Ka-226 Hoodlum-C vs Mi-17 Hip-H
The Ka-226 Hoodlum-C and the Mi-17 Hip-H are both Military Helicopters, manufactured by Kamov and Mil respectively. Top speed is 205 km/h for the Ka-226 Hoodlum-C vs 250 km/h for the Mi-17 Hip-H. The Ka-226 Hoodlum-C has an operational range of 600 km vs 800 km for the Mi-17 Hip-H. The Ka-226 Hoodlum-C operates at altitudes up to 6,200 m compared to 6,000 m for the Mi-17 Hip-H. At 13,000 kg MTOW, the Mi-17 Hip-H is 3.8x the Ka-226 Hoodlum-C's 3,450 kg. The Ka-226 Hoodlum-C has been produced in 269 units vs 12,000 for the Mi-17 Hip-H. The Mi-17 Hip-H first flew 22 years before the Ka-226 Hoodlum-C (1975 vs 1997).
| Russian light utility helicopter, operational since late 20th century, frequently deployed for medical, policing and aerial work. | |
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| Origin country | 🇷🇺 Russia |
| Category | Military Helicopters |
| Manufacturer | Kamov |
| First flight | 4 September 1997 |
| Year introduced | 2002 |
| Number produced | 269 units |
| Average unit price | $-- 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 | 13.0 m â—‰ |
| Height | 4.2 m â—‰ |
| Length | 8.1 m â—‰ |
| Maximum speed | 205 km/h â—‰ |
| Operational range | 600 km â—‰ |
| Service ceiling | 6,200 m â—‰ |
| Max. takeoff weight | 3,450 kg â—‰ |
| Empty weight | 1,950 kg â—‰ |
| Total thrust | 2 x 336 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 Ka-226 Hoodlum-C or Mi-17 Hip-H?
The Mi-17 Hip-H is faster with a maximum speed of 250 km/h compared to the Ka-226 Hoodlum-C's 205 km/h, a difference of 45 km/h.
Which has longer range, the Ka-226 Hoodlum-C or Mi-17 Hip-H?
The Mi-17 Hip-H has a longer range at 800 km compared to the Ka-226 Hoodlum-C's 600 km.
Which can fly higher, the Ka-226 Hoodlum-C or Mi-17 Hip-H?
The Ka-226 Hoodlum-C has a higher service ceiling at 6,200 meters (20,341 ft) compared to the Mi-17 Hip-H's 6,000 meters (19,685 ft).
Which is heavier, the Ka-226 Hoodlum-C or Mi-17 Hip-H?
The Mi-17 Hip-H has a higher maximum takeoff weight at 13,000 kg compared to the Ka-226 Hoodlum-C's 3,450 kg.
Which is larger, the Ka-226 Hoodlum-C or Mi-17 Hip-H?
The Mi-17 Hip-H is longer at 18.5 meters compared to the Ka-226 Hoodlum-C's 8.1 meters.
Which entered service first, the Ka-226 Hoodlum-C or Mi-17 Hip-H?
The Mi-17 Hip-H entered service first in 1977, 25 years before the Ka-226 Hoodlum-C which entered service in 2002.
Which has been built in greater numbers, the Ka-226 Hoodlum-C or Mi-17 Hip-H?
The Mi-17 Hip-H has been produced in greater numbers with 12,000 units compared to 269 units of the Ka-226 Hoodlum-C.