FIELD: weapons and ammunition.
SUBSTANCE: guided projectile comprises tandem explosive assembly, including leading jet charge (LJC) and main explosive assembly (EA), and also protective device and steering linkage unit (SLU). Protective device is arranged in the form of armoured disk-shaped base profiled with preferable provision of axial rigidity, where LJC is installed. Base is fixed in projectile on circular support element with support along external circuit. Base is arranged on the basis of glass-filled plastic material with density that is less than density of support element material, at the same time it is armoured and profiled with structural elements and functional cavities of SLU composite parts.
EFFECT: increased efficiency of tandem explosive assembly due to reduction of effect at main explosive assembly as leading cumulative charge actuates.
2 dwg
Title | Year | Author | Number |
---|---|---|---|
GUIDED MISSILE | 2007 |
|
RU2351886C1 |
GUIDED MISSLE | 2007 |
|
RU2358229C2 |
GUIDED MISSILE | 2001 |
|
RU2218546C2 |
GUIDED SHELL | 2007 |
|
RU2351887C1 |
GUIDED MISSILE | 2008 |
|
RU2370726C1 |
GUIDED MISSILE | 2008 |
|
RU2370725C1 |
GUIDED MISSILE | 1994 |
|
RU2084809C1 |
METHOD OF GUIDED MISSLE LAUNCH | 2007 |
|
RU2358232C2 |
GUIDED MISSILE | 2002 |
|
RU2222768C2 |
GUIDED MISSILE | 2000 |
|
RU2172923C1 |
Authors
Dates
2010-12-10—Published
2009-04-20—Filed