Device for Ejecting Submunition

This object is met by means for controlling pressure relative to time in a compressed gas space. The control is provided by a programming device. Constructions and an embodiment example is treated in the description. More detailed explanations can be gathered from the drawing.

FIG. 1 shows a schematic drawing of a flying device with scattering vessel and the flight paths of the submunitions which are ejected at different velocities,

FIG. 2 shows a cross section through the embodiment example of a scattering vessel ejecting on both sides, in a schematic presentation, and

FIG. 3 shows a partial cross section of the end part of an ejecting tube according to detail E of FIG. 2 in an embodiment example.

As can be seen from FIG. 1, submunition or individual projectiles 10 from a flying device with suspended or installed scattering vessel forms a scattering field, the submunition or individual projectiles 10 having different firing ranges "a, a1, a2 to b". This object is already met by the device indicated in the prior art. But a uniform "scattering pattern" is produced in this case. The object of the present invention, however, is to make the scattering pattern variable so that, for example, waterways can be left out, front positions at various distances can be covered simultaneously, etc. For this purpose, the general inventive concept provides that an adjustable igniter is arranged, which, when activated in a time-delayed manner, achieves the respective desired firing range "a to b.sub.n ".

The corresponding device is shown in FIGS. 2 and 3. As already mentioned, the scattering vessel B consists of a plurality of ejecting tubes R1 to Rn. The submunition 10 is stored in the ejecting tubes, each tube having a propelling piston 13 which ejects the submunition by means of the compressed gas which is produced by means of a powder charge 20 in the compressed gas space 12. The powder charge 20 is ignited--via the boreholes 11a--by means of the igniting device 11b and the igniting charge 11. The device, which is described in the following, is provided in order that each submunition 10 has a desired firing range, wherein this can be a matter of the submunition 10 within an ejecting tube R1, R2, etc., or submunition 10 from tubes R1 to R2, etc.

Each of the ejecting tubes R1 to Rn has a tube closing plate 14 at its end opposite the ejecting opening, which tube closing plate has a borehole in its central axis 19 which is sealed with a plug 15. A bearing borehole 14a, which is likewise guided through the sealing plug so as to fit exactly with respect to dimensioning and position, is arranged in the radial axis of the tube closing plate 14. A locking bolt 16, which locks the sealing plug 15 with the tube closing plate 14, is located in this borehole 14a. Accordingly, a gastight compressed gas space 12 is formed in conjunction with the propelling piston 13 located against the submunition 10. In the normal ejecting process, the compressed gas formed by the powder charge 20 flows into this compressed gas space 12, presses on the propelling piston 13, and the latter pushes the submunition out of the ejecting tube R1, R2, etc. in axial direction A at a high velocity. If different ejecting velocities and, accordingly, different scattering patterns or hit ranges are to be achieved, the locking bolt 16 is pressed into the free space of the bearing borehole 14a by means of a powder charge 17, which is likewise arranged in the bearing borehole 14a and is activated by means of an igniting device 18a. The propelling charge pressure in the compressed gas space 12 now ejects the sealing plug 15 from its unlocked position out of the tube closing plate in direction S. The bearing borehole of the sealing plug is accordingly opened and a portion of the compressed gas escapes from the gas compressed space 12, also in direction S, so that none of the desired ranges "a to b" effects a corresponding increased acceleration of the submunitions 10.

The ignition of the powder charge 17 by means of the igniting device 18a can be effected either by means of manual presetting or, according to a special embodiment example, by means of a programming device 18b in a fully automatic manner. The programming device 18b comprises not only an ignition line 18c for the igniting device 18a, but also an ignition line 18d for the igniting device 11b. In this way, a program can be input in the program unit prior to the beginning of the mission with respect to the given geographical conditions or the enemy position, the battle plan, etc. However, the ignition times can also be controlled by means of the on-board computer, which conveys enemy location target recognition to the igniting devices 18a on the basis of the distance measurements which are accordingly effected.