RU2003118470A - ROCKET - Google Patents

Claims (1)

A missile containing an engine equipped with a receiver mounted inside the engine along its longitudinal axis, in which a projectile detachable on the trajectory is installed, the caliber of which is less than the caliber of the engine, and a propelling charge, characterized in that the propelling charge is placed in a cavity made in the rear of the projectile , the rear part of the outer surface of the projectile is made of variable cross section with a decrease in the direction of the rear end, while the cavity with a propelling charge is made communicating by means of gas ducts with a reduced power by the projectile’s surface, the outlets of the gas ducts are located symmetrically along the cross section of the shell of the shell, and the bottom of the barrel is connected to the atmosphere through a channel whose area is less than the cross-sectional area of the barrel.