Mi-17 Hip-H vs UH-1N Twin Huey
Overview
The Mi-17 Hip-H and the UH-1N Twin Huey are both Military Helicopters, manufactured by Mil and Bell respectively.
Top speed is 250 km/h for the Mi-17 Hip-H vs 240 km/h for the UH-1N Twin Huey. The Mi-17 Hip-H has an operational range of 800 km vs 459 km for the UH-1N Twin Huey. The Mi-17 Hip-H operates at altitudes up to 6,000 m compared to 5,300 m for the UH-1N Twin Huey. At 13,000 kg MTOW, the Mi-17 Hip-H is 2.7x the UH-1N Twin Huey's 4,763 kg.
The UH-1N Twin Huey first flew 6 years before the Mi-17 Hip-H (1969 vs 1975).
| Soviet transport helicopter, prominently deployed during Afghan War, globally used for cargo, troop transport, and rescue missions. | |
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| Origin country | π¨π³ Ex-USSR |
| Category | Military Helicopters |
| Manufacturer | Mil |
| First flight | 1 January 1975 |
| Year introduced | 1977 |
| Number produced | 12000 units |
| Average unit price | $15 million |
| American medium military utility helicopter, introduced in the late 20th century, widely used for tactical transport, search and rescue, and close air support. | |
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| Origin country | πΊπΈ United States |
| Category | Military Helicopters |
| Manufacturer | Bell |
| First flight | 1 April 1969 |
| Year introduced | 1970 |
| Number produced | N/A |
| Average unit price | -- |
| Wing area | -- mΒ² |
| Wingspan | 21.3 m β |
| Height | 4.8 m β |
| Length | 18.5 m β |
| Maximum speed | 250 km/h β |
| Operational range | 800 km β |
| Service ceiling | 6,000 m β |
| Max. takeoff weight | 13,000 kg β |
| Empty weight | 7,489 kg |
| Total thrust | 2 x 746 kW β |
| Wing area | 168.0 mΒ² |
| Wingspan | 14.6 m β |
| Height | 4.4 m β |
| Length | 17.6 m β |
| Maximum speed | 240 km/h β |
| Operational range | 459 km β |
| Service ceiling | 5,300 m β |
| Max. takeoff weight | 4,763 kg β |
| Empty weight | -- kg |
| Total thrust | 2 x 465 kW β |
Performance Radar Chart
Detailed Comparison
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Frequently Asked Questions
Which is faster, the Mi-17 Hip-H or UH-1N Twin Huey?
The Mi-17 Hip-H is faster with a maximum speed of 250 km/h compared to the UH-1N Twin Huey's 240 km/h, a difference of 10 km/h.
Which has longer range, the Mi-17 Hip-H or UH-1N Twin Huey?
The Mi-17 Hip-H has a longer range at 800 km compared to the UH-1N Twin Huey's 459 km.
Which can fly higher, the Mi-17 Hip-H or UH-1N Twin Huey?
The Mi-17 Hip-H has a higher service ceiling at 6,000 meters (19,685 ft) compared to the UH-1N Twin Huey's 5,300 meters (17,388 ft).
Which is heavier, the Mi-17 Hip-H or UH-1N Twin Huey?
The Mi-17 Hip-H has a higher maximum takeoff weight at 13,000 kg compared to the UH-1N Twin Huey's 4,763 kg.
Which is larger, the Mi-17 Hip-H or UH-1N Twin Huey?
The Mi-17 Hip-H is longer at 18.5 meters compared to the UH-1N Twin Huey's 17.6 meters.
Which entered service first, the Mi-17 Hip-H or UH-1N Twin Huey?
The UH-1N Twin Huey entered service first in 1970, 7 years before the Mi-17 Hip-H which entered service in 1977.