H135M / EC365 vs Mi-17 Hip-H
The H135M / EC365 and the Mi-17 Hip-H are both Military Helicopters, manufactured by Airbus Helicopters and Mil respectively. Top speed is 287 km/h for the H135M / EC365 vs 250 km/h for the Mi-17 Hip-H. The H135M / EC365 has an operational range of 630 km vs 800 km for the Mi-17 Hip-H. The H135M / EC365 operates at altitudes up to 6,096 m compared to 6,000 m for the Mi-17 Hip-H. At 13,000 kg MTOW, the Mi-17 Hip-H is 4.5x the H135M / EC365's 2,900 kg. The H135M / EC365 has been produced in 1,400 units vs 12,000 for the Mi-17 Hip-H. Unit cost is $12M for the H135M / EC365 vs $15M for the Mi-17 Hip-H. The Mi-17 Hip-H first flew 19 years before the H135M / EC365 (1975 vs 1994).
| European light utility helicopter, prominent in law enforcement, medical services, and military operations worldwide since the late 20th century. | |
|
|
| Origin country | 🇫🇷 France |
| Category | Military Helicopters |
| Manufacturer | Airbus Helicopters |
| First flight | 15 February 1994 |
| Year introduced | 1996 |
| Number produced | 1400 units |
| Average unit price | $12 million |
| Soviet transport helicopter, prominently deployed during Afghan War, globally used for cargo, troop transport, and rescue missions. | |
|
|
| 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 | 10.2 m â—‰ |
| Height | 3.5 m â—‰ |
| Length | 12.2 m â—‰ |
| Maximum speed | 287 km/h â—‰ |
| Operational range | 630 km â—‰ |
| Service ceiling | 6,096 m â—‰ |
| Max. takeoff weight | 2,900 kg â—‰ |
| Empty weight | 1,490 kg â—‰ |
| Total thrust | 2 x 519 kW â—‰ |
| Wingspan | 21.3 m â—‰ |
| Height | 4.8 m â—‰ |
| Length | 18.5 m â—‰ |
| Maximum speed | 250 km/h â—‰ |
| Operational range | 800 km â—‰ |
| Service ceiling | 6,000 m â—‰ |
| Max. takeoff weight | 13,000 kg â—‰ |
| Empty weight | 7,489 kg â—‰ |
| Total thrust | 2 x 1,491 kW â—‰ |
Performance Radar Chart
Frequently Asked Questions
Which is faster, the H135M / EC365 or Mi-17 Hip-H?
The H135M / EC365 is faster with a maximum speed of 287 km/h compared to the Mi-17 Hip-H's 250 km/h, a difference of 37 km/h.
Which has longer range, the H135M / EC365 or Mi-17 Hip-H?
The Mi-17 Hip-H has a longer range at 800 km compared to the H135M / EC365's 630 km.
Which can fly higher, the H135M / EC365 or Mi-17 Hip-H?
The H135M / EC365 has a higher service ceiling at 6,096 meters (20,000 ft) compared to the Mi-17 Hip-H's 6,000 meters (19,685 ft).
Which is heavier, the H135M / EC365 or Mi-17 Hip-H?
The Mi-17 Hip-H has a higher maximum takeoff weight at 13,000 kg compared to the H135M / EC365's 2,900 kg.
Which is larger, the H135M / EC365 or Mi-17 Hip-H?
The Mi-17 Hip-H is longer at 18.5 meters compared to the H135M / EC365's 12.2 meters.
Which is more expensive, the H135M / EC365 or Mi-17 Hip-H?
The Mi-17 Hip-H is more expensive at approximately $15 million per unit compared to the H135M / EC365 at $12 million.
Which entered service first, the H135M / EC365 or Mi-17 Hip-H?
The Mi-17 Hip-H entered service first in 1977, 19 years before the H135M / EC365 which entered service in 1996.
Which has been built in greater numbers, the H135M / EC365 or Mi-17 Hip-H?
The Mi-17 Hip-H has been produced in greater numbers with 12,000 units compared to 1,400 units of the H135M / EC365.