MISSILE Russian patent published in 2006 - IPC F42B15/00 

FIELD: armament.

SUBSTANCE: the missile has a sustainer stage, separated zero stage, adapter frame, slit nut, gas generator and a pyrocomposition. A probe is fastened on the end face of the sustainer stage aft compartment with the aid of the catches and fixed against longitudinal motion of the slit nut. The gas generator is positioned in the probe with obturation. The outer part of the probe is provided with a stepped annular groove, whose deeper part is filled with annular sections of a material that is less strong than the material of the probe and adapter frame. The inner part of the adapter frame is provided with an annular groove whose depth is less than the difference of the steps of the stepped groove and is remote from the stepped groove at a distance not less than the path of motion of the catches in the adapter frame before their release and not more than the path of motion of the gas generator in the probe after of motion of the gas generator in the probe after its release by the slit nut. The adapter frame is provided with a taper from the inner surface to the annular groove. Through holes are made under each annular section in the probe.

EFFECT: reduced dispersion of missiles with control systems providing the necessity of information exchange of the ground control equipment with the units of the on-board control equipment.

6 dwg