The VILKHA multiple launch rocket system (MLRS) is designed to destroy armored, lightly armored, and unarmored vehicles, enemy manpower, command posts, communication centers, military-industrial facilities, aboveground facilities for storage and other purposes at long distances. The peculiarity is that at the initial part of the trajectory a rocket projectile flight correction is provided with the help of pulse engines that reduce to minimum rocket projectile fly deviation from the preset trajectory. In the final part, the rocket projectile is aimed at the target by an inertial and satellite navigation system using aerodynamic control surfaces. VILKHA MLRS ensures forming of individual flight task for each rocket projectile that makes possible to defeat several targets by one salvo.