Mi-8 Hip vs OH-6 Cayuse
Overview
The Mi-8 Hip and the OH-6 Cayuse are both Military Helicopters, manufactured by Mil and Hughes Helicopters respectively.
Top speed is 250 km/h for the Mi-8 Hip vs 240 km/h for the OH-6 Cayuse. The Mi-8 Hip has an operational range of 495 km vs 610 km for the OH-6 Cayuse. The OH-6 Cayuse operates at altitudes up to 4,800 m compared to 4,500 m for the Mi-8 Hip. At 12,000 kg MTOW, the Mi-8 Hip is 9.8x the OH-6 Cayuse's 1,225 kg.
The Mi-8 Hip has been produced in 17,000 units vs 1,422 for the OH-6 Cayuse. The Mi-8 Hip first flew 2 years before the OH-6 Cayuse (1961 vs 1963).
| 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 |
| American light observation helicopter, introduced in the mid-1960s, designed for personnel transport, escort, and observation missions. | |
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| Origin country | 🇺🇸 United States |
| Category | Military Helicopters |
| Manufacturer | Hughes Helicopters |
| First flight | 27 February 1963 |
| Year introduced | 1966 |
| Number produced | 1422 units |
| Average unit price | -- |
| Wing area | -- m² |
| Wingspan | 21.3 m ◉ |
| Height | 5.7 m ◉ |
| Length | 25.2 m ◉ |
| Maximum speed | 250 km/h ◉ |
| Operational range | 495 km ◉ |
| Service ceiling | 4,500 m ◉ |
| Max. takeoff weight | 12,000 kg ◉ |
| Empty weight | 7,160 kg ◉ |
| Total thrust | 2 x 560 kW ◉ |
| Wing area | 50.6 m² |
| Wingspan | 8.0 m ◉ |
| Height | 2.5 m ◉ |
| Length | 9.2 m ◉ |
| Maximum speed | 240 km/h ◉ |
| Operational range | 610 km ◉ |
| Service ceiling | 4,800 m ◉ |
| Max. takeoff weight | 1,225 kg ◉ |
| Empty weight | 557 kg ◉ |
| Total thrust | 1 x 236 kW ◉ |
Performance Radar Chart
Detailed Comparison
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Frequently Asked Questions
Which is faster, the Mi-8 Hip or OH-6 Cayuse?
The Mi-8 Hip is faster with a maximum speed of 250 km/h compared to the OH-6 Cayuse's 240 km/h, a difference of 10 km/h.
Which has longer range, the Mi-8 Hip or OH-6 Cayuse?
The OH-6 Cayuse has a longer range at 610 km compared to the Mi-8 Hip's 495 km.
Which can fly higher, the Mi-8 Hip or OH-6 Cayuse?
The OH-6 Cayuse has a higher service ceiling at 4,800 meters (15,748 ft) compared to the Mi-8 Hip's 4,500 meters (14,763 ft).
Which is heavier, the Mi-8 Hip or OH-6 Cayuse?
The Mi-8 Hip has a higher maximum takeoff weight at 12,000 kg compared to the OH-6 Cayuse's 1,225 kg.
Which is larger, the Mi-8 Hip or OH-6 Cayuse?
The Mi-8 Hip is longer at 25.2 meters compared to the OH-6 Cayuse's 9.2 meters.
Which entered service first, the Mi-8 Hip or OH-6 Cayuse?
The OH-6 Cayuse entered service first in 1966, 1 years before the Mi-8 Hip which entered service in 1967.
Which has been built in greater numbers, the Mi-8 Hip or OH-6 Cayuse?
The Mi-8 Hip has been produced in greater numbers with 17,000 units compared to 1,422 units of the OH-6 Cayuse.