The 9A55-E launch vehicle (LV) of the Sarma Multiple Launch Rocket System is designed to engage offensive means, armor, mechanized infantry and infantry units in concentration areas, on the move and in the battle order, artillery battalions in concentration areas, on the move and in the battle order, artillery battalions in concentration areas, helicopter units on helipads, air defense and ballistic missile defense units at positions, airborne assault and amphibious assault units in areas of their operations and other targets.
The primary firing method is from the covered fire position in absence of visible orientation points, without LV cabin leaving by the crew. Firing from the LV can be from a shelter using the remote console.
The LV can be operated on all types of roads acceptable for the base chassis.
|
Main performance characteristics: |
|
|
Caliber, mm |
300 |
|
Number of launch tubes in the removable container, ea. |
6 |
|
Full salvo time, s |
Max. 18 |
|
Transfer time of LV from traveling to firing position, min |
3 |
|
Transfer time of LV from firing to traveling position, min |
3 |
|
Crew, men. |
3 |
|
Weight of fully loaded LV without rocket projectiles and crew, kg |
Max. 21,800 |
|
Weight of fully loaded LV with rocket projectiles and crew, kg |
Max. 28,000 |
|
Chassis type |
KAMAZ-63501 vehicle and its modifications |
|
Crew, men |
3 |
This website uses cookies in order to provide you with a better user experience on our site. By continuing to use this site, you agree to our use of cookies. For more information, see Cookie Policy.