Ka-226 Hoodlum-C vs Mi-8 Hip
The Ka-226 Hoodlum-C and the Mi-8 Hip 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-8 Hip. The Ka-226 Hoodlum-C has an operational range of 600 km vs 495 km for the Mi-8 Hip. The Ka-226 Hoodlum-C operates at altitudes up to 6,200 m compared to 4,500 m for the Mi-8 Hip. At 12,000 kg MTOW, the Mi-8 Hip is 3.5x the Ka-226 Hoodlum-C's 3,450 kg. The Ka-226 Hoodlum-C has been produced in 269 units vs 17,000 for the Mi-8 Hip. The Mi-8 Hip first flew 36 years before the Ka-226 Hoodlum-C (1961 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 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 | 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 | 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 Ka-226 Hoodlum-C or Mi-8 Hip?
The Mi-8 Hip 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-8 Hip?
The Ka-226 Hoodlum-C has a longer range at 600 km compared to the Mi-8 Hip's 495 km.
Which can fly higher, the Ka-226 Hoodlum-C or Mi-8 Hip?
The Ka-226 Hoodlum-C has a higher service ceiling at 6,200 meters (20,341 ft) compared to the Mi-8 Hip's 4,500 meters (14,763 ft).
Which is heavier, the Ka-226 Hoodlum-C or Mi-8 Hip?
The Mi-8 Hip has a higher maximum takeoff weight at 12,000 kg compared to the Ka-226 Hoodlum-C's 3,450 kg.
Which is larger, the Ka-226 Hoodlum-C or Mi-8 Hip?
The Mi-8 Hip is longer at 25.2 meters compared to the Ka-226 Hoodlum-C's 8.1 meters.
Which entered service first, the Ka-226 Hoodlum-C or Mi-8 Hip?
The Mi-8 Hip entered service first in 1967, 35 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-8 Hip?
The Mi-8 Hip has been produced in greater numbers with 17,000 units compared to 269 units of the Ka-226 Hoodlum-C.