The armour piercing hollow charge has a leading explosive charge and a following hollow charge which is activated in a given time span after the detonation of the leading charge. The secondary hollow charge (15) is foamed (19) directly into the shell body (12). A ring (20) to secure the shrouding (18) of the main hollow charge (15) and a ring (21) to mount the safety unit is foamed with the charge. The secondary charge is foamed using a twin-component polyurethane foam (19).
申请公布号
DE19706687(C1)
申请公布日期
1998.11.12
申请号
DE19971006687
申请日期
1997.02.20
申请人
DAIMLER-BENZ AEROSPACE AKTIENGESELLSCHAFT, 81663 MUENCHEN, DE
发明人
MAYER, HEINRICH, DIPL.-ING., 86565 GACHENBACH, DE;SPENGLER, HANS, 86551 AICHACH, DE