| 摘要 |
FIELD: weapons and ammunition.SUBSTANCE: claimed missile comprises airframe, instrument unit with onboard control system hardware units, replaceable self-guidance head, the main fragmentation, piercing and demolition warhead. Additionally, it incorporates extra warhead with identical weight-centring properties relative to the self-guidance head. The mission is generated including aiming point, missile flight path parameters and type of targets to be hit. The missile with replaceable warhead or interchangeable warhead with extra warhead is selected. Changes are made in the flight mission profile subject to the target type. The missile is launched and supported with the diving sections subject to the target type to the point with preset coordinates. The warhead is blasted with programmed undershot to geometrical centre of area target or to target proper.EFFECT: higher efficiency of hitting.5 cl, 8 dwg |
