Mi-17 Hip-H vs SA340 Gazelle
Overview
The Mi-17 Hip-H and the SA340 Gazelle are both Military Helicopters, manufactured by Mil and Aérospatiale respectively.
Top speed is 250 km/h for the Mi-17 Hip-H vs 310 km/h for the SA340 Gazelle. The Mi-17 Hip-H has an operational range of 800 km vs 361 km for the SA340 Gazelle. The Mi-17 Hip-H operates at altitudes up to 6,000 m compared to 4,450 m for the SA340 Gazelle. At 13,000 kg MTOW, the Mi-17 Hip-H is 6.2x the SA340 Gazelle's 2,100 kg.
The Mi-17 Hip-H has been produced in 12,000 units vs 1,775 for the SA340 Gazelle. Unit cost is $15M for the Mi-17 Hip-H vs $1.7M for the SA340 Gazelle. The SA340 Gazelle first flew 8 years before the Mi-17 Hip-H (1967 vs 1975).
| Soviet transport helicopter, prominently deployed during Afghan War, globally used for cargo, troop transport, and rescue missions. | |
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| Origin country | 🇨🇳 Ex-USSR |
| Category | Military Helicopters |
| Manufacturer | Mil |
| First flight | 1 January 1975 |
| Year introduced | 1977 |
| Number produced | 12000 units |
| Average unit price | $15 million |
| French light utility helicopter, known for its extensive use in military and civil applications since its 1960s introduction. | |
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| Origin country | 🇫🇷 France |
| Category | Military Helicopters |
| Manufacturer | Aérospatiale |
| First flight | 7 April 1967 |
| Year introduced | 1971 |
| Number produced | 1775 units |
| Average unit price | $1.7 million |
| Wingspan | 21.3 m ◉ |
| Height | 4.8 m ◉ |
| Length | 18.5 m ◉ |
| Maximum speed | 250 km/h ◉ |
| Operational range | 800 km ◉ |
| Service ceiling | 6,000 m ◉ |
| Max. takeoff weight | 13,000 kg ◉ |
| Empty weight | 7,489 kg ◉ |
| Total thrust | 2 x 746 kW ◉ |
| Wingspan | 10.5 m ◉ |
| Height | 3.2 m ◉ |
| Length | 11.9 m ◉ |
| Maximum speed | 310 km/h ◉ |
| Operational range | 361 km ◉ |
| Service ceiling | 4,450 m ◉ |
| Max. takeoff weight | 2,100 kg ◉ |
| Empty weight | 1,009 kg ◉ |
| Total thrust | 1 x 650 kW ◉ |
Performance Radar Chart
Detailed Comparison
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