RU54212U1 - RADAR STATION - Google Patents

Abstract

Technical field; radar, export version.

The essence of the utility model:

By making changes to the design of the 40BB (M) tower (shortening the boom of the tower, changing the design of the upper strut, stretch marks, frame of the tower), the F5MU antenna post was transported to the tower chassis, which significantly reduces the folding-deployment time of the 76N6 radar (by 2-3 times ), with a slight decrease in the detection range of low-altitude targets. Due to the use of gas turbine power units (type GAP-75, SES-75 (M) or similar) as means of power supply to the radar 76N6, as well as the use of power take-off generators (type SEP-2L, GOM-20 or similar) from engines KRAZ-260 (255), MAZ-537G tractors carry out multiple backups of the 76N6 radar power supply and shorten the deployment-deployment time of the 76N6 radar. At the same time, the power supply facilities are equipped with a thermal insulation system for the exhaust pipes of the HAP and exhaust exhaust pipes, cooling (several times) and exhaust pipes, which will increase the survivability of the 76N6 radar when using missiles with thermal imaging (thermal) homing heads (homing heads) on it, an increase in the secrecy of its work (a decrease in the reconnaissance range of operating power supply facilities), including during the march of the 76N6 radar. Due to the equipment of the 76N6 radar with pro-fragmentation armor plates, casings and anti-fragmentation, the survivability of the 76N6 radar will significantly increase when anti-radar missiles (PRR) are used on it, missiles with television, thermal imaging and thermal seekers, anti-tank guided missiles (ATGMs) (when attacking non-helicopters) missile shells (NURS), air bombs (guided and free fall), as well as other means of destruction, including during the march.

Due to the equipment of the 76N6 radar with the equipment for transmitting radar and command information to RPN 30N6E (30N6B1, 30N6B2) via the radio channel (from the composition of the 96L6B radar or similar), the coagulation and deployment time of the 76N6 radar is significantly reduced, its survivability increases (due to the use of the 2nd communication channel except cable). Due to the equipment of the 76N6 radar, an autonomous navigation, topographic and orientation (ANTO) system (from the S-300VM air defense system or similar) and the successor to the GLONAS satellite navigation system, its mobility and autonomy are increased.

Due to the equipment of the radar 76N6 integrated ground-based radar interrogator (NRZ) - to determine

the nationality of the targets (from the composition of the radar 96L6E or similar), the efficiency of its work increases due to the exclusion of target designation RPN 30N6E (30N6E1, 30N6E2) for its aircraft (aircraft, helicopters, etc.), which is essential for a complex and rapidly changing air defense environment battlefield.

Due to the equipment of the 76N6 radar active, adaptive to changing the interference environment of the phased array antenna (AFAR) and equipment for processing received radar signals, including microcomputers and / or computers using microprocessors (from the radar 96L6E or similar), it is possible to detect targets not only on small heights, but also at medium and high (with a malfunction of the F5MU antenna post and at low altitudes), including in the sector of deceleration of rotation of not only aerodynamic, but also ballistic targets. Application of AFAR will allow solving problems, including target recognition, selection of false and true goals, etc.

Description

1. Area of technology

This utility model relates to radar equipment exported by air defense vehicles.

2. The level of technology

In the existing main version of the 76N6 radar station (prototype), for lifting and placing the F5MU antenna post at the working height of use, the 40V6 (M) tower is used (see the attached photocopy of the figure 1-76N6 radar in the working position, where the 1-antenna F5MU post, 2-boom tower 40V6). When changing positions, the S-300PMU, PMU-1, PMU-2 anti-aircraft missile division (SAM) 90ZH6E, 90ZH6E1, 90ZH6E2 anti-aircraft missile system) the F5MU antenna post is detached from the 40V6 (M) tower and reloaded using a crane beam towers 40V6 (M) on a transport vehicle (TM) 5T58 (as part of a wheeled tractor KRAZ-260 (255) and the wagon itself with the F5MU antenna post). The tower 40B6 (M) itself is transported using the MAZ-53 7G wheeled tractor (indicated in figure-2, as-1, tower 40B6 is indicated in figure-2, as-2). In addition, another 5T58 transport vehicle is used to transport the 76N6 radar, with the F52MU hardware container and MK-1 mounting kit placed on it. Power supply of the 76N6 radar is carried out using a diesel power station (DES) 5I57A and a distribution converter (RPU) 5I58A, for the transportation of which two KRAZ-265B tractors are used. Thus, 5 vehicles are used to transport the 76N6 radar. Upon arrival at a new position, the F5MU antenna post is docked to tower 40B6 (M) using a crane beam of tower 40B6 (M). The process of coagulation, deployment and change of position of the 76N6 radar is laborious and lengthy in nature, which does not meet the mobility requirements for the technology of anti-aircraft missile forces (ZRV). The time-consuming and lengthy nature is laying and winding up the cable economy from the 76N6 radar to the light and guidance radar (RPN) 30N6E, 30N6E1, 30N6E2 of the anti-aircraft missile system (SAM) 90ZH6E, 90ZH6E1, 90ZH6E2 which includes 76N6 radar.

Significant disadvantages of the radar 76N6 in addition are:

1) The height limit of the detected targets (see the attached TTX radar 76N6S - figure 3), which makes it difficult to conduct independent actions air defense 90ZH6E, 90ZH6E1, 90ZH6E2;

2) The lack of an integrated radar interrogator (NRZ), which can lead to complex and rapidly changing environments

air combat to the introduction of target designation for their aircraft and distraction calculation from work on targets, etc. etc.;

3) Low survivability when using radar 76N6 anti-radar missiles (PRR), for example type HARM (US Air Force) or ALARM (UK Air Force), missiles with thermal and thermal imaging homing heads (such as "Mayverick");

4) The lack of a built-in autonomous system of orientation and topographic location.

The appearance and performance characteristics of the 76N6 radar are given, including in the Russian Arms catalog, volume 5, Armament and Military Equipment of the Air Defense Forces (1996-1997) (edition of the Military Parade company "(Russian Federation)), in the catalogs" Arms of Russia-2000 "," Arms of Russia 2001-2002 "," Arms of Russia 2004 ", as well as in the magazines" Military Parade "No. 6, 1999 (p.99), No. 6, 2000 (p. 79).

RLS 76N6S variant (analogue), developed by the manufacturer of RLS 76N6-Lianozovsky Electromechanical Plant (LEMZ) and the Defensive Systems company, with the F5MU antenna post and the F52MU hardware container powered by a gas turbine power supply unit located on the same MAZ-543 chassis ( HAP) (see the attached prospectus, figure 3), has a number of significant drawbacks:

1) The elevation height of the antenna center of the F5MU antenna post is clearly insufficient, which will lead to increased reflections from the underlying surface, a decrease in the detection range of targets, difficulties in choosing a position - it is necessary to place this version of the 76N6 radar at heights, with virtually no forest cover, which is only possible in the steppe, but on the hills in the coastal areas;

2) Low survivability, so when hit by radar 76N6S PRR HARM (US Air Force), ALARM (British Air Force) or when pointing a rocket with a thermal, thermal imaging seeker, the calculation in the F52MU container will die, and all Radar 76N6S, including the MAZ-543 chassis.

3) HAP does not have a thermal insulation, cooling and exhaust system.

3. Disclosure of utility model

Tower 40B6 (M) (figure-4, designated as-2), previously used only for lifting to the working height of the antenna post F5MU (see photocopy of figure 1-radar 76N6 in working position, antenna post F5MU designated as-1 ), will be applied, after changing its design - mainly shortening the boom of the tower (indicated on the photocopy of figure 1, as-2), stretch marks (reference in figure 1, as-4), changing the design of the upper strut (reference to figure 1, as-3), the new

appointment: including for transportation of the antenna post F5MU (see the attached drawing-figure-4, antenna post F5MU, marked -4), which will lead to a significant reduction in the time of coagulation and deployment of the radar 76N6 (presumably not less than 3 times), with a practically insignificant decrease in the detection range of low-altitude targets (the expected height of the antenna center of the F5MU antenna post is 15 meters), with the course position being correctly selected for the 76N6 radar: at the prevailing height, with minimal closing angles, with optimal bosom of the antenna system antenna post F5MU elevation.

The formula for determining the detection range of a low-altitude target (range of direct visibility) is:

where ha is the height of the radar antenna,

Нц - the flight altitude of the target,

4.12 - coefficient taking into account normal refraction.

From this formula it can be seen that the detection range of the low-altitude target of the 76N6 radar will decrease slightly. When flying a target at an altitude of 50 meters (with ha РЛС 76Н6 = 24m) it will be 49km, and Ext. (with ha 76N6 radar = 15m) will be 45 km.

To increase the mobility of the 76N6 radar, GAP-75 gas turbine power units (75 kW) or similar will be used as power supplies, which is sufficient for the 76N6 radar (in the first 3 minutes after turning on, the radar power consumption is not more than 65 kW (real - about 60 kW), the rest of the time after switching on, the power consumption is not more than 58 kW (actually 40-50 kW) .In order to reduce infrared visibility, the GAP-75 high-temperature exhaust gases will be cooled by passing the GAP-75 exhaust pipe through a heat exchanger with atmospheric air pumped through it using a 242BO-14-2 fan (or similar), as well as these gases will be cooled and removed from the 76N6 radar using a 3-knee (10-meter knee) flexible, quick-disconnect (connectors as used for connecting fire hoses to fire engines), a metal pipe (sleeve).

The main GAP-75 is located on the chassis of the KRAZ-260 (255) tractor transporting TM 5T58 with AK F52MU and MK-1. The backup GAP-75 is located on the chassis of the MAZ-537G tractor (there is similar experience in the MAZ-537D tractor version). The second variant of GAP-75 placement: the main GAP-75 on TM 5T58, backup on the 40V6 (M) tower chassis. In addition, wheeled tractors KRAZ-260 (255), MAZ-537G are equipped with power take-off generators of the SEP-2L, GOM-20 type to provide power to the 76N6 radar during the operation of tractor engines.

To increase the survivability of the 76N6 radar when using various means of destruction on it (PRR, NURS, aerial bombs, etc.), it is necessary to equip the F52MU hardware container, the F5MU antenna post, especially important parts (engine, cabin, including seats - from the bottom and back , fuel tanks and fuel lines) of MAZ-537G and KRAZ-260 (255) wheeled tractors from the outside with anti-shatter armor plates and covers (from aluminum armor - used, for example, in BMP-3 or armor steel), and from the inside with anti-shatter lining (from armor nylon or Kevlara) for localization zab Onewa action fragments. To assess the effectiveness of this event and measures to reduce the temperature of the exhaust and exhaust gases GAP-75, it is advisable to bombard a prototype of the 76N6 radar with domestic weapons (PR-X-25MP, MPU, X-31P, X-29T / TE / L, X missiles -59M, NURS, air bombs KAB-500KR, KAB-1500KR, etc.). At the same time, check the equipment with the name "Gazetchik" and the PRS mode of the radar 76N6. In addition, it must be borne in mind that the Gazetchik equipment can simply fail, as a result of electrical or mechanical failures. It would be good to fire at 76N6 radar and foreign means of destruction, if possible, with the corresponding conclusions.

To increase the mobility, survivability and autonomy of the 76N6 radar, it is necessary to equip it with a system for transmitting radar and command information to the F2U (UM) hardware container over the air (from the 96L6E radar). If there is time and opportunity and to increase stealth, communication can be done via cable.

To increase the mobility and autonomy of the 76N6 radar, it is necessary to equip it with navigation, topographic and orientation (ANTO) equipment from, for example, the S-300VM air defense system, supplementing it with the GLONAS receiver (global navigation system).

As a built-in NRZ it is necessary to use the equipment NRZ RLS 96L6E. At the same time, the receiver and receiver of the NRZ is located in the F5MU antenna post (in place of the spare parts cabinet, the spare parts cabinet is moved to another place), and the NRZ control equipment in the F52MU hardware container. The antenna of the NRZ is located on the roof of the AK FA52MU in one unit with the phased array of target detection at medium and high altitudes.

To ensure independent operation of the S-300PMU, PMU-1, PMU-2, 76N6 radar, to detect targets at medium and high altitudes, it is necessary to equip an active, adaptive to changing interference environment PAR, while placing the PAR itself on the roof of the F5MU antenna post - in the direction opposite to the F5MU antenna device, in the same unit as the NRZ antenna, the control, verification and tuning equipment in the F5MU antenna post, and the equipment for processing received radar signals and calculating target coordinates, including a microcomputer and / or computers on a microprocessor sors, in hardware F52MU container. When transporting AP F5MU PHAR

stacked on the roof of the AP F5MU using 2 hydraulic cylinders. The tempo of the space survey can be either 3s (20 revolutions per 1 minute) - when searching at low altitudes, or 6 seconds (10 revolutions per 1 minute) - when searching at medium and high altitudes. Space survey programs for AFAR can be:

1) When searching for aerodynamic targets - in azimuth - 360 degrees, in elevation from 1 to 14 (20) degrees, the rate of view of the space is 6 s (10 rpm).

2) When searching for ballistic targets - in azimuth in the sector of deceleration of rotation - 120 degrees, in elevation in the same sector - up to 55 (60) degrees. In the rest of the sector, in elevation from 1 to 14 (20) degrees.

3) When searching for low-altitude targets - by elevation 0-1 degrees, azimuth of 360 degrees, viewing speed 3s.

4. A brief description of the drawings.

The attached photocopy figure 1- shows the radar 76N6 in working position, where: 1-antenna post F5MU, 2-boom tower 40V6 (M), 3-top strut, 4-stretch.

In the drawing - figure 2 shows the tower 40B6 (M) in the stowed position, where: 1-tractor MAZ-537G, 2-tower 40B6 (M).

On the attached prospectus, the figure 3-depicts the 76N6S radar and its tactical and technical characteristics.

In the drawing - figure 4 shows the tower 40B6 (M) in the stowed position with the antenna post F5MU on the chassis, where: 1-tractor MAZ-537G, 2 tower 40V6 (M), 3-top strut, 4-antenna post F5MU, 5 -active PAR in transport position.

5. Implementation of a utility model.

To ensure the possibility of transporting the antenna post F5MU to the chassis of the 40V6 (M) tower, it is necessary to change the design of the tower and in particular:

1) Shorten the boom of the tower by eliminating 3 boom sections (at the welds) (see cop. Cop. 1-radar 76N6 in working position, designate as-2) by about 9 meters, with the corresponding change electrical installation and installation of the hydraulic system.

2) Change the design of the upper strut, see cop. cop.Fig. 1-radar 76N6 in the slave. floor, reference as-3), making it retractable and retractable, using a hydraulic cylinder (similar to how an arrow was made in the Ivanovets truck crane, that is, the retractable part of the strut is retracted and extends stationary inside) with fixation in two positions (extended and retracted) with hydraulic locks, to ensure, if necessary, undocking and undocking of the antenna post F5MU. In addition, you can undock and undock the F5MU antenna post with

using a K-162M truck crane or any other, with a carrying capacity of at least 12 tons.

3) Reduce the length of stretch marks (see cop. Cop. 1-radar 76N6 in working position, designation as-4) by 9 meters, without changing their designation.

4) Lengthen the frame of the tower 40V 6 (M) by 0.5 meters (by welding the corresponding site) to accommodate the rear support of the antenna F5MU (see figure 4).

5) Change (shorten) the ladder of the tower boom by about 9 meters (see figure 4).

These changes in the design of the 40V6 tower can be carried out at one of the RVTI (weapon and technical property repair) plants in Russia, with the participation of the Lianozovsky Electromechanical Plant (LEMZ), and, if necessary, the factory manufacturing the 40V6 tower: Novokramatorsky Machine-Building Plant (NKMZ), ( Kramatorsk, Ukraine), (of course it is more expedient at NKMZ).

After the implementation of the above changes, the coagulation-deployment time of the 76N6 radar will decrease several times. So, at least 3 operations will be excluded when rolling out the radar (taking together - 28 minutes):

1) installation of the strut in the position of the crane beam and the attachment of suspensions, taking 13 minutes in time (time is given in accordance with the maintenance instructions for tower 40B6 (40B6IO), p. 218, 219);

2) undocking the antenna post F5MU, which takes 6 minutes, according to 40V6IO;

3) folding the strut into the stowed position and removing the suspensions, taking 9 minutes - according to 40V6IO.

When deploying a 76N6 radar, at least 3 operations are excluded (taking a total of 30 minutes):

1) installation of the strut in the position of the crane beam and the attachment of suspensions, taking according to 40V6IO -13 minutes;

2) docking of the antenna post F5MU, taking according to 40V6IO -8 minutes;

3) folding the strut and remove the suspensions, taking time according to 40V6IO - 9 minutes.

Saving time of 28-30 minutes when rolling up and deploying the 76N6 radar for air defense missiles 90ZH6E (90ZH6E1, 90ZH6E2) is of great importance.

To reduce the coagulation and deployment time of the 76N6 radar, for its power supply it is necessary to use gas turbine power units of the GAP-75 type (SES-75, SES-75M or similar), with a power of at least 75 kW, placed in two versions. In the first embodiment, the GAP-75 (SES-75 (M)) is located on the chassis of the KRAZ-260 (255) and MAZ-537G tractors (the first option is more preferable, since it allows you to have one cooling system and exhaust gas as GAP-75 (SES-75), so

and the tractor engine), in the 2nd embodiment, the GAP-75 are placed on the TM 5T58 and the chassis of the 40V6 tower. Tractors KRAZ-260 (255) and MAZ-537G are equipped with power take-off generators of the SEP-2L type (GOM-20 or similar) to provide power to the 76N6 radar during the operation of tractor engines. As can be seen from the foregoing, multiple backups of the 76N6 radar power are carried out. At the same time, both GAP-75 (SES-75) and tractor engines are equipped with cooling and exhaust systems for high-temperature (GAP-75 exhaust gas temperature of about 850 degrees Celsius) exhaust gases. The exhaust gas cooling system of the KRAZ-260 (255) and MAZ-537G tractors is also used on the march (when changing the position of the 76N6 radar). To cool the exhaust gases, it is proposed to use a system of 1 or 2 (arranged in series) heat exchangers (through which atmospheric air will be pumped using fans 242BO-14-2 or similar) to which the GAP-75 exhaust pipe will be connected and in parallel the exhaust pipe from the engine of the tractor KRAZ-260 (255) or MAZ-537G is connected. In addition, the exhaust gases will be cooled and discharged using a 3-elbow (10-meter elbow), flexible, quick-detachable (connectors according to the type used to connect fire hoses to fire engines) pipes (hoses). Supposedly, the exhaust gases of the HAP and engines will be cooled at least several times. Through the use of autonomous power supply, the coagulation and deployment time of the 76N6 radar will be reduced. For thermal insulation of the exhaust pipes of the HAP, exhaust exhaust sleeves, composite sheets based on foams or polyurethanes are used.

Due to the fact that the F52MU hardware container, the F5MU antenna post, gas turbine power units and wheeled tractors KRAZ-260 (255), MAZ-537G do not have protection against fragments of PRR, NURS, aerial bombs and other means of destruction, they must be equipped outside (hardware containers, HAP, tractor cabs (including seats below and behind), tractor engines, fuel tanks, fuel lines) with shatterproof armor plates and covers (for example, from aluminum armor used in the BMP-3 or armored steel, and inside the equipment containers and tractor cabs fragmentation lining (from armored nylon or Kevlar) to localize the wagon action of the fragments. During the implementation of this measure, the 76N6 radar will have protection against fragments. The effectiveness of this measure must be checked in a practical way, that is, by shelling the 76N6 radar with domestic weapons: Kh-25 MP missiles (MPU), X-31P, X-29T / TE / L, NURS, air bombs.

To reduce the coagulation - deployment, increase survivability and autonomy radar 76N6, it is equipped with equipment for transmitting radar and command information to RPN 30N6E (30N6E1, 30N6E2) via a radio channel (with directional antenna)

from the composition of the radar 96L6E or similar. At the same time, the transceiver equipment, antenna devices of the radio data transmission system are located respectively on the RPN 30N6E (30N6E1, 30N6E2) chassis and on the chassis of the transport vehicle (TM) 5T58, as well as in the F52MU hardware container. The implementation of this measure will significantly reduce and facilitate the coagulation - deployment of the 76N6 radar, and will also provide another communication channel (except for cable) via the 76N6-RPN 30N6E radar line (30N6E1, 30N6E2).

To increase the mobility and autonomy of the 76N6 radar, it is necessary to equip it with navigation, topographic and orientation (ANTO) equipment from the S-300VM or similar. At the same time, this equipment is located in AK F52MU and on the chassis of the 40V6 (M) tower. AK F52MU is equipped, in addition, with the receiver of the satellite navigation system - GLONAS or similar. Compared with the orientation with the help of the PG-1M panorama and the 1T12-2M topographic bin, the orientation time of the 76N6 radar will be reduced several times.

To unify and facilitate the modernization of the 76N6 radar, as the integrated ground-based radar interrogator (NRZ), it is necessary to use the NRZ radar 96L6E equipment. At the same time, the NRZ transceiver is located in the F5MU antenna post (in place of the ZIP-1 A cabinet, the ZIP-1 A cabinet is reduced in volume and transferred to another location (fixed above the NRZ equipment)). The NRZ control equipment is located in the F52M hardware container. The antenna of NRZ is located on the roof of the antenna post F5MU and is a phased antenna array.

To detect targets at medium and high altitudes (if the F5MU AP malfunctions, or if necessary at low altitudes), the F5MU antenna post (AP) is equipped with an active phased array (AFAR) adaptive to changing the interference environment, which is located on the roof of the F5MU antenna post in the same block with the antenna NRZ, in the direction opposite to the antenna device F5MU. During transportation, the AFAR is laid on the roof of the AP F5MU using 2 hydraulic cylinders. The control equipment, checks and settings of AFAR, preliminary processing of targets are located in the AP F5MU (there are places for the corresponding blocks). Equipment for processing received target signals and calculating their coordinates (range, speed, azimuth, flight altitude), AFAR control equipment, noise protection equipment (auto-compensation for interference on the side lobes of the AFAR radiation pattern) and automatic tuning of the frequency of the emitting signal (according to the minimum interference level), equipment direction finding of interference jammers of active interference, equipment for setting paths of targets (with the exception of false paths, including those formed artificially from strategic and tactical aircraft ), Information exchange apparatus with RNP 30N6E (30N6E1, 30N6E2) located in hardware F52MU container (while it

includes micro computers and / or computers on microprocessors). For the basis of this equipment, you can take the appropriate radar equipment 96L6E or similar. The use of AFAR will allow, inter alia, solving problems of recognition of aircraft, selection of false and true targets, etc.

It is possible to operate the 76N6 radar even with the lowered boom of the 40V6 (M) tower on the horizontal flange of the tower (if position allows: at a prevailing height with virtually no vegetation cover, in the absence of positive closing angles, in flat, treeless terrain (in the steppe, desert, etc. .)), if there is no need to raise the 40B6 (M) tower boom to a vertical position. At the same time, measures must be taken to level the AP F5MU in the lower position and ensure its safe operation during rotation, which is technically possible.

It is necessary to halve the time for lowering and raising the boom of the 40V6 (M) tower (not 10 minutes, but 5 minutes), respectively, to reduce the time spent working out the F5MU antenna post from the working position to transport and vice versa, which is technically possible.

In the working position, the appearance of the modified radar 76H6 will be almost the same as the prototype depicted in figure 1, taking into account the changes. Power supply will be provided from the main or backup HAP, and in case of failure from the HOM. Communication with RPN 30N6E (30N6E1, 30N6E2) will be carried out by radio or cable, depending on the current situation. To detect targets at medium and high altitudes (in the event of a malfunction of the AP F5MU, then at low altitudes), AFAR will be used. To determine the state of ownership of the goals will be used NRZ. To translate into a stowed position, the boom of the 40V6 (M) tower together with the F5MU antenna post will lower from a vertical to a horizontal position (it is necessary to provide for a stop of the boom of the tower at an angle of about 20-30 degrees, if the F5MU AP does not finish working out in elevation to transport position - until the end of the antenna post completion by elevation to the transport position, as well as to realize the technically possible reduction in the time for lowering the tower boom to the horizontal position from the vertical and testing of the antenna post F5MU elevation from the working position into the transport (reducing them 2-3 times and align them with each other in time)) as depicted in Figure 4, the radar 76N6 other means are also translated to the stowed position. After the march, the 76N6 radar is transferred to the operating position, if necessary.

Note:

1) The 76N6 radar has been exported by the Russian Federation (to Greece and China) and is not an object of state secret, therefore, an application for it cannot be classified.

Claims (5)

1. A radar station (radar), consisting of an antenna post, a hardware container, a tower, wheel tractors, power supplies, characterized in that by reducing the length of the tower boom, top strut and stretch towers, the antenna post is transported to the tower chassis; radar power is supplied from gas-turbine power units or from power take-off generators from wheeled tractor engines equipped with thermal insulation, cooling and exhaust systems; a hardware container, an antenna post, gas-turbine power units, a cabin, an engine, fuel tanks, fuel lines of wheeled tractors are equipped with shells on the outside with shells, and on the inside with shell-splinter lining. 2. The radar according to claim 1, characterized in that it is equipped with equipment for transmitting to the radar illumination and guidance (RPN) radar and command information over the air. 3. The radar according to claim 2, characterized in that it is equipped with an autonomous navigation, topographic and orientation (ANTO) system and a satellite navigation system receiver. 4. The radar according to claim 3, characterized in that it is equipped with a built-in ground-based radar interrogator (NRZ) with a transceiver antenna in the form of a phased array antenna (PAR). 5. The radar according to claim 4, characterized in that the antenna post is equipped with an active, adaptive to changing interference environment, phased array antenna (AFAR) for detecting targets at medium and high altitudes (if the antenna post is malfunctioning and at low altitudes), has a digital a phase calculator (CVC) for controlling the active headlamp and a high-frequency receiver for pre-processing the received radar signals, and the hardware container is equipped with control equipment for the active headlamp, processing equipment for the received radar systems catch and calculating coordinates of targets consisting of a microcomputer and / or a computer microprocessor.