SOV - 5N64 / 64N6 (prehľadový rádiolokátor)

OVERVIEW RADIATORS 5N64 and 64N6



History:


The efforts of several generations of specialists from many scientific research institutes and design offices created many anti-aircraft missile systems and complexes securing the air borders of present-day Russia in the former Soviet Union. One of the best known systems today is the anti-aircraft missile system S-300PMU-1 ( & # 1057 ; -300 & # 1055; & # 1052; & # 1059; 1) with automated command system 83M6, anti-aircraft missile system S-300V ( & # 1057; -300 & # 1042;) and the anti-aircraft missile complex "Buk-M1" (" & # 1041; & # 1091; & # 1082; - & # 1052; 1"), which in many parameters they represent the current world leader in their category. This is achieved, among other things, thanks to the qualities achieved by surveillance radars used in system assemblies (also called RKO circular horizon radars)
These radars are developed in FGUP "NIIIP" Novosibirsk ( & # 1060; & # 1077; & # 1076; & # 1077; & # 1088; & # 1072; & # 1083; & # 1100; & # 1085; & # 1086; & # 1077; & # 1075; & # 1086; & # 1089; & # 1091; & # 1076; & # 1072; & # 1088; & # 1089; & # 1090; & # 1074; & # 1077; & # 1085; & # 1085; & # 1086; & # 1077; & # 1091; & # 1085; & # 1080; & # 1090; & # 1072; & # 1088; & # 1085; & # 1086; & # 1077; & # 1087; & # 1088; & # 1077; & # 1076; & # 1087; & # 1088; & # 1080; & # 1103; & # 1090; & # 1080; & # 1077; "& # 1053; & # 1072; & # 1091; & # 1095; & # 1085; & # 1086; - & # 1080; & # 1089; & # 1089; & # 1083; & # 1077; & # 1076; & # 1086; & # 1074; & # 1072; & # 1090; & # 1077; & # 1083; & # 1100; & # 1089; & # 1082; & # 1080; & # 1081; & # 1080; & # 1085; & # 1089; & # 1090; & # 1080; & # 1090; & # 1091; & # 1090; & # 1080; & # 1079; & # 1084; & # 1077; & # 1088; & # 1080; & # 1090; & # 1077; & # 1083; & # 1100; & # 1085; & # 1099; & # 1093; & # 1087; & # 1088; & # 1080; & # 1073; & # 1086; & # 1088; & # 1086; & # 1074; ") (Federal State Joint Undertaking" Measurement Equipment Scientific Research Institute ").


The development of radar equipment in this institute began in the middle of the 20th century, after the end of World War II. Due to the great importance of radar technology for the defense of the USSR and the provision of a unified base for research and development, it was decided on 15 August 1949 by the leadership of the Communist Party and Soviet Soviet ministers under No. 3516-1465 to establish the Scientific Research Institute 208 (& # 1053; & # 1048; & # 1048; -208), which was based on the decision of the Minister of Radar Industry of the USSR ( & # 1052; & # 1080; & # 1085; & # 1080; & # 1089; & # 1090; & # 1088; & # 1072; & # 1088; & # 1072; & # 1076; & # 1080; & # 1086; & # 1087; & # 1088; & # 1086; & # 1084; & # 1099; & # 1096; & # 1083; & # 1077; & # 1085; & # 1085; & # 1086; & # 1089; & # 1090; & # 1080; & # 1057; & # 1057; & # 1057; & # 1056;) of March 24, 1966 No. 160 renamed the "Scientific Research Institute of Measuring Instruments" ("& # 1053; & # 1072; & # 1091; & # 1095; & # 1085; & # 1086; - & # 1080; & # 1089; & # 1089; & # 1083; & # 1077; & # 1076; & # 1086; & # 1074; & # 1072; & # 1090; & # 1077; & # 1083; & # 1100; & # 1089; & # 1082; & # 1080; & # 1081; & # 1080; & # 1085; & # 1089; & # 1090; & # 1080; & # 1090; & # 1091; & # 1090; & # 1080; & # 1079; & # 1084; & # 1077; & # 1088; & # 1080; & # 1090; & # 1077; & # 1083; & # 110 0; & # 1085; & # 1099; & # 1093; & # 1087; & # 1088; & # 1080; & # 1073; & # 1086; & # 1088; & # 1086; & # 1074; ") and in 1999 received the status of Federal State Unified Enterprise" Scientific Research Institute of Measuring Devices " ( & # 1060; & # 1043; & # 1059; & # 1055; "& # 1053; & # 1048; & # 1048; & # 1048; & # 1055;" ).


In the beginning of its activity, the institute provided the production of measuring instruments and connecting means for radar means manufactured „ & # 1079; & # 1072; & # 1074; & # 1086; & # 1076; & # 1086; & # 1084; & # 1080; & # 1084; & # 1077; & # 1085; & # 1080; & # 1050; & # 1086; & # 1084; & # 1080; & # 1085; & # 1090; & # 1077; & # 1088; & # 1085; & # 1072; Later, after stabilizing the team of developers and mastering the necessary technologies, the institute began to develop and produce separate types of radar technology with a dual purpose:
- "OWN - FOREIGN" target recognition recognition systems
- surveillance radars (RKO - circular horizon radars)


Over the years, NIIIP has become a major site for the development and manufacture of ground-based instruments for target recognition systems. Until 1982 (when the production of NRZ devices was centralized at another manufacturer), the institute provided a large volume of production of ground recognition devices (NRZ - & # 1085; & # 1072; & # 1079; & # 1077; & # 1084; & # 1085; & # 1099; & # 1093; & # 1088; & # 1072; & # 1076; & # 1080; & # 1086; & # 1079; & # 1072; & # 1087; & # 1088; & # 1086; & # 1089; & # 1095; & # 1080; & # 1082; & # 1086; & # 1074; (& # 1053; & # 1056; & # 1047;)),


1950 - development of the "Krapiva" system completed (" & # 1050; & # 1088; & # 1072; & # 1087; & # 1080; & # 1074; & # 1072; ") for the autonomous NRZ Kremnyj-1 (" & # 1050; & # 1088; & # 1077; & # 1084; & # 1085; & # 1080; & # 1081; -1 ")


1955 - completed development of the Tantal-3 system for NRZ Kremnyj-2 intended for incorporation into other radars.


1955 - Malachite system development completed (" & # 1052; & # 1072; & # 1083; & # 1072; & # 1093; & # 1080; & # 1090; ") for a radio theodolite of complex atmospheric monitoring. This device has gained great expansion not only in the USSR but also abroad (it was successfully used, for example, by the first Soviet Antarctic expedition in the International Year of Solar Monitoring).


1957 - development of the "Kopija" radar system completed (" & # 1050; & # 1086; & # 1087; & # 1100; & # 1077;[/i ] ") (chief designer of AI Rasskazov ( & # 1040;. & # 1048 ;. & # 1056; & # 1072; & # 1089; & # 1089; & # 1082; & # 1072; Â & # x20AC; & # x153; The radar-controlled lighting system also enabled the guidance of its own fighter aircraft.


1960 - Completed development of "Céder" and "Quantum" systems (" & # 1050; & # 1077; & # 1076; & # 1088; "a" & # 1050; & # 1074; & # 1072; & # 1085; & # 1090; ") (chief designer of AA Jurov ( & # 1040;. & # 1040 ;. & # 1070; & # 1088; & # 1086; & # 1074;)) for NRZ Kremnyj-2M (" & # 1050; & # 1088; & # 1077; & # 1084; & # 1085; & # 1080; & # 1081; -2 & # 1052; ").


1960 - completed work on the "Shar" system (" & # 1064; & # 1072; & # 1088;") - used for verification and research of possibilities of antennas with electronic beam deflection (FAR antennas).


1962 - completed work on the "Mockup" system (" & # 1052; & # 1072; & # 1082; & # 1077; & # 1090;[/i ] ") - for the needs of research into optimal processing of composite signals


1965 - completed work on the unified radar of the circular horizon 1S12 (1RL111D) ( 1 & # 1057; 12 ( 1 & # 1056; & # 1051; 111 & # 1044;)) - mobile radar on one crawler chassis, with preparation time for combat use approx. 5 min. Radar 1S12 was used in PLRK 2K11 "Krug"., 1RL111D in cooperation with an altimeter at radar survey stations. Behind this radar was the chief designer V.V Rajzberg ( & # 1042;. & # 1042 ;.& # 1056; & # 1072; & # 1081; & # 1079; & # 1073; & # 1077; & # 1088; & # 1075;) became a laureate of the Lenin Council in 1967 ( & # 1051; & # 1072; & # 1091; & # 1088; & # 1077; & # 1072; & # 1090; & # 1072; & # 1051; & # 1077; & # 1085; & # 1080; & # 1085; & # 1089; & # 1082; & # 1086; & # 1081; & # 1087; & # 1088; & # 1077; & # 1084; & # 1080; & # 1080; )


1965 - completed work on the "Beam" system (" & # 1051; & # 1091; & # 1095;") - tracking system beam deflections of electronically deflected beam antennas in perspective circular horizon radars.


1967 - completed work on the "Prism" system (" & # 1055; & # 1088; & # 1080; & # 1079; & # 1084; & # 1072 ; ") - research into the creation of multifunctional (multifunctional) radars with antennas formed by a phase antenna array. ( & # 1092; & # 1072; & # 1079; & # 1080; & # 1088; & # 1086; & # 1074; & # 1072; & # 1085; & # 1085; & # 1086; & # 1081; & # 1072; & # 1085; & # 1090; & # 1077; & # 1085; & # 1085; & # 1086; & # 1081; & # 1088; & # 1077; & # 1096; & # 1077; & # 1090; & # 1082; & # 1086; & # 1081; (& # 1060; & # 1040; & # 1056;)


1968 - completed modernization of the unified radar of the circular horizon 1S12A (1RL128D) ([ i] 1 & # 1057; 12 & # 1040; ( 1 & # 1056; & # 1051; 128 & # 1044;)), including increasing the target detection distance flying at low altitudes as in 1S12 (1RL111D) ( 1 & # 1057; 12 ( 1 & # 1056; & # 1051; 111 & # 1044;)) and also added the ability to partially measure the third coordinate of the target (position angle).


1971 - "Konus" system development completed (" & # 1050; & # 1086; & # 1085; & # 1091; & # 1089; "), which tested the possibilities of different variants of antennas with electronic beam deflection.


1975 - development of "Parol-4" systems completed (" & # 1055; & # 1072; & # 1088; & # 1086; & # 1083; & # 1100; -4 ") and" Parol-5 "(" & # 1055; & # 1072; & # 1088; & # 1086; & # 1083; & # 1100; - 5 ") for autonomous radar interrogators (NRZ, IFF) 71E6 ( 71 & # 1045; 6), 73E6 ( 73 & # 1045; 6), 75E6 ( 75 & # 1045; 6), 1L22 ( 1 & # 1051; 22), and built-in radar interrogators 1L23-6 ( 1 & # 1051; 23-6 ), 76E6 ( 76 & # 1045; 6), 1L24 ( 1 & # 1051; 24) and the Parol 1L26 ( 1 & # 1051; 26). With these systems, the NRZ of the "Parol" system became highly resistant to the processing of a false response signal and gained a high resistance to radio electronic interference. At the same time, a space was created for possible further improvement of this system.


1977 - development of the "Lúč-1" system completed (" & # 1051; & # 1091; & # 1095; -1") for ground radar interrogator 1RL246 ( 1 & # 1056; & # 1051; 246) (for anti-aircraft missile kits 9K31 Shot-1 ( 9K31 "& # 1057; & # 1090; & # 1088; & # 1077; & # 1083; & # 1072; -1") a 9K35 Strela-10 ( 9K35 "& # 1057; & # 1090; & # 1088; & # 1077; & # 1083; & # 1072; -10 ")) and 1RL 247 ( 1 & # 1056; & # 1051; 247 ) (for PPLRK 9K32 Strela-2 ( 9K32 "& # 1057; & # 1090; & # 1088; & # 1077; & # 1083; & # 1072; -2 ") a 9K34 Strela- 3 (9K34 "& # 1057; & # 1090; & # 1088; & # 1077; & # 1083; & # 1072; -3"))


1977 - Igla-1 system development completed (" & # 1048; & # 1075; & # 1083; & # 1072; -1 ") for NRZ 1L14 ( 1 & # 1051; 14) PPLRK 9K310 Igla-1 (" & # 1048; & # 1075; & # 1083; & # 1072; -1").The NRZs of these PPLRKs achieved better characteristics than their analogous American counterparts used in PPLRKs FIM-92 Stinger.


1977 - "Dome" system development completed (" & # 1050; & # 1091; & # 1087; & # 1086; & # 1083; ") for mobile unified circular horizon radar 9S18 ( 9 & # 1057; 18) (1RL135 ( 1 & # 1056; & # 1051; 135)) on one transport vehicle, comprising a mirror of an antenna using electronic beam deflection in a position angle with mechanical radiation control in azimuth. The system used had a deployment time of up to 5 minutes. Radar 9S18 ( 9 & # 1057; 18) is used in PLRK 9K37 „Buk“ (" & # 1041; & # 1091; & # 1082;") and circular horizon radar 1RL135 ( 1 & # 1056; & # 1051; 135) is used in radar survey stations.


1980 - development of the circular horizon radar 5N64 (chief designer of VV Rajzberg ( & # 1042; &. . & # 1056; & # 1072; & # 1081; & # 1079; & # 1073; & # 1077; & # 1088; & # 1075;), JA Kuznecov ( & # 1070;. & # 1040 ;. & # 1050; & # 1091; & # 1079; & # 1085; & # 1077; & # 1094; & # 1086; & # 1074;) system [ url=/viewtopic.php/t/39954] S-300P[/url] ( & # 1057; -300 & # 1055;). This radar was used for the first time with a double-sided phase antenna array with electronically controlled position angle deviation and mechanically controlled azimuthal deviation.This radar was manufactured in two modifications - 5N64K ( ] 5 & # 1053; 64 & # 1050;) - container variant a 5N64S ( 5 & # 1053; 64 & # 1057;) ( 5N64A ( 5 & # 1053; 64 & # 104 0;)) - self-propelled (automobile) variant, on the chassis and trailer of a heavy truck MAZ-74106 -9988 ( & # 1052; & # 1040; & # 1047; -74106-9988) in three containers. The development and preparation time for this radar is less than 5 minutes. Radar 5N64 ( 5 & # 1053; 64) provided tracking of targets within the needs of the command post PLRK S-300P (& # 1057; -300 & # 1055;).


1983 - development of the "Horizon-3" system completed (" & # 1054; & # 1073; & # 1079; & # 1086; & # 1088; -3 ") for the 9S15M Mobile Unified Circular Horizon Radar ( 9 & # 1057; 15 & # 1052;) (1RL140 ( 1 & # 1056; # 1051; 140)). RL 9S15M ( 9 & # 1057; 15 & # 1052;) is used in PLRK S- 300V ( & # 1057; -300 & # 1042;) and RL 1RL140 ( 1 & # 1056; & # 1051; 140[/i ]) for work in radar survey stations. In RL 9S15M ( 9 & # 1057; 15 & # 1052; (1RL140 ( 1 & # 1056; & # 1051; 140)) is used single-sided flat waveguide phased array antenna (from S-type waveguides ( & # 1064; - & # 1074; & # 1086; & # 1083; & # 1085; & # 1086; & # 1074; & # 1086; & # 1076; & # 1086; & # 1074;)) with electronically controlled beam at position angle and mechanical beam control in azimuth with variable speed.


1983 - Target Tracking Station development completed ( & # 1089; & # 1090; & # 1072; & # 1085; & # 1094; & # 1080; & # 1080; & # 1086; & # 1073; & # 1085; & # 1072; & # 1088; & # 1091; & # 1078; & # 1077; & # 1085; & # 1080; & # 1103; & # 1094; & # 1077; & # 1083; & # 1077; & # 1081; (& # 1057; & # 1054; & # 1062;)) 9S18M1 ( 9 & # 1057; 18 & # 1052; 1) belonging to PLRK "Buk-M1". This radar uses a single-sided flat waveguide phase antenna system and electronic beam deflection in the position angle and mechanical control in azimuth with variable speed.A 9S18M1E radar modification ( 9 & # 1057; 18 & # 1052; 1 & # 1069;) is produced for export.


1988 - radar development completed 64N6 ( 64 & # 1053; 6 automated system url=/viewtopic.php/t/40093] 83M6[/url] ( 83 & # 1052; 6) PLRK S-300PMU-1 ( & # 1057; -300 & # 1055; & # 1052; & # 1059; 1). The radar 64N6 is, unlike its predecessor 5N64, located in two containers on the same chassis MAZ-74106 -9988 ( & # 1052; & # 1040; & # 1047; -7410-9988), has increased target detection distance, improved immunity to radio interference, and reduced production requirements. The development time remained less than 5 minutes. Modification 64N6E ( 64 & # 1053; 6 & # 1045;) is intended for export.


1990 - completed development of the mobile radar of the circular horizon 9S15M2 ( 9 & # 1057; 15 & # 1052; 2) located on one transport vehicle for PLR S -300VM ( & # 1057; -300 & # 1042; & # 1052;). In addition to detecting the target, the radar is also able to process information about the target and is able to sell this information to the command post of the S-300VM system ( & # 1057; -300 & # 1042; & # 1052;) . In the radar, some analog radar information processing systems are replaced by digital systems. The system used has improved the processing of signals received from radio interference and is also easier to manufacture and maintain.

In the years 1990 -1999, the institute, like many other similar institutions of the USSR military-industrial complex, got into existential problems, but nevertheless retained the ability to research, develop and train future experts in the field of radioelectronics. research and development.
The institute is currently working on the modernization of current radar technology and on the development of next generations of radars.

PREHĽADVANCED RADIOLOCATOR 5N64


5N64(5Н64) - a circular horizon radar (over-the-horizon radar) with an electronically detected beam at a position angle, mechanically controlled beam steering in azimuth and with a two-sided antenna. Individual radar variants used in the PLRK S-300P (С-300П) and S-300PT (С-300ПT)


In the late 1960s, the Soviet Union completed the development of the first-generation anti-aircraft missile complexes providing effective defense against aerodynamic targets. On the basis of forecasts of the change in the nature of attack targets, other means of air attack and means of jamming, and the need for protection against operational tactical missiles and tactical ballistic missiles (which occupied an overlooked place among the means of air attack), it was decided that there was a need for the development of new antiaircraft missile assets for the air defense system of the state and the air defense system of ground troops.
The basic requirements were clear - mobility, the ability to detect, track and destroy ballistic missiles at long range. At the same time, these systems had to deal with the tasks of anti-missile and anti-aircraft defence and destroy aerodynamic targets over a wide range of altitudes


The importance of the overhead radar (RKO circular horizon radar) has increased rapidly. In addition, žthat this radar will most likely be the target of the first attack of the adversary by all means of anti-radio warfare (anti-radio warfare;missiles, various types of active and passive jamming) must be able to determine the coordinates of targets at a greater distance, with a greater speed of information recovery, even in conditions of various types of jamming.
In 1966, it was decided to develop an anti-aircraft missile system S-300(С-300). The development was divided into several designčn offices depending on the determination of the means, the development of the RKO for the systems S-300P (С-300П) and S-300V (С-300В) was given to the NIIIP design office.


Because of the increasing speed of targetsľand their maneuverability, development was also focused on the radar's ability to shorten ť čtime required for the recovery of radar information and to reduce the errors in determining the coordinates of the targets, which was to enable the tracking of the targets by the radar.
It was necessary to operatively adapt the radar to the radar situation. In order to ensure the accuracy of the coordinates of the targets even for small-sized targets in the distance and at the same time to suppress various noises and "echo" signals, the research found žthat the most suitable is to use an electronically enhanced beam, which also allows to divide the survey zone into a regular horizon zone and a target tracking zone. The regular horizon zone is a zone of false position angles and large distances - it is used to detect targets in the distance. The target tracking zone is an area of larger position angles and smaller distance - it ensures tracking of targets.


All this was implemented in the 5N64(5Н64) radar (chief designer V.V. Rajzberg (В.В. Райзберг), potom J. A. Kuznecov (Ю.А.Кузнецов) a G. N. Golubev (Г.Н.Голубев)).


The 5N64 (5Н64)radar is deployed in three containers:
- Antenna F6 (Ф6)
- receiving-transmitting F7 (Ф7)
- instrument F8 (Ф8).
After trials with the S-300P (С-300П) system had been underway since 1978, mass production began.


Versions:
- 5N64K (5Н64К) - container variant (stationary)
- 5N64S (5N64A) (5Н64С (5Н64А))- self-propelled (automotive variant)


The development of the 5N64 (5Н64) radar was completed in 1980 with the introduction of its self-propelled version mounted on a [url]9988[/url]ťahan ťahačom MAZ-74106 (МАЗ-74106-9988)


5N64S radar - the diagram shows the division of the superstructure into individual containers



5N64S radar:



As significant gaps in the technology used were identified during the development and production of the radar, it was decided in 1981 to upgrade the radar in parallel under the designation 64N6(64Н6), intended for the upgraded system S-300PM (С-300ПМ). The purpose of the modernization was to improve the radar's ability to detect even small-sized targets of various types of cruise missiles, increase protection against various types of interference and increase the number of tracked targets. The modernization was also aimed at reducing the requirements for radar preparation for combat use and prediction of the mean time between operations.

PREHĽADOVÝ RÁDIOLOKÁTOR 64N6


64N6 (kód NATO "Big Bird", alebo "Tombstone" (Jane's Land-Based Air Defence Book 2000-2001)) - mobilný prehľadový rádiolokátor s obojstrannou fázovou anténou, automatickým systémom zmeny režimu činnosti v závislosti na podmienkach a automatickým snímaním informácií pre ďašie spracovanie v automatizovanom systéme velenia. Rádiolokátor pracuje v centimetrovom pásme.


Je určený pre zabezpečenie rádiolokačnej informácie pre kabínu bojového riadenia 54K6 automatizovaného systému velenia 83M6 protilietadlového raketového systému S-300PM (S-300PMU1).


Rádiolokátor 64N6 zabezpečuje zistenie vzdušných cieľov s dostatočnou presnosťou na určenie trasy cieľa a jeho rýchlosti pri činnosti bez rušenia ako aj v podmienkach aktívneho a pasívneho rušenia. Zároveň zabezpečuje rozpoznanie príslušnosti cieľa (vlastný - cudzí), a určenie polohových súradníc cieľov vytvárajúcih aktívne rušenie.


Elektronické skenovanie lúčom FAM (fázovaná anténna mriežka) (ФАР — Фазированная антенная решетка) v azimute a v námere v spojení s rýchlym prepínaním smerov vyžarovania FAM a rovnomernou elektromechanickou rotáciou FAM v azimute umožňuje programové prerozdelenie vyžarovanej energie v rozličných smeroch a sektoroch zóny prehľadávania. Tento systém umožňuje v závislosti na vzdušnej situácii stanoviť obsluhe sektory kde rádiolokátor vykonáva len prehľadávanie priestoru a sektory kde vykonáva aj sledovanie vzdušných cieľov (prípadne určiť sektor kde vôbec neprebieha vyžarovanie, napr. z dôvodu možného rušenia iného rádiolokátoru a pod.). Týmto je dosiahnuté zníženie nárokov na prijímací systém hlavne v dvojstupňových režimoch sledovania v kombinácii s režimov selekcie pohyblivých cieľov (SPC - селекциa движущихся целей (СДЦ)). Hranice sektorov (v diaľke, výške a v azimute) činnosti SPC sú stanovované manuálne operátormi, alebo automaticky.


Anténa rádiolokátoru 64N6E2 (výstava MAKS 97)



Ochrana pred aktívnym rušením je zabezpečovaná automatickou zmenou nosnej frekvencie na základe výsledkov analýzy rušenia. Ochranu pred ktívnym rušením tvoreným bočnými lalokmi vyžarovacieho diagramu FAR zabezpečuje trokanálový autokompenzátor pripojený ku kompenzačným anténam.


Ochrana pred pasívnym rušením je zabezpečovaná aparatúrou SPC. Pre zmenšenie množstva klamných odrazov v blízkej zóne (na vzdialenosť 65 km) je do kanálu sledovania vložený blok ČARZ (временная автоматическая регулировка усиления (ВАРУ)) - časová automatická regulácia zosilnena. Z dôvodu zrušenia odrazov od terénnych predmetov v zóne nízkoletiacich ceľov je do prijímacieho kanálu vložený blok porovnávania signalov prijatých z toho istého miesta počas niekoľkých otáčok antény.


Režim činnosti rádiolokátora, spracovanie rádiolokačnej informácie a snímanie súradníc cieľov je zabezpečované výpočtovým systémompostaveným a báze dvoch špecializovaných počítačov (v ruskom originále EVM - elektro-vyčisliteľnyje mašiny). Rádiolokátor je vybavený autonómnym systémom kontroly funkčnosti, ktorý v prípade pouchy automaticky určí príčinu poruchy.


Rádiolokátor je vybavený hlasovým a dátovým komuikačným systémom. Širokopásmový komunikačný blok 5JA312 (5Я312) slúži na prenos dátovej informácie do kabíny bojového riadenia 54K6 systému 83M6 (alebo pre iný automatizovaný systém velenia) buď rádiovo, alebo linkovým spojením.


Rádiolokátor je vybavený nezávislým energetickým systémom 220V/400Hz, tvoreným elektrocentrálou. Napájaný môže byť tiež z vonkajšej siete 220V/50Hz (pomocou meniča 63T6A (63Т6А)), alebo zo samostatnej elektrocentrály 5I57A (5И57А).


Rádiolokátor je umiestnený v dvoch kontajneroch.
- kontajner F6 - anténny systém, prijímač, vysielač
- kontajner F8 - systémy ochrany proti rušeniu, spracovania informácie
Oba kontajnery sú miestnené na návese MAZ-9988 ťahanom ťahačom MAZ-74106. Obsluhu tvoria 4 osoby. Celková hmotnosť dosahuje 60 t.


Rádiolokátor 64N6





Varianty:
64N6E (64Н6Э) - pre S-300PMU-1
64N6E2(64Н6Э2) - pre S-300PMU-2

PREHĽADOVÝ RÁDIOLOKÁTOR 64N6E


Exportná verzia rádiolokátoru 64N6E (64Н6Е) bola v roku 1995 testovaná na polygóne Kapustin Jar (Капустин Яр) spolu s exportnou verziou automatizovaného systému velenia 83M6E (83М6Е) určeného pre riadenie bojovej činnosti systému S-300PMU11 (С-300ПМУ1).


Systémy rádiolokátoru sú schopné vykonávať automatickú kontrolu všetkých systémov s rôznou periodicitou a úrovňou. Na áklade výsledkov testov je rádiolokátor schopný upozorniť na hrozbu technických problémov a navrhovať riešenie na predídenie výpadkom v činnosti.


Rádiolokátor sa skladá z dvoch kontajnerov:
- prijímací a vysielací F6E (Ф6Е)
- prístrojový F8E (Ф8Е)
Obsluha v počte 4 osôb má svoje pracovisko v prístrojovom kontajneri.


Topopripojenie rádiolokátora sa vykonáva pomocou topopripojovača, ktorý je súčasťou komplexu.
Vlastný náves s vozidlom je vybavený elekktocetrálou SEC-75 (СЭС-75), ktorá zabezpečuje nezávislosť systému na napájaní, samozrejme je možné (a v praxi používané častejšie) napájať rádiolokátor z vonkajšej (priemyselnej) siete a z elektrocentrál komplexu. Ďalšie vybavenie tvoria prostriedky nočného videnia, prostriedky radiačného a chemického prieskumu, spojovacie prostriedky a súpravy náhradných dielcov (ZIP (ЗИП)).


Takticko-technické údaje (64N6E):


Zóna prehľadávania:
- azimut: 360°
- námer: 13,4° ( štandartný režim), 55° (sledovanie), do 75° (špeciálny sektor)
Diaľka zisteia cieľa (Mig-21): 260 km
Presnosť určenia súradníc:
- v diaľke: 200 m
- v azimute: 30´
- v námere: 35´
Obnovenie informácie o vzdušnej situácii:
- štandartný režim - 12 s (5 ot/min)
- sledovanie cieľov - 6/12 s (10/5 ot/min)
Počet súčasne sledovaných cieľov : 2x200 (každá FAM 200 cieľov)
Čas prípravy z pochodovej do bojovej polohy: 5 min


Rádiolokátor je schopný pracovať v rôznych meteorologických podmienkach, v zime i v lete bez ohľadu na dennú dobu, s teplotami do 50 °C, vlhkosťou vzduchu 98%, nadmorskej výšky 3000 m a rýchlosti vetra do 30 m/s (v prípade zloženej antény do 50 m/s).

Rádiolokátor 64N6



Rádiolokátor 64N6



Rádiolokátor 64N6E2 systému S-300PMU-2 "Favorit"

Zdroje: www.vko.ru
www.russianarms.ru
http://pvo.guns.ru
http://legion.wplus.net
old.vko.ru


A ešte zopár snímkov zo skúšok jednej z exportných verzií rádiolokátora 64N6E2:


























© Георгий ДАНИЛОВ