RU2544037C1 - Launching facility - Google Patents

Abstract

FIELD: weapons and ammunition.

SUBSTANCE: launching facility for missile launching includes base (1), rack (2), and frame (3) with guides (4). The guides have a possibility of independent guidance from each other as to an angle of elevation. On guides (4) there installed are remotely controlled devices (5) of depression of a limit stop retaining the missile. The guides are charged with target-missiles (6) in launching containers. Missiles (6) are electrically connected to connectors of the launching facility.

EFFECT: enlarging technical capabilities of a launching facility; improving quality.

2 cl, 2 dwg

Description

The proposal relates to launchers of target missiles and can be used in the development of launchers of target complexes with simulators of aerial missile-type targets.

Known launcher for launching missiles (patent RU No. 2466342, IPC F41F 3/04, publ. 10.11.12, Bull. No. 31), which contains a base that is movable with the possibility of orientation in elevation and azimuth package launch tubes, located fan-shaped, and two actuators, launch tubes are fan-shaped along the generators of the hyperboloid of rotation and pivotally connected to two spaced apart disks kinematically connected to the drives.

This installation is complex in design, requires the use of a computer for operation and cannot provide the required range of launch angles of target missiles. The orientation of the launch tubes in elevation and azimuth is dependent.

The prototype launcher of the target complex for launching missile-type aerial targets simulators is known. It includes a base plate, turret rack and a guide that can be guided by the elevation angle and azimuth (article - “Phalange” prolongs life, magazine “Equipment and armaments”, 2002, No. 4).

This launcher has a simple functional design, however, it is charged with only one target missile, which does not allow organizing on its basis a simulation of a massive attack of an enemy air attack means with different flight paths of targets.

The objective of the invention is to develop an optimized design of the launcher of the target complex, which allows to organize a simulation of a massive attack of air attack weapons.

The technical result of the invention is to expand the technical capabilities of the launcher, improving the quality of combat training of anti-aircraft gunners.

The specified technical result is achieved in that in a launcher for launching target missiles containing a base, a strut and a guide that can be guided in the elevation angle and in azimuth, the new thing is that the installation is equipped with at least two guides having independent guidance from each other at elevation angles; remotely controlled devices for recessing the stopper holding the rocket are mounted on the rails.

Guides can also have independent guidance from each other in azimuth.

Providing the launcher with at least two guides having independent guidance from each other at elevation angles, as well as independent guidance from each other in azimuth, allows you to simulate a massive air attack of air attack weapons with different flight paths, which improves the quality of combat training of anti-aircraft guns .

Installing on the guides of remotely controlled devices to heat the stopper holding the missile allows launching of target missiles made on the basis of military equipment of portable anti-aircraft missile systems of the Igla type, in which the missiles are fixed in the launch containers with movable stoppers (before the launch of this missile, the anti-aircraft gunner rotates the handle located on the container tube with the hand, while the stopper disengages from the rocket).

Technical solutions with features distinguishing the claimed solution from the prototype are not known and do not follow explicitly from the prior art. This suggests that the proposed solution is new and has an inventive step.

The invention is illustrated by drawings, where figure 1 and 2 shows a General view of a variant of the proposed device (main view and top view, respectively).

The launcher for launching missiles comprises a base 1, a rack 2, a frame 3 with guides 4. The guides have the possibility of independent guidance from each other in elevation. On the guides 4 installed remotely controlled devices 5 recesses stopper holding the rocket. The guides are loaded with target missiles 6 in launch containers. Missiles 6 are electrically connected to the launcher connectors.

Launcher works as follows.

The location of the starting positions of the anti-aircraft systems and the launcher of the target complex are determined by the assigned combat training or research task.

The flight paths of unguided target missiles 6 are set by setting the heading angle and elevation angles of the guides 4 of the launcher.

The launcher is loaded with target missiles 6, after which the service crew leaves for allotted safe positions.

At the command of the shooting director, the crew makes a remote launch of the target missiles. From the control panel, an electric signal is first supplied to the remotely controlled devices 5, the stoppers holding the rockets 6 are disengaged from the rockets. Then, signals are received to ignite the electric igniters of the starting engines and the missiles begin ballistic flights, the trajectories of which are determined by the elevation angles of the guides.

At the simultaneous (or sequential with small intervals between launches) launch from the launcher of several target missiles, a massive attack of enemy air attack means having different flight paths is simulated.

Anti-aircraft gunners detect, capture, track targets, and can also fire at targets.

Claims (2)

1. Launcher for launching target missiles, containing a base, a rack and a guide having the ability to guide in elevation and azimuth, characterized in that the installation is equipped with at least two guides having independent guidance from each other in elevation angles , on the rails installed remotely controlled devices for sinking the stopper holding the rocket. 2. Launcher according to claim 1, characterized in that the guides have independent guidance from each other in azimuth.

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