Ka-50 Hokum "Black Shark" vs UH-1 Iroquois "Huey"
Overview
The Ka-50 Hokum "Black Shark" and the UH-1 Iroquois "Huey" are both Military Helicopters, manufactured by Kamov and Bell respectively.
Top speed is 315 km/h for the Ka-50 Hokum "Black Shark" vs 222 km/h for the UH-1 Iroquois "Huey". The Ka-50 Hokum "Black Shark" has an operational range of 460 km vs 510 km for the UH-1 Iroquois "Huey". The UH-1 Iroquois "Huey" operates at altitudes up to 5,910 m compared to 5,500 m for the Ka-50 Hokum "Black Shark". At 10,800 kg MTOW, the Ka-50 Hokum "Black Shark" is 2.5x the UH-1 Iroquois "Huey"'s 4,309 kg.
The Ka-50 Hokum "Black Shark" has been produced in 19 units vs 16,000 for the UH-1 Iroquois "Huey". Unit cost is $16M for the Ka-50 Hokum "Black Shark" vs $1.3M for the UH-1 Iroquois "Huey". The UH-1 Iroquois "Huey" first flew 26 years before the Ka-50 Hokum "Black Shark" (1956 vs 1982).
| Soviet attack helicopter, distinctive for service during the Chechen conflicts, primarily used for reconnaissance and direct fire support. | |
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| Origin country | 🇨🇳 Ex-USSR |
| Category | Military Helicopters |
| Manufacturer | Kamov |
| First flight | 17 June 1982 |
| Year introduced | 1995 |
| Number produced | 19 units |
| Average unit price | $16 million |
| American utility helicopter, essential in the Vietnam War, extensively employed for medevac, transport, and combat operations. | |
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| Origin country | 🇺🇸 United States |
| Category | Military Helicopters |
| Manufacturer | Bell |
| First flight | 22 October 1956 |
| Year introduced | 1959 |
| Number produced | 16000 units |
| Average unit price | $1.3 million |
| Wingspan | 14.5 m ◉ |
| Height | 4.9 m ◉ |
| Length | 16.0 m ◉ |
| Maximum speed | 315 km/h ◉ |
| Operational range | 460 km ◉ |
| Service ceiling | 5,500 m ◉ |
| Max. takeoff weight | 10,800 kg ◉ |
| Empty weight | 7,700 kg ◉ |
| Total thrust | 2 x 821 kW ◉ |
| Wingspan | 14.6 m ◉ |
| Height | 4.5 m ◉ |
| Length | 12.7 m ◉ |
| Maximum speed | 222 km/h ◉ |
| Operational range | 510 km ◉ |
| Service ceiling | 5,910 m ◉ |
| Max. takeoff weight | 4,309 kg ◉ |
| Empty weight | 2,087 kg ◉ |
| Total thrust | 1 x 820 kW ◉ |
Performance Radar Chart
Detailed Comparison
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