FIELD: ammunition with a high-explosive fragmentation warhead.
SUBSTANCE: the projectile has a solid-propellant engine and an elongated warhead with a nose fuse interconnected by a bearing shell, an axial detonator provided with a cross diaphragm is installed in a channeled body that is closed with a bottom cover and filled with a detonable mixture. An expansion chamber is formed in the bottom part of the body made with an ogival nose section, it is formed by means of a filling skirt on the bearing shell, and an ignition pyrotechnical charge is coaxially installed in the axial detonator fastened on the cross diaphragm through a set of plates.
EFFECT: enhanced power of the projectile.
3 cl, 5 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| HIGH-EXPLOSIVE WARHEAD OF JET PROJECTILE | 2005 |
|
RU2291377C1 |
| ROCKET COMMON-CHARGE WARHEAD | 2009 |
|
RU2401978C1 |
| ROCKET | 2005 |
|
RU2291376C1 |
| AMMUNITION | 2009 |
|
RU2402741C1 |
| JET PROJECTILE | 2005 |
|
RU2291378C1 |
| JET PROJECTILE WARHEAD | 2013 |
|
RU2522178C1 |
| ARTILLERY SHELLS WITH UNITARY LOADING | 2015 |
|
RU2576719C1 |
| MISSILE | 2022 |
|
RU2795013C1 |
| GRENADE LAUNCHER ROUND | 2007 |
|
RU2347176C2 |
| RIFLE-ATTACHED GRENADE LAUNCHER ROUND | 2007 |
|
RU2342625C1 |
Authors
Dates
2006-10-27—Published
2005-08-29—Filed