DETONATOR FOR A SMALL-SIZED GUIDED GROUND-TO-AIR MISSILE

摘要

The invention relates to military engineering and makes it possible to improve the efficiency and reliability of the knocking out of thin-walled air targets by exploding the part of a missile inside an obstacle. The inventive detonator (1) for a small-sized guided ground-to-air missile comprises a contactless and a contact magnetoelectric target detector provided with a signal processing system and an initiation chain, an eddy-current transducer (4) provided with a constant magnet (5) embodied in the form of a cylindrical tube which is magnetised along a longitudinal axis of symmetry and coaxially disposed on the external side surface of a device, and an induction coil (6) coaxially arranged on the external side surface of the magnet, the parameters of the magnet and the coil being determined by specified relationships. A wave effect magnetoelectric transducer (8) is used as a contact detector. A unit for firing pulse delay, for example a pyrotechnic device is connected to the initiation chain through said magnetoelectric transducer. The contact detector is rigidly fixed to the inner end wall (9) of the body of the detonator (1) on the side of a missile warhead (2).