| 摘要 |
The invention relates to a subwarhead which is arranged to be separated from a missile, for example a carrier shell or the like, over a target area, the subwarhead comprising an active part (4), a target detector (5) and an arrangement which imparts to the subwarhead a rotation for scanning of the target area in a helical pattern during the descent of the subwarhead towards the target area. The target detector is arranged displaceably in order to allow a free view at the side of the active part. Two diametrically situated aerofoils (1, 2) are arranged to be pivotable from a folded-in position, in which the aerofoils connect with the outer surface of the subwarhead, to a 90 DEG folded-out position, in which the two aerofoils form a braking area for the rate of descent of the subwarhead. The two aerofoils are pivotably arranged via a double joint (4, 5; 6, 7; 8, 9). <IMAGE> |
