
In numbers Through the lens Video
A variant with twin GSh-30 30mm cannon mounted in a "holster" on the side of the fuselage. Design began in 1974 and production began in 1981 and continued until 1991.
Technical specifications
DESIGNER | OKB Mil |
COUNTRY | Russia |
TYPE |
Multipurpose assault helicopter
|
CREW | 2 + 1 (optionally) |
POWER-PLANT | Two turboshaft engines Klimov TV3-117V |
Power, h.p. | 2x2.225 |
DIMENSIONS | |
Length, m | 18,57 |
Main rotor diameter, m | 17,30 |
Tail rotor diameter, m | 3,91 |
Height, m | 4,39 |
Wing span, m | 6,66 |
WEIGHT | |
Maximum take-off, kg | 11.500 |
Normal take-off, kg | 11.300 |
Empty, kg | 8.570 |
Internal fuel, l | - |
Weight of transported fuel with external tanks, l | - |
Warload, kg | up to 804 |
Payload, kg | |
- soldier | 8 |
- stretcher | 4 |
- freight in cabin | 1.500 |
- with on hook | 2.000 |
PERFORMANCE | |
Maximum speed, km/h | 320 |
Cruising speed, km/h | 270 |
Range, km | - |
Ferry range, km | 1.000 |
Combat range, km | 450 |
Service ceiling, m | 4.500 |
Static ceiling, m | 2.000 |
Rate of climb, m/s | - |
Maximum overload, g | - |
ARMAMENT |
1x two-barrel cannon GSh-23 with 250 rounds. Number external hardpoints: 6. Transportation of weapons: up to 4 launcher B-8B20A, 4xB-13L1.
4x16 Anti-tank missile 9Μ114 Shtorm-V, or pods UPK-23-250 with 23-mm cannon GSh23L x 250 rounds, pods with machine-guns or 30-mm grenade launchers, 4xS-24, 2xGUV-1, 4xGUV-8700, UPK-23-250, Bombs: 8xOFAB-100, 4xOFAB-250, 4xRBK-250, 2xRBK-500, 2xKMGU-2, 2xODAB-500, 2x3B-500. |