Mi-8 Hip vs SA316 Alouette III
Overview
The Mi-8 Hip and the SA316 Alouette III are both Military Helicopters, manufactured by Mil and Sud Aviation respectively.
Top speed is 250 km/h for the Mi-8 Hip vs 210 km/h for the SA316 Alouette III. The Mi-8 Hip has an operational range of 495 km vs 540 km for the SA316 Alouette III. The Mi-8 Hip operates at altitudes up to 4,500 m compared to 3,200 m for the SA316 Alouette III. At 12,000 kg MTOW, the Mi-8 Hip is 5.5x the SA316 Alouette III's 2,200 kg.
The Mi-8 Hip has been produced in 17,000 units vs 2,000 for the SA316 Alouette III. Unit cost is $4M for the Mi-8 Hip vs $1.5M for the SA316 Alouette III. The SA316 Alouette III first flew 2 years before the Mi-8 Hip (1959 vs 1961).
| Soviet multipurpose helicopter, prevalent during the Cold War, extensively utilized for transport, combat and humanitarian operations globally. | |
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| Origin country | 🇨🇳 Ex-USSR |
| Category | Military Helicopters |
| Manufacturer | Mil |
| First flight | 24 June 1961 |
| Year introduced | 1967 |
| Number produced | 17000 units |
| Average unit price | $4 million |
| French utility helicopter, popular in the Cold War-era, extensively utilized for search and rescue, and light transport roles. | |
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| Origin country | 🇫🇷 France |
| Category | Military Helicopters |
| Manufacturer | Sud Aviation |
| First flight | 28 February 1959 |
| Year introduced | 1961 |
| Number produced | 2000 units |
| Average unit price | $1.5 million |
| Wingspan | 21.3 m ◉ |
| Height | 5.7 m ◉ |
| Length | 25.2 m ◉ |
| Maximum speed | 250 km/h ◉ |
| Operational range | 495 km ◉ |
| Service ceiling | 4,500 m ◉ |
| Max. takeoff weight | 12,000 kg ◉ |
| Empty weight | 7,160 kg ◉ |
| Total thrust | 2 x 560 kW ◉ |
| Wingspan | 11.0 m ◉ |
| Height | 3.0 m ◉ |
| Length | 10.0 m ◉ |
| Maximum speed | 210 km/h ◉ |
| Operational range | 540 km ◉ |
| Service ceiling | 3,200 m ◉ |
| Max. takeoff weight | 2,200 kg ◉ |
| Empty weight | 1,143 kg ◉ |
| Total thrust | 1 x 713 kW ◉ |
Performance Radar Chart
Detailed Comparison
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