| 摘要 |
FIELD: defensive equipment. SUBSTANCE: guided missile warhead uses a leading shaped charge, air-dynamic control actuator unit, fairing with the central air-intake opening, leading shaped charge fuze contact, the air-intake opening is made in the front part of the contact, a filter mesh is secured inside it, a partition is positioned in the middle part on the external surface between the fairing internal surface. A fastening flange is made on the contact rear end. The partition and the fastening flange are made of insulating material (plastic). EFFECT: enhanced developed torque and dynamic characteristics of the control actuator unit operating from incoming air flow, enhanced reliability of operation of leading shaped charge fuze contacts and simplified design. |
