| 摘要 |
1. A self-propelled mechanical system of a remote impact missile, consisting of a round base plate with a rotary mechanism secured to and rotating on the base plate. The mechanism is equipped with a war head, secured to rotate between the bearers of the rotary mechanism, and with a tracking and decision making system. The optical axis of the latter is parallel to the targeting axis of the head. It is characterised in that the grip (43) of a known warhead (5) is connected to and separable from the tracking and decision-making system (39) by means of a mechanical and electric connection (38). The system cooperates with an external control block (33). Moreover, the grip (43) of a known warhead (5) is connected by means of a separable rigid flat tension member (54) to the grip (43) of the second warhead (6), which is also secured to rotate between the bearers (2, 3) of the rotary mechanism (1, 2, 3). The rotation axes (7, 8) of the relevant warheads (5, 6) are located in horizontal planes. The longitudinal symmetry axes (9, 10) of the relevant warheads (5, 6), which are their targeting axes (9, 10), are parallel to each other and located in the vertical plane, perpendicular to the rotation axis (7, 8) of the relevant warheads (5, 6) and passing through the rotation axis of the round base plate (1) of the rotary mechanism (1,2,3)... |
