H145M / EC645 vs Mi-17 Hip-H
Overview
The H145M / EC645 and the Mi-17 Hip-H are both Military Helicopters, manufactured by Airbus Helicopters and Mil respectively.
Top speed is 269 km/h for the H145M / EC645 vs 250 km/h for the Mi-17 Hip-H. The H145M / EC645 has an operational range of 660 km vs 800 km for the Mi-17 Hip-H. The Mi-17 Hip-H operates at altitudes up to 6,000 m compared to 5,486 m for the H145M / EC645. At 13,000 kg MTOW, the Mi-17 Hip-H is 3.6x the H145M / EC645's 3,585 kg.
The H145M / EC645 has been produced in 1,500 units vs 12,000 for the Mi-17 Hip-H. Unit cost is $25M for the H145M / EC645 vs $15M for the Mi-17 Hip-H. The Mi-17 Hip-H first flew 24 years before the H145M / EC645 (1975 vs 1999).
| German utility helicopter, recognized for military application and primarily used for search and rescue, medical evacuation, and troop transportation. | |
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| Origin country | 🇫🇷 France |
| Category | Military Helicopters |
| Manufacturer | Airbus Helicopters |
| First flight | 12 June 1999 |
| Year introduced | 2002 |
| Number produced | 1500 units |
| Average unit price | $25 million |
| 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 |
| Wingspan | 10.8 m ◉ |
| Height | 3.5 m ◉ |
| Length | 13.0 m ◉ |
| Maximum speed | 269 km/h ◉ |
| Operational range | 660 km ◉ |
| Service ceiling | 5,486 m ◉ |
| Max. takeoff weight | 3,585 kg ◉ |
| Empty weight | 1,792 kg ◉ |
| Total thrust | 2 x 275 kW ◉ |
| 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 ◉ |
Performance Radar Chart
Detailed Comparison
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