | 9 April 1964 |
| Year introduced | 1965 |
| Number produced | 122 units |
| Average unit price | $25 million |
| American tiltrotor military aircraft, known for operations in Iraq and Afghanistan, employed for transport and evacuation tasks. | |
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| Origin country | πΊπΈ United States |
| Category | Military Transport Aircraft |
| Manufacturer | Bell/Boeing |
| First flight | 19 March 1989 |
| Year introduced | 2006 |
| Number produced | 400 units |
| Average unit price | $72 million |
| Wing area | 88.0 mΒ² β |
| Wingspan | 29.0 m β |
| Height | 8.8 m β |
| Length | 24.0 m β |
| Maximum speed | 467 km/h β |
| Operational range | 1,100 km β |
| Service ceiling | 9,449 m β |
| Max. takeoff weight | 22,317 kg β |
| Empty weight | 11,412 kg β |
| Total thrust | 2 x 1,168 kW β |
| Wing area | 28.0 mΒ² β |
| Wingspan | 14.0 m β |
| Height | 6.7 m β |
| Length | 17.5 m β |
| Maximum speed | 565 km/h β |
| Operational range | 1,628 km β |
| Service ceiling | 7,925 m β |
| Max. takeoff weight | 60,500 kg β |
| Empty weight | 33,140 kg β |
| Total thrust | 2 x 2,293 kW β |
Performance Radar Chart
Detailed Comparison
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