| 摘要 |
FIELD: weapons and ammunition. ^ SUBSTANCE: invention relates to combat equipment. In compliance with the proposed invention, the missile engine housing front part surface features taper-section bulges arranged uniformly thereon to accommodate inclined jet holes. The housing inner surface features a shear annular ledge accommodating the missile front cover moving axially thereon, the front cover outer surface being furnished with sealing rings. The powder charge features an axial channel housing central tube jointed with aforesaid cover. The central tube front end face is closed by a membrane, its read end face being open and fitted into the truncated-cone funnel branch pipe. The latter has its inner surface forms the area of shaped charge jet formation. ^ EFFECT: increased armour penetration. ^ 1 dwg |
