Long intercontinental flights - artillery shell

摘要

Long intercontinental flights - artillery projectile with– a payload (2), a rocket engine assembly (3) and the ignition delay or hangfire condition a direction (15) for delaying the ignition of the rocket drive unit by a predetermined period of time after the firing of the projectile,– the rocket engine assembly (3) an end-side rockets nozzle (14) and a combustion chamber in which an end face is designed for burning solid rocket propellant material (9) is arranged,characterized in that– in the combustion chamber between the rocket propellant material (9) and of the rockets nozzle (14) a hollow space (8) is provided and– in this hollow space (8) a permeable propellant set holder (11), (12) is arranged, which the rocket propellant material (9) at the time of firing the projectile against movements and deformations and a load transmission of a direction (12) having a part of the at the time of firing the projectile (1) acceleration load occurring on the walls of the cavity (8) transmits.