KA52

KAMOV Ka-52

Aircraft
Name
Ka-52
Manufacturer
Wing
Rotary
Position
Twin coaxial three-blade rotor
Tail
Booms with twin fins
Type Code
H2T
Engine
Turboshaft
Engine Count
Multi
Position
Both sides of fuselage
Landing gear
Tricycle retractable
Manufactured as
KAMOV Alligator
KAMOV Ka-52 Alligator

KA52

The Ka-52 (NATO reporting name: Hokum B) is a modification of the basic Ka-50 design. It features a two-seat side-by-side cockpit, and is designed to detect targets and redistribute them among supporting Ka-50s. In comparison to the original Ka-50, it has a somewhat softer nose profile due to the wider cockpit, reduced cockpit armor, and large nose-mounted radome. Equipment includes radar with two antennas—mast-mounted for aerial targets and nose-mounted for ground targets, and Samshite day-and-night TV/thermal sighting system in two spherical turrets (one over the cockpit and second under the nose).

Technical Data
Wing span (metric)
14.50 m
Length (metric)
13.50 m
Height (metric)
5.40 m
Powerplant

2 x Klimov TV3-117VK turboshafts, 1,660 kW (2,226 shp) each

Indicative Performance Data
Take-Off
V2
n/a
Distance
n/a
MTOW
10500 kg
Initial Climb (to 5000 ft)
IAS
n/a
ROC
1580 ft/min
Initial Climb (to FL150)
IAS
n/a
ROC
n/a
Initial Climb (to FL240)
IAS
n/a
ROC
n/a
MACH Climb
MACH
n/a
ROC
n/a
Cruise
TAS
190 kts
MACH
n/a
Ceiling
180
Range
240 NM
Initial Descent (to FL240)
MACH
n/a
ROD
n/a
Descent (to FL100)
IAS
n/a
ROD
n/a
Descent (FL100 & below)
IAS
n/a
MCS
n/a
ROD
n/a
Approach
Vapp (IAS)
n/a
Distance
n/a

SKYbrary Partners:

Safety knowledge contributed by: