|
Iskander-M |
|
Entered service |
2006 |
|
Crew |
3 men |
|
Launcher dimensions and weight |
|
Number of missiles |
2 |
|
Combat weight |
~ 40 t |
|
Length |
7.2 m |
|
Width |
? |
|
Height |
? |
|
Missile |
|
Missile length |
7.2 m |
|
Missile diameter |
950 mm |
|
Missile launching weight |
? |
|
Warhead weight |
? |
|
Warhead type |
conventional |
|
Range of fire |
400 km (estimated) |
|
CEP |
5 - 7 m |
|
Chassis mobility |
|
Engine |
YaMZ-846 diesel |
|
Engine power |
500 hp |
|
Maximum road speed |
70 km/h |
|
Range |
1 000 km |
|
Chassis maneuverability |
|
Gradient |
60% |
|
Side slope |
30% |
|
Vertical step |
~ 0.6 m |
|
Trench |
~ 2 m |
|
Fording |
1 m |
|
The Iskander
(NATO designation SS-26 Stone) short-range ballistic missile is a
successor to the
Oka (SS-23 Spider), which was eliminated under the
INF Treaty. It was first launched in 1996 and was initially designated by NATO
as the SS-X-26. It is considered the most advanced missile of it's
kind. The Iskander-M missile system was officially adopted
by the Russian Army in 2006. Currently Russian Army operates only
about 20 of these missile systems. It's export variant, the Iskander-E, was sold to Syria
(26 units).
The Iskander
road mobile missile system is equipped with two short-range
ballistic missiles, which substantially increases firepower of
missile units. Each missile can be independently targeted.
System is capable of hitting moving targets, as target coordination
can be adjusted while missile is in-flight. The Iskander has several
different conventional warheads, including cluster, fuel-air
explosive, bunker-busting and electro-magnetic pulse. Minimum firing
range is 50 km.
The Iskander
was designed to overcome air defense systems. Missile files at
supersonic speed, excessively maneuvers in the terminal phase of the
flight and releases decoys. In some cases this ballistic missile can
be used as an alternative to precision bombing.
Missiles can
be launched 16 minutes from traveling or 4 minutes from highest
readiness. The second minute can be launched after less than a
minute.
The
transport-erector-launcher (TEL) vehicle uses
MZKT-7930 Astrolog 8x8 high mobility
chassis. It is powered by the YaMZ-846 diesel engine, developing 500
hp. Vehicle can be airlifted by the
An-124 transport aircraft.
The Iskander
TEL is supported by a reloading vehicle, based on the same 8x8
chassis, which carries
two reload missiles. Full missile system also includes command
vehicle, information preparation vehicle, maintenance and repair
vehicle and life support vehicle. All of these vehicles are based on
KamAZ 6x6 trucks.
Variants
Iskander-E,
export version, specially designed to meet MTCR restrictions. It a
maximum range of 280 km. This missile is fitted with internal
guidance system and has a CEP of 30 - 70 m. This missile system has
been exported to Syria (26 units);
Iskander-M
improved version adopted by the Russian army. It's estimated maximum
range is 400 km. It is worth mentioning that this range can be
extended, however this will violate INF Treaty. This ballistic missile is also fitted with both internal and
optical guidance and has significantly improved firing accuracy. Optical seeker provides self-homing capability;
R-500
Iskander-K cruise missile.
|
Video of the Iskander-E short-range
ballistic missile system |
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