EA201600007A1 - ZENITNY ROCKET COMPLEX - Google Patents
ZENITNY ROCKET COMPLEXInfo
- Publication number
- EA201600007A1 EA201600007A1 EA201600007A EA201600007A EA201600007A1 EA 201600007 A1 EA201600007 A1 EA 201600007A1 EA 201600007 A EA201600007 A EA 201600007A EA 201600007 A EA201600007 A EA 201600007A EA 201600007 A1 EA201600007 A1 EA 201600007A1
- Authority
- EA
- Eurasian Patent Office
- Prior art keywords
- radar
- tracking
- guided
- launchers
- launcher
- Prior art date
Links
Landscapes
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Radar Systems Or Details Thereof (AREA)
Abstract
Заявлен зенитный ракетный комплекс (ЗРК), имеющий в составе как пусковые установки (ПУ) самонаводящихся зенитных управляемых ракет (ЗУР) с полуактивным радиолокационным самонаведением, так и ПУ телеуправляемых ЗУР с радиокомандным наведением. Информационное обеспечение ЗРК осуществляет радиолокатор обзора-сопровождения (РОС), который связан с постом боевого управления (ПБУ) ЗРК. При этом ПУ самонаводящихся ЗУР оборудованы радиопередающими устройствами подсвета с возможностью наведения антенны подсвета на цель, обстреливаемую с данной ПУ, а ПУ телеуправляемых ЗУР - радиопередающими устройствами команд управления с возможностью наведения антенны в направлении ЗУР, запущенной с данной ПУ. РОС содержит не менее 2-х выносных передатчиков подсвета (ВПП) с возможностью вращения веерной диаграммы направленности антенны (ДНА) и собственно активно-полуактивную радиолокационную станцию (АП РЛС) с возможностью трассового сопровождения целей в режиме кругового обзора и возможностью следящего сопровождения телеуправляемых ЗУР и обстреливаемой ими цели. АП РЛС имеет в составе две взаимно ортогонально ориентированные приемные фазированные антенные решетки (ПФАР), каждая из которых формирует набор парциальных ДНА, взаимно расстроенных на ширину парциального луча в соответствующей плоскости. При этом направление ДНА ВПП непрерывно согласовано с направлением ДНА ПФАР.Declared anti-aircraft missile system (ZRK), having as part of the launchers (PU) self-guided anti-aircraft guided missiles (SAM) with semi-active radar homing, and PU-controlled radio-guided missile launcher. The information support of the air defense missile system is provided by a survey-tracking radar (POS), which is connected with the combat command post (PBU) of the air defense missile system. At the same time, self-guided missile launchers are equipped with radio transmitting devices with the ability to target the antenna to the target being fired at this launcher, and remote control-controlled launchers with radio transmitters of control commands with the ability to direct the antenna in the launcher direction. The DEW contains at least 2 remote illumination transmitters (runways) with the ability to rotate the fan antenna pattern (DND) and the active semi-active radar station itself (AP radar) with the possibility of route tracking in a circular view mode and tracking tracking of remote-controlled SAM and they are shooting at a target. The AP of the radar consists of two mutually orthogonally oriented receiving phased antenna arrays (PPAR), each of which forms a set of partial DND, mutually upset by the width of the partial beam in the corresponding plane. The direction of the bottom of the runway is continuously aligned with the direction of the bottom of the PFAR.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EA201600007A EA030987B1 (en) | 2015-11-18 | 2015-11-18 | Air defence missile system |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EA201600007A EA030987B1 (en) | 2015-11-18 | 2015-11-18 | Air defence missile system |
Publications (2)
Publication Number | Publication Date |
---|---|
EA201600007A1 true EA201600007A1 (en) | 2017-05-31 |
EA030987B1 EA030987B1 (en) | 2018-10-31 |
Family
ID=58793981
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EA201600007A EA030987B1 (en) | 2015-11-18 | 2015-11-18 | Air defence missile system |
Country Status (1)
Country | Link |
---|---|
EA (1) | EA030987B1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2733600C1 (en) * | 2019-09-17 | 2020-10-05 | Федеральное государственное казенное военное образовательное учреждение высшего образования "Военная академия материально-технического обеспечения имени генерала армии А.В. Хрулёва" | Thermobaric method of swarm control of small-size unmanned aerial vehicles |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2102772C1 (en) * | 1985-12-29 | 1998-01-20 | Научно-исследовательский электромеханический институт | Control system of army close air defense missile complex |
US6414622B1 (en) * | 1999-12-21 | 2002-07-02 | Lockheed Martin Corporation | Anti-radar missile (ARM) countermeasure method |
RU2333450C1 (en) * | 2007-03-09 | 2008-09-10 | Открытое акционерное общество "Научно-исследовательский институт приборостроения имени В.В. Тихомирова" | Mobile firing unit for detection, tracking and illumination of targets, direction and missile launching of air defense system of medium range |
RU100213U1 (en) * | 2009-10-05 | 2010-12-10 | Открытое акционерное общество "Ульяновский механический завод" (ОАО "УМЗ") | COMMAND POST |
-
2015
- 2015-11-18 EA EA201600007A patent/EA030987B1/en not_active IP Right Cessation
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2733600C1 (en) * | 2019-09-17 | 2020-10-05 | Федеральное государственное казенное военное образовательное учреждение высшего образования "Военная академия материально-технического обеспечения имени генерала армии А.В. Хрулёва" | Thermobaric method of swarm control of small-size unmanned aerial vehicles |
Also Published As
Publication number | Publication date |
---|---|
EA030987B1 (en) | 2018-10-31 |
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Legal Events
Date | Code | Title | Description |
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MM4A | Lapse of a eurasian patent due to non-payment of renewal fees within the time limit in the following designated state(s) |
Designated state(s): AM AZ KZ KG TJ TM |
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MM4A | Lapse of a eurasian patent due to non-payment of renewal fees within the time limit in the following designated state(s) |
Designated state(s): BY RU |