MAIN SOLID ROCKET MOTORS

The main functions are:

• thrust application;
• producing control force along the yaw and pitch channels with rotating control  nozzle (RCN);
• performance of all SRM characteristics under the specified external influences in every phase of operation.

These SRM are used as the first and second stages of the space launch vehicle (SLV).

Basic characteristics:

MAIN SRM FOR SHORT-RANGE MISSILE

The main functions are:

• thrust application;
• performance of all main motor characteristics under the specified external influences in every phase of operation.

The short-range missiles are intended for killing enemy targets within the operational penetration limit relative to the front line.

Basic characteristics:

MAIN SRM FOR MEDIUM-RANGE AND SHORT-RANGE SURFACE-TO-AIR MISSILES

The main functions are:

• thrust application;
• performance of all main motor characteristics under the specified external influences in every phase of operation.

The surface-to-air missiles are parts of the air defense missile complex and intended for killing various air targets.

Basic characteristics:

SRM FOR MULTIPLE LAUNCH ROCKET SYSTEM

Multiple launch rocket systems are one of the widespread and promising types of the ground tactical missile-artillery armament; they are capable of engaging various targets and executing various tasks depending on the head module.

Basic characteristics:

MAIN SRM FOR REBOOST STAGE

It is intended for increasing payload mass injected into orbit by SLV.

Basic characteristics: