| 摘要 |
FIELD: weapons and ammunition.SUBSTANCE: rocket missile includes a housing with an explosive, a fuse, a power source, a detonator, a safety gun cocking gear and an optic target sensor. The power source, the detonator and the safety gun cocking gear are arranged in the fuse housing. The safety gun cocking gear is connected to the optic target sensor. The optic target sensor includes an electronic unit and two and more receiving and emitting channels. Each of the receiving and emitting channels includes a pulse optic emission source and a photoreceiver, which are connected to an electronic unit. The optic emission source and the photoreceiver form a receiving and emitting channel. The optic emission source and the photoreceiver are located almost tightly to each other. Optic axes of the optic emission source and the photoreceiver are directed in the movement direction at an angle of <90° to longitudinal axis of the fuse and are mainly parallel. Required number of emitters in the optic target sensors is determined on the basis at which at least for one of the emitters of optic sensor T??t, where T - period of one working detection cycle with one receiving and emitting channel, ?t - time interval.EFFECT: improving efficiency of ammunition of discontinuous action.3 cl, 2 dwg |
