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Kamov Ka-52

Lighter-Than-Air Craft and Rotorcraft

The Kamov Ka-52 Alligator, NATO reporting name Hokum B, is a twin-engined, two-seat combat helicopter with coaxial counter-rotating rotors, developed by the Kamov design bureau as the side-by-side, two-crew development of the single-seat Ka-50 Black Shark. The second crew member operates the reconnaissance and target designation suite, and both pilots sit on ejection seats. Compared with the Ka-50 it has a new nose radome carrying a targeting radar, a day and night television and thermal sighting turret under the nose, and six wing hardpoints instead of four. It first flew on 25 June 1997 and is produced by the Progress Arsenyev Aviation Company in Russia. It is a distinct aircraft from the Ka-50, and has export and naval derivatives including the Egyptian Nile Crocodile, the shipborne Ka-52K Katran and the modernised Ka-52M.

Facts
Year
1997 1
Engine Class
Turboshaft 1
Status
In Production 1
Top Speed (km/h)
350 1
Mass (kg)
7700 1
Maximum Mass (kg)
11,300 1
Engine
Klimov TV3-117VMA 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Exemplifies

Source Kamow / Kamov Ka-52 Alligator (Flugzeuginfo.net)

Of Make

Source Kamow / Kamov Ka-52 Alligator (Flugzeuginfo.net)
Sources
1. Kamow / Kamov Ka-52 Alligator (Flugzeuginfo.net)
  • Data table: first flight
    First Flight 25.06.1997
  • Data table: empty weight
    Empty Weight 7.700 kg 16.976 lbs
  • Data table: maximum takeoff weight
    max. Takeoff Weight 11.300 kg 24.912 lbs
  • Data table: speed
    Speed 350 km/h 189 kts
  • Data table: engine
    Engine Model Klimov TW3-117VMA / TV3-117VMA
  • Data table: propulsion
    Propulsion 2 Turboshaft Engines
  • Data table: production status
    Production Status in production
  • Lead
    twin-engined two-seat combat helicopter
  • Lead, manufacturer
    twin-engined two-seat combat helicopter with coaxial rotors developed by the Soviet Design Bureau OKB Kamov (OKB-2), today Kamov JSC, Russia
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