BG642Y1 - Anti-tank guided missile - Google Patents

Abstract

The missile is used in warfare technology for destroying armoured targets. It comprises a missile (1), ejection motor (2) and container (3). The missile (1) comprises a control compartment (7) with cross-contact (8), warhead (9) with a copper funnel (10), lens (11), briquettes of explosive (12 and 13) with a contact cone (15) connected to them, sustainer (16), control unit (17), coil (18) comprising a base (19) and fairing (20), interconnected in a fixed manner and enabling the winding of a conductor (21) of specified length. In the ejection motor (2), a charge of specific weight (4) is fitted, and the front and rear nozzle apertures have specified dimensions. 1 claim, 2 figures

Description

Technical field

The utility model refers to an anti-tank guided missile (ATGM), which is used to hit armored and other targets.

BACKGROUND OF THE INVENTION

Known is the ATGM (1), which consists of a rocket stored and fired from a container by means of an ejection engine located at the rear of the rocket, locked in and remaining in the container after launch.

The missile consists of a sequentially coupled control compartment, combat unit, propulsion engine, control unit and coil.

The ejection motor is a steel balloon with a discharge charge, front and rear nozzle openings that ensure trouble-free start-up.

The container is made of fiberglass with glass compound wrapped around it, soaked in compound.

The warhead contains cumulative explosive-type briquettes that are placed in the pre-paraffinized inner surface of the warhead housing. The warhead includes two contact cones in the structure which, when hit by a rocket, aim to connect the electrical circuit of the safety detonation mechanism and they (the detonation mechanism and the combat part) consecutively operate.

The construction of the known device provides the following tactical and technical characteristics maximum distance 2000 w, armor penetration - 400 mm.

Characteristic of the known device is that it operates at a shorter distance and has less armor penetration.

The technical nature of the utility model

The task of the utility model is to create an anti-tank guided missile, which: operates at a greater distance, achieved by winding a longer conductor; greater armor penetration achieved by designing a new warhead; to simplify the technology of container tube production.

The task is solved by constructing a new rocket, with a cross contact cone added to the control compartment. The warhead consists of sequentially connected: inverted U-shaped cone, electrically insulated from the housing, copper funnel, cumulative-type explosive briquettes, lens enclosed. The coil consists of a base and a fairing, which are fixedly connected and allow winding of a wire of 2500 sh. As a result of the increased weight of the rocket, caused by the greater weight of the warhead and the coil, an ejection engine with increased dimensions of the front and rear nozzle openings and an ejection charge of greater weight are used. The container is made of fiberglass tube.

The advantages of the device are as follows: providing a maximum distance to the affected targets 2500 w, providing armor-piercing 460 mm, and a new design solution for the manufacture of a fiberglass tube container, which simplifies production technology, with these changes in the warfare is achieved by matching the axes of the functional parts (copper funnel, explosive briquettes, lens), homogenization of the explosive density in the briquettes both in volume and adjacent surfaces to the other details, incl. an effect that increases the armor penetration.

Description of the attached figures

Figure 1 is a general view of an anti-tank guided missile in a container;

Figure 2 is a general view of an anti-tank guided missile.

Examples of implementation of the utility model

An exemplary embodiment of the utility model is shown in Figures 1 and 2.

The device consists of a rocket 1, an ejector engine 2 and a container 3 of a fiberglass tube (Figure 1).

The missile consists of a sequentially coupled control bay 7 with a cross contact 8, a warhead 9 with a copper funnel 10, a lens 11, explosives of cumulative type 12 and 13 with a U-shaped cone 15 connected to them, a marching engine 16, a control unit 17, a coil 18 consisting of a base 19 and a fairing 20 fixedly interconnected to allow winding 21 of 2500 w in length in the form of a trapezoidal coil (Fig. 2).

A charge 4 is placed in the ejector motor 2, which through the front 5 and rear 6 nozzle openings ejects the rocket from the container, providing a trouble-free start (Figure 1).

Application of utility model

The ATGM device is used in military equipment to hit armored targets.

The action of the ATGM is as follows.

The rocket 1 and the ejection engine 2 mounted in the container 3 are placed on a launcher which, upon actuation, prepares the container 3 and the missile 2, which causes the ejection engine 2 to launch the missile 1 from the container 3, providing a trouble-free launch (figure 1).

The rocket in its flight is controlled by the launcher through a coil 21 coiled by the coil 18. The electrical signals from the conductor link are converted into control commands, which through the control compartment 7 direct the missile to the target. When the missile meets the target, the cross contact cone 15 of the control compartment 7 and the U-shaped cone 5 15 of the warhead 9 close the trigger circuit of the warhead 9 and actuate (Fig. 2).

Claims (1)

1. An anti-tank guided missile consisting of a rocket with a sequentially coupled control compartment, a warhead, a propulsion engine, a control unit and a 15-conductor coil, an ejector engine and a container, characterized in that it is directed to the control compartment (7) the cross contact cone (8) is fixed, and the copper funnel (10), the cumulative type explosive briquettes (12 and 13) and the lens (11) are placed in a housing (14) of the warhead (9) to which it is fixed U-shaped contact cone (15), electrically insulated from the housing (14), as a base (19) from b the nozzle (18) is fixed to the fairing (20) with a coiled wire (21), and the container (3) is made of fiberglass tube, with nozzle openings in the ejector motor (2) with front (5) and rear (6) mounted charge (4), providing rocket launch (1) from the container (3).