RU25077U1 - MOBILE ANTI-AIR DEFENSE MISSILE COMPLEX - Google Patents

Abstract

1. A mobile air defense missile system containing a rotating turret mounted on a carrier, a launcher mounted on a turret with missiles equipped with homing heads, launcher guidance aids, communications, a digital computer and a control panel, characterized in that as a means target detection introduced a passive infrared station containing an infrared radiation receiver mounted on the launcher and made with the possibility of a circular view, and yazanny with infrared radiation receiver coordinate extracting unit mounted in the turret and in turn associated with a digital vychislitelem.2. The mobile air defense missile system according to claim 1, characterized in that the passive infrared station installed on it is connected to several missile systems that are not equipped with means for detecting targets, with the possibility of transmitting target designation coordinates to them.

Description

Mobile air defense missile system

The utility model relates to military equipment, namely to short-range mobile air defense systems (air defense) and is intended to destroy airborne, mainly low-flying targets.

The following analogues of the claimed utility model are known.

Mobile anti-aircraft missile systems (SAM) short-range air defense "Roland-1 and" Roland-2 (Germany - France) 1. In these systems, target detection is carried out by a radar station, and target tracking and missile guidance, respectively, optical and infrared (IR ) devices. In the second modification of the complex, radar for target tracking was additionally used.

The air defense air defense system Rapier 2000 (USA) 1,2, designed to protect strategic objects from aviation, has a modular design and consists of three modules, each of which is placed on a separate trailer. The main module is the launcher, which houses anti-aircraft guided missiles (SAM) and an optical-electronic system (ECO) for automatic target and missile tracking. On the second trailer there is a radar for viewing and detecting targets, on the third two-beam radar for target tracking and missiles. The missile control system is radio command, missile commands are sent through the transmitter, which is part of the tracking radar.

Multi-purpose missile system ADATS (Air Defense Anti-Tank System) 1, developed jointly by Switzerland and the United States, is designed to destroy both air and ground targets. Target detection

IPC F 41 G 7/20

in ADATS is carried out using radar, missiles are guided by a laser beam.

Short-range air defense missile systems "Crotale NG 1.3 is designed to protect armored units on the march and stationary objects from massive attacks by enemy aircraft and helicopters. On one platform are launchers with missiles, radar target detection, radar target tracking and direction finding missiles, optical equipment: front view system FLIR (Forward Looking Infrared Receiver), a daytime television camera with a telemetry tracking target and missiles, infrared direction finder to capture the missile and its guidance during the first seconds of flight.

The Tunguska Ml (USSR) 4 anti-aircraft missile and cannon complex (ZRPK) contains cannon and rocket weapons combined in a single combat vehicle, radar and optical systems for detecting, tracking and controlling fire using common means for aiming guns and aiming SAM systems: radar detection, Radar tracking, sighting optical equipment, computer system.

ZRPK "Shell-S 4, also known by Russian patents 5,6,7, is a modification of the complex" Tunguska Ml. The complex contains a turret with a guidance drive, launchers with anti-aircraft missiles placed on it, anti-aircraft guns, target detection radars, target and missile tracking radars, and a computer system. In addition, the tower houses an optoelectronic system (OES), which includes a thermal imaging device with a telecommand, an infrared direction finder, an antenna with a missile command transmitter and ECO guidance drives.

the work of each of them, significantly reduce the secrecy of these systems from enemy radio reconnaissance systems and can lead to their rapid detection and defeat. In addition, these missile systems are ineffective in conditions of strong enemy radio opposition.

The closest analogues of the claimed utility model are self-propelled air defense systems Strela-1 and Strela-10 (USSR) 8.

The combat vehicle of these complexes is equipped with a launcher mounted on a rotating turret with four missiles in transport and launch containers, means for detecting targets and aiming, communications and a control panel. Detection and aiming tools contain a passive direction finder and an optical sight. After the missile is launched, its guidance on the target is carried out by the homing head. The developers of these air defense systems managed to avoid the disadvantages of the analogues described above. The use of passive (non-radiating) means of detection and aiming ensures high concealment of air defense systems from enemy technical reconnaissance systems.

At the same time, the closest analogues (Strela-1 and Strela-10) are characterized by a number of features that significantly limit the possibilities of their application. A passive direction finder provides detection only of targets with the onboard radio facilities turned on, when the onboard radio devices are turned off, the target becomes “invisible to him.” Optical sight is applicable only in conditions of good visibility during daylight hours; at night and in conditions of poor visibility during the day, the complex is ineffective.

action effective in the fight against targets moving in the radio silence mode, which at the same time would have high stealth during combat work.

The technical result of the claimed utility model consists in expanding the possibilities of using a mobile air defense missile system in low visibility conditions, strong radio interference, as well as against targets in radio silence mode, while maintaining high security of the complex.

The essence of the claimed utility model is that in a mobile air defense missile system containing a rotating turret mounted on a carrier, a launcher with missiles equipped with homing heads, means for guiding the launcher to the target, communications equipment, a digital computer and a control panel, as a means of detecting targets, a passive infrared (IR) station was introduced, containing a PC radiation receiver installed on the launcher and made with the possibility of circular viewing pa, and the associated receiver of infrared radiation block allocation coordinate which is mounted in the tower and, in turn, is connected to digital computer. The use of passive detection tools operating in the infrared range of the spectrum and receiving thermal radiation from objects makes it possible to detect targets in conditions of any optical visibility and at any level of radio noise with high stealth of the combat operation of the complex, regardless of whether the target emits radio waves or not.

In addition, a mobile air defense missile system characterized by the aforementioned features is proposed, the passive infrared station of which is connected via a digital computer to several other missile systems not equipped with target detection means, with the possibility of transmitting coordinates to them

target designation. This makes it possible to use the inventive mobile air defense missile system for coordinated combat operations as part of a battery together with cheaper simplified missile systems (without means of target detection).

The claimed technical solution is illustrated by graphic materials, where in FIG. 1 is a schematic diagram of a mobile air defense missile system, and FIG. 2 is a diagram of the combat operation of a mobile air defense missile system as part of a battery using one passive infrared station.

The following notation is used in the diagrams:

1- carrier

2-tower

3- launcher,

4- transport and launch container with a rocket,

5- receiver of infrared radiation,

6 - block allocation of coordinates,

7- horizontal guidance drive,

8- vertical guidance drive,

9 - missile launch equipment,

10- digital computer,

11- control panel,

12-wire connection

13- radio communication,

Mobile missile defense system has the following design (Fig. 1). A tower 2 is mounted on the carrier 1 with the possibility of circular rotation in the horizontal plane. Various self-propelled or transported vehicles, as well as stationary objects, can be used as the carrier 1. A launcher 3 with several transport and launch containers 4 is placed on the tower, in each of which there is a missile equipped with a homing head. A passive infrared target detection station consists of an infrared receiver 5 located in the upper part of the launcher and made with the possibility of circular viewing, and the associated coordinate allocation unit 6 installed inside the tower. Here are located in the tower: horizontal guidance drive 7, vertical guidance drive 8, missile launch equipment 9 and digital computer 10. The latter is connected by wire connections 12 to the coordinate allocation unit, horizontal and vertical guidance drives, missile launch equipment and control panel 11. Communications with other missile systems during joint combat operation as part of the battery (Fig. 2) are telecode, they can be either wired 12 or radio 13.

The operation of the mobile air defense missile system in offline mode (Fig. 1) is as follows. The launcher 3 is set to a position with such an angle so that the zero line of the field of view of the infrared receiver 5 is parallel to the horizon. In this position of the launcher, the infrared receiver receives a circular overview of the air situation. At the same time, tower 2 is stationary, all the equipment of the complex, except for guidance drives 7 and 8, is turned on. The radiation signals of the targets 14 from the infrared radiation receiver 5 are fed to the coordinate allocation unit 6, where these signals are processed, after which information about

the coordinates of the targets enters the digital computer 10. In the digital computer, the signals are selected, the signals from the stationary sources of heat radiation are eliminated and are not subsequently displayed on the control panel display. The display of the control panel 11 reflects the air situation taking into account only moving targets. After detecting the targets, the digital computer selects the most dangerous one based on the range to the target and its speed, and sends signals to the vertical 7 and horizontal 8 guidance drives, which deploy the launcher 4 of the mobile air defense missile system to the selected target. From the control panel 11 through a digital computer 10, a signal is sent to the rocket launcher 9 to capture the selected target with the missile homing head. After receiving a signal from the rocket about capturing the target and holding it, a signal is sent to the rocket launch from the control panel through a digital computer to the rocket launch equipment. After the missile is launched, the launcher is turned by the guidance drives towards the next selected target. The defeat of targets is recorded by the IR station and is displayed on the control panel display.

When the mobile air defense missile system in the centralized target designation mode, the telecode information via wire or radio is transmitted to a digital computer 10, where it is compared with information received from the infrared detection station 5 targets. In case of identification of these target designations, the calculator gives signals to turn the launcher 4 in the direction of target 14 and to launch the rocket - in the same way as in the autonomous mode described above.

A mobile air defense missile system, equipped with an infrared target detection station 5, can act as a command post by exchanging information about the air situation or providing the coordinates of targets 14 to other missile systems of this type, in

including simplified configuration (without means of target detection). The combat operation scheme of a mobile air defense missile system in this mode is shown in FIG. 2.

The combat operation of a mobile air defense missile system in all the prescribed modes (in stand-alone, with centralized target designation, as part of the battery) can be effectively carried out both when deployed on the spot and when moving on the march. In the latter case, telecode radio communications are established between jointly operating air defense systems 13. When deployed at a stationary position between several air defense systems, both wire communications 12 (usually at short distances) and radio communications 13 can be used as part of the battery.

Sources of information:

1. Foreign Military Review, 1987, No. 3, p. 25-32.

2. Soldat und Technik, 1987, No. 4, p. 262.

3.Defense et Armement, 1989, No. 89, p. 76.

4. Equipment and weapons, 1999, p. 64-70.

5. Patent RU 2131577, publ. 06/10/1999.

6. Patent RU 2156943, publ. 09/37/2000.

7. Patent RU 2165582, publ. 20.04.2001.

8. Equipment and weapons, 1999, No. 5-6, p. 55-63.

Utility Model Formula

1. A mobile air defense missile system comprising a rotating turret mounted on a carrier, a launcher mounted on a turret with missiles equipped with homing heads, launcher guidance aids, communications, a digital computer and a control panel, characterized in that as a means target detection introduced a passive infrared station containing an infrared radiation receiver mounted on the launcher and made with the possibility of circular

of the survey, and the coordinate allocation unit connected to the infrared receiver installed in the tower and in turn

associated with a digital computer.

2. A mobile air defense missile system according to paragraph 1, characterized in that the passive infrared station installed on it is connected to several missile systems that are not equipped with means for detecting targets, with the possibility of transmitting target designation coordinates to them.

Mobile air defense missile system

Claims (2)

1. A mobile air defense missile system containing a rotating turret mounted on a carrier, a launcher mounted on a turret with missiles equipped with homing heads, launcher guidance aids, communications, a digital computer and a control panel, characterized in that as a means target detection introduced a passive infrared station containing an infrared radiation receiver mounted on the launcher and made with the possibility of a circular view, and yazanny with infrared radiation receiver coordinate extracting unit mounted in the turret and in turn connected to digital computer. 2. The mobile air defense missile system according to claim 1, characterized in that the passive infrared station installed on it is connected to several missile systems that are not equipped with means for detecting targets, with the possibility of transmitting target designation coordinates to them.