| 摘要 |
FIELD: missilery. ^ SUBSTANCE: an air defence missile-target comprising a propulsion unit with a stabilizer, a front radiotransparent section with liquid propellant, a UHF corner reflector, a fairing and a tracer unit. On the propulsion unit side of the fairing there is a fuze safety and arming mechanism with a damaging agent, and an electric power source, a protection circuit board and a switching circuit board electrically connected to one another. Moreover, said UHF corner reflector is wound along its entire perimeter supported by the fairing facets with an insulated cable that is connected to said switching electronic board, and said liquid propellant is placed in airtight containers, wherein the longitudinal axis of said damaging agent coincides with the longitudinal axis of one of the airtight containers, and said electric power source is a pyrotechnic battery. ^ EFFECT: ensuring visual effects of damaging the missile target by fragments of the warhead of an air defence guided missile at a calculated acceptable miss distance and with a guaranteed changing of the missile target flight trajectory. ^ 2 cl, 3 dwg |
