.jpg "Mi-35MS Command and control helicopter. First flight: 2013")
In numbers Through the lens Video
Mi-35MS Command and control helicopter.
Mi-35MS - Upgrades and changes are shown in red.
Three-view drawing
Technical specifications
| DESIGNER | OKB Mil |
| COUNTRY | Russia |
| TYPE |
Command and control helicopter
|
| CREW | 2 |
| POWER-PLANT | Two VK-2500 turboshaft engines |
| Power, h.p. | 2x2.466 |
| DIMENSIONS | |
| Length, m | 18,57 |
| Main rotor diameter, m | 17,20 |
| Tail rotor diameter, m | 1,90 |
| Height, m | 4,39 |
| Wing span, m | 6,66 |
| Wing area, m2 | - |
| WEIGHT | |
| Maximum take-off, kg | 11.500 |
| Normal take-off, kg | - |
| Empty, kg | 8.000 |
| Internal fuel, l | 1.500 + available fuel 1.000 |
| Weight of transported fuel with external tanks, l | 1.200 (4x500) |
| Warload, kg | - |
| Payload, kg | 4-5 passenger (maximum up to 8 passenger). |
| PERFORMANCE | |
| Maximum speed, km/h | 335 |
| Cruising speed, km/h | 260 |
| Range, km | 420 |
| Combat range, km | - |
| Service ceiling, m | 4.800 |
| Static ceiling, m | 2.400 |
| Rate of climb, m/s | 816 |
| Maximum overload, g | 3 |
| ARMAMENT | Doesn't have (defensive). |