FIELD: weapons.
SUBSTANCE: group of inventions refers to military equipment, mainly to the antiweapon with rigid targets, e.g. thickwalled protective works and/or flight landing strips. The fighting unit includes anterior and posterior blocks with bursting explosives and base detonating. The anterior block is made thickwalled, sub-calibered relative to the posterior one and with the front section of a penetrating type, the posterior one being thinwalled. The front section of the anterior block is made as two conjugate cones of the total length of 2.4-5.0 calibres of the anterior block with the vertex angle of the anterior cone being equal or more than 100 and less than 180 degrees. The device includes all-solid rocket engine with a cylindrical body with protrusions on its inner surface, anterior bottom, nozzle block, channel charge of the solid fuel, bushing and ignition device. The engine is additionally equipped with the posterior diaphragm made in the form of glass with lateral long slots and bottom ports.
EFFECT: improved reliability of fighting unit delivery to the target point and performance at the approach angle to the target surface of 28-90 degress without ricochet.
4 cl, 3 dwg
Title | Year | Author | Number |
---|---|---|---|
CONCRETE-PIERCING AMMUNITION | 2005 |
|
RU2277691C1 |
SOLID PROPELLANT ROCKET ENGINE | 2012 |
|
RU2493401C1 |
SOLID-PROPELLANT CHARGE FOR ROCKET ENGINE OF AIRCRAFT ROCKET | 2011 |
|
RU2459969C1 |
KINETIC-ACTION ANTI-TANK MISSILE | 1994 |
|
RU2108537C1 |
MISSILE | 2010 |
|
RU2448321C1 |
CONCRETE-PIERCING AMMUNITION | 2003 |
|
RU2238513C1 |
ROCKET PROJECTILE WITH A PENETRATING WARHEAD | 2022 |
|
RU2800674C1 |
PROJECTILE WITH READY-MADE INJURIOUS MEMBERS | 1998 |
|
RU2148244C1 |
HIGH-EXPLOSIVE WARHEAD | 2003 |
|
RU2247928C1 |
TANDEM TYPE WARHEAD | 2003 |
|
RU2251069C1 |
Authors
Dates
2008-09-10—Published
2006-09-21—Filed