In numbers Through the lens Video
NATO reporting name: SS-26 Tender Iskander-E
In Greek M. Alexandros
Entered service: 2006 or 2007
The system is intended to use conventional warheads for engagement of small and area targets, such as:
- command posts and communications nodes
- hostile fire weapons
- air and antimissile defense weapons
- other vital small and area targets
- fixed- and rotary-wing aircraft at airfields
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| Missile: | |
| Length, m | 7,10 |
| Diameter, m | 0,90 |
| Weight missile, kg | 3.800 |
| Warhead weight, kg | 480 (+54 bombs) |
Technical specifications
| DESIGNER | KB Mashinostroyeniya (KBM) |
| COUNTRY | Russia |
| TYPE |
Tactical ballistic missile
|
| CREW | 3 |
| POWER-PLANT | - |
| Thrust, kgf | - |
| ROLLING CHASSIS | MZKT-7930 |
| Weight of launcher with missile, kg | 42.000 |
| Payload, kg | 19.000 |
| Number of missiles: | |
| - on launcher | 2 |
| - on transloader | 2 |
| Time of preparation of shot, min | |
| - conditions of high readiness | 4 |
| - situation of movement | 16 |
| Maximum speed, km/h | |
| - road speed | 70 |
| - off road speed | 40 |
| Autonomy on the road, km | 1.000 |
| DIMENSIONS | |
| Length, m | 7,3 |
| Missile diameter, m | 0,920 |
| WEIGHT | |
| Missile launch | 3.800 |
| Warhead weight, kg | 480 |
| PERFORMANCE | |
| Maximum speed, km/h | Hypersonic |
| - end stage | 7.350 |
| Maximum flight height, m | +100.000 |
| Launch range, km: | until 500 |
| - minimum | 50 |
| Circular error probable, m | |
| - with combination his electrooptics sensor | 1 - 2 |
| - with combination GLONASS | 5 - 7 |
| - with combination INS | 30 - 70 |
| Probability of destruction of objective, % | +70 |
| Operating temperature range, °C | ± 50 |
| Warhead type | Cluster, HE fragmentation, penetrating, HE incendiary |
| Guidance system | Independent, inertial, integrated with optical homing head, GLONASS. |