Abstract: Ammunition incorporating a sensing fuse and a parachute, and which has the trajectory thereof correctable during its final flight phase, and a method for the combating of armored target objects with the utilization of such ammunition. The ammunition with the sensing fuse is equipped with a pulse transmitter for a course alignment or correction in the direction towards the lateral or sideways offset of a target object which has been detected by the sensing fuse, and with devices for suspending the action of a parachute during the approach to a target by the ammunition along a quasi-ballistic trajectory.

Abstract: An arrangement for generating a firing or triggering signal for a projectile which is conveyed in a flying body overflying a target, wherein a target identifying circuit requires a processing period for the identification of a detected target pursuant to predetermined characteristics, and in which, subsequent to a waiting period dependent upon the flying altitude, there occurs a delay or lag period between the initiation of the firing signal and the ejection or, respectively, target impact of the projectile.