| 摘要 |
The invention relates to a method for separating an actuation part (3) from a non-spin-stabilized missile, for example a winged shell or the like, by means of first removing the front or rear part of the missile. Thereafter, the remaining missile part (4) together with the actuation part (3) rolls, in which respect the actuation part is slung off from the missile part by the centrifugal force and is positioned to the side of the trajectory of the missile part. Also described are arrangements for facilitating the separation method. |
