H135M / EC365 vs Mi-17 Hip-H

Overview

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).

H135M / EC365

European light utility helicopter, prominent in law enforcement, medical services, and military operations worldwide since the late 20th century.
Airbus Helicopters H135M / EC365 Helicopter profile drawing
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
→ View full H135M / EC365 details

Mi-17 Hip-H

Soviet transport helicopter, prominently deployed during Afghan War, globally used for cargo, troop transport, and rescue missions.
Mil Mi-17 Hip-H Helicopter profile drawing
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
→ View full Mi-17 Hip-H details

H135M / EC365

Wingspan 10.2 m ◉
Height 3.5 m ◉
Length 12.2 m ◉
Maximum speed 287 km/h ◉
Operational range 630 km ◉
Service ceiling 6,096 m ◉
Max. takeoff weight 2,900 kg ◉
Empty weight 1,490 kg ◉
Total thrust 2 x 260 kW ◉

Mi-17 Hip-H

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

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.

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