DE2307581A1 - MISSILE AMMUNITION - Google Patents

Description

Rocket ammunition The invention relates to rocket ammunition with a combat charge and a solid rocket propellant of the form downstream of the combat charge a forehead burner, which is facing away from the combat charge burns down.

A variety of military-style missiles will be optional used against targets of different distances.

It is therefore often the case that only a small part of the rocket fuel is used up when the missile reaches its target and its combat charge takes effect. This is especially true for guided missiles with immutable incorporated Solid rocket propellants too.

It is known to use the propellant parts that have not yet been burned at the finish Increasing the destructive effect of the combat charge with the latter detonating to bring, but only with missiles whose solid propellant charge the shape has a burn-insulated inner burner on the outside. The battle charge is in this case, on the one hand, from the combustion insulation of the internal burner, on the other hand arranged by the combustion chamber housing limited gap.

It is the object of the invention to also be able to fly and / or swim Rocket ammunition of the type mentioned at the beginning, for example due to the requirement long drive tents with a solid rocket propellant in the shape of a forehead burner is equipped to ensure with simple means that in the target if necessary any remaining unburned propellant material detonated with the combat charge This object is achieved in that the combat charge on their the front burner facing one or more shaped charges with spike-forming Has linings or projectile-forming coverings.

The spikes or projectiles that are used in the combat charge detonation from the lining or covering material, penetrate due to the impact Lining or occupancy arrangement with high speeds in the unburned Propellant material and in this way ensure a safe detonation same.

The higher destructive effect achieved thereby experiences a further one Increase if, according to the design features of the invention, the housing, in dcm the Forehead burner is installed, at least in the area adjacent to the combat charge a) is covered with splinters or b) consists of preformed splinters or c) through the cutting effect of an embossed foil that has the forehead torch in addition to a Isolation or instead of the same surrounds it, is broken down into splinters.

The invention is illustrated schematically on the basis of and below detailed embodiment described in detail.

The single figure shows partly in side view, partly in longitudinal section a rocket-propelled missile 1 with a combat charge 2. When the combat charge 2 downstream rocket engine 3 is of the solid type. Its propellant charge is designed as a forehead burner 4 and burns from that of the combat charge 2 facing away from the face. The forehead burner 4 is encased by an embossed one Foil 5. This foil 5 ensures that the combustion chamber housing labeled 6 is broken up into fragments in the case of the detonation of the non-combusted material present in the cell, as described below Forehead burner section. It is not necessary if the combustion chamber housing -as in the one half of the figure indicated from the outset cared for, interconnected Splinters 7 is built up.

The combat charge 2 is facing away from the forehead burner 4 on its side Front side assigned a Betonatorelement 8, which when the target object is reached appeals to. On their end face facing the front burner 4 there are two Full charges 9.10. One of the two shaped charges 9, 10 has for example a spike-forming lining 11, the other a projectile-forming coating 12 on.

If the missile 1 just described comes against a target object Use whose distance from the location of the missile launch is only a fraction of the missile range, a large percentage of the forehead torch will target .4 r. Not yet burned. He is detonated by dic fencing charge 2 with the detonation brought. In the event of a combat charge detonation, it forms from the lining 11 of the one shaped charge 9 is a high-energy sting and from the occupancy 12 the other shaped charge 10 a high-energy projectile. Sting and projectile penetrate the unburned forehead burner mass at high speeds, from which their initiation results. The consequence of this initiation is already mentioned decomposition of the combustion chamber housing 6 into high-energy splinters through which the destructive effect of the missile in question experiences a noticeable increase.

Patent claims:

Claims (5)

Claims 1. Rocket ammunition with a combat charge and one solid rocket propellant in the form of a forehead burner, downstream of the combat charge, which burns down from its front facing away from the combat charge, thereby It is not noted that the combat charge (2) is on its stalking burner (4) facing the end face one or more shaped charges (9, 10) with spike-forming Has linings (11) or projectile-forming coverings (12). 2. Rocket ammunition according to claim 1, characterized in that g e k e n n -z e i c h n e t that the forehead burner in an at least partially with preformed splinters occupied combustion chamber housing is installed. 3. Rocket ammunition according to claim 1, characterized in that g e k e n n -z e i c h n e t that the forehead burner (4) in t -'Lnein at least partially from preformed Splinters (7) composite combustion chamber housing (6) is installed. 4. rocket ammunition nnch claim 1, characterized g e k e n n -z e i c h n e t that the front burner (4) is installed in a combustion chamber housing (6), which is at least partially defined in splinters with the help of an embossed film (5) Shape and size can be dismantled. 5. rocket ammunition nsch claim d, characterized g e k a n n -z e i c h n c t that the forehead burner (4) is covered with the embossed foil (S).