| 摘要 |
<p>The ammunition i.e. rocket (1), has an explosive charge (6) confined in a compartment (5), and a deconfinement device (12) for deconfinement of the explosive charge under effect of elevation of pressure or temperature within the ammunition. An activation unit activates the deconfinement device, where the activation unit is controllable. The activation unit comprises an igniter (14) for igniting combustion of a powder charge (15) provided in the compartment. A channel (16) of the activation unit connects an output of the igniter to the powder charge.</p> |
