FIELD: ammunition.
SUBSTANCE: the guided projectile has a detonating device with target sensors and safety-actuating mechanisms, leading shaped charge, shaped warhead, control compartment positioned between them, having a central channel, high-explosive warhead and a blast delay electronic unit. The high-explosive warhead is positioned between the control compartment and the shaped warhead, the main charge is positioned in the body with the central channel. Positioned on the rear end face of the body regarding the flight the glight are additional charges made of an explosive with a higher sensitivity to impact as compared with the high explosive of the main charge.
EFFECT: enhanced efficiency of action of the guided projectile.
2 dwg
Title | Year | Author | Number |
---|---|---|---|
TANDEM TYPE WARHEAD | 2003 |
|
RU2251069C1 |
GUIDED PROJECTILE | 2004 |
|
RU2262065C1 |
GUIDED MISSILE | 2004 |
|
RU2278351C1 |
SELF-PROPELLED PROJECTILE OF GUIDED TYPE | 2010 |
|
RU2439473C1 |
GUIDED MISSILE | 1992 |
|
RU2046281C1 |
HIGH-EXPLOSIVE NON-ISOTROPIC WARHEAD | 2006 |
|
RU2301958C1 |
HIGH-EXPLOSIVE WARHEAD | 2003 |
|
RU2247928C1 |
METHOD FOR ARMOR PIERCING BY SHAPED-WARHEAD MISSILE AND GUIDED MISSILE FOR ITS REALIZATION | 2000 |
|
RU2173443C1 |
COMBAT SECTION OF GUIDED MISSILE | 2002 |
|
RU2247927C2 |
GUIDED MISSILE | 2000 |
|
RU2172923C1 |
Authors
Dates
2005-10-10—Published
2004-04-19—Filed