SAFETY-COCKING DEVICE Russian patent published in 1998 - IPC

FIELD: small-sized projectiles furnished with solid-propellant jet engine and warhead with electric fuze. SUBSTANCE: the device has a body with cavity, orifice and sealed partition and control. The body cavity is closed. The orifice is formed on the side of the rocket engine chamber, and the sealed partition is made in the form of a plastic diaphragm with spherical surface and fastened in the middle part of the cavity. The convex part of the diaphragm faces the rocket engine chamber, and on the concave side of the diaphragm a make contact set of the safety-cocking circuit is installed providing its closing at diaphragm deformation. EFFECT: enhanced safety of crew. 2 dwg