H135M / EC365 vs Mi-8 Hip
The H135M / EC365 and the Mi-8 Hip 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-8 Hip. The H135M / EC365 has an operational range of 630 km vs 495 km for the Mi-8 Hip. The H135M / EC365 operates at altitudes up to 6,096 m compared to 4,500 m for the Mi-8 Hip. At 12,000 kg MTOW, the Mi-8 Hip is 4.1x the H135M / EC365's 2,900 kg. The H135M / EC365 has been produced in 1,400 units vs 17,000 for the Mi-8 Hip. Unit cost is $12M for the H135M / EC365 vs $4M for the Mi-8 Hip. The Mi-8 Hip first flew 33 years before the H135M / EC365 (1961 vs 1994).
| European light utility helicopter, prominent in law enforcement, medical services, and military operations worldwide since the late 20th century. | |
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| 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 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 |
| 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 | 5.7 m â—‰ |
| Length | 25.2 m â—‰ |
| Maximum speed | 250 km/h â—‰ |
| Operational range | 495 km â—‰ |
| Service ceiling | 4,500 m â—‰ |
| Max. takeoff weight | 12,000 kg â—‰ |
| Empty weight | 7,160 kg â—‰ |
| Total thrust | 2 x 1,119 kW â—‰ |
Performance Radar Chart
Frequently Asked Questions
Which is faster, the H135M / EC365 or Mi-8 Hip?
The H135M / EC365 is faster with a maximum speed of 287 km/h compared to the Mi-8 Hip's 250 km/h, a difference of 37 km/h.
Which has longer range, the H135M / EC365 or Mi-8 Hip?
The H135M / EC365 has a longer range at 630 km compared to the Mi-8 Hip's 495 km.
Which can fly higher, the H135M / EC365 or Mi-8 Hip?
The H135M / EC365 has a higher service ceiling at 6,096 meters (20,000 ft) compared to the Mi-8 Hip's 4,500 meters (14,763 ft).
Which is heavier, the H135M / EC365 or Mi-8 Hip?
The Mi-8 Hip has a higher maximum takeoff weight at 12,000 kg compared to the H135M / EC365's 2,900 kg.
Which is larger, the H135M / EC365 or Mi-8 Hip?
The Mi-8 Hip is longer at 25.2 meters compared to the H135M / EC365's 12.2 meters.
Which is more expensive, the H135M / EC365 or Mi-8 Hip?
The H135M / EC365 is more expensive at approximately $12 million per unit compared to the Mi-8 Hip at $4.0 million.
Which entered service first, the H135M / EC365 or Mi-8 Hip?
The Mi-8 Hip entered service first in 1967, 29 years before the H135M / EC365 which entered service in 1996.
Which has been built in greater numbers, the H135M / EC365 or Mi-8 Hip?
The Mi-8 Hip has been produced in greater numbers with 17,000 units compared to 1,400 units of the H135M / EC365.