FIELD: defense equipment, in particular, mobile antiaircraft guided missile systems. SUBSTANCE: the firing section has an installation with a lighting and guidance radar composed of a multifunctional radar, whose input-output is connected by a busbar to the first input-output of a digital computer system, whose second input-output is connected by a busbar to the data receiving-transmitting equipment, the third input-output of the digital computer system is connected by a busbar to the navigation, topographical survey and orientation system. The output of the data measuring and input equipment is connected to the input of the digital computer system. The firing section has also a launcher with an antiaircraft guidance missile containing an equipment of the launcher data receiving-transmission, information-computer system, the second input-output of the information computer system is connected by a busbar to the input-output of the navigation, topographical survey and orientation system of the launcher, the third input-output of the information-computer system is connected by a busbar to the first input-output of the starting automatic equipment, the first input of the information-computer system is connected to the output of the data measuring and input equipment of the launcher. The output of the launch cycle forming device is connected to the input of the turbogenerator supply source, the third output of the launch cycle forming device is connected to the input of the chemical supply source. The firing section uses a supply source of the active channel, 2 AND logic unit and a switch of the active channel supply source, the input of the active channel supply source is connected to the first output of the starting automatic equipment, and the output is connected to the first input of the supply source switch, whose second input is connected to the output of the chemical supply source. EFFECT: produced a firing section, in which the launch of the antiaircraft guided missile with an active radar homing head and supply of the transmitting device of the active radar homing head is performed after a target "lock-on" signal, which results in "nullification" of the errors of target designation by angular coordinated at the moment of the launch of the antiaircraft guided missile and in direct estimation of the sufficiency of the level of the reflected signal for fulfillment of missile guidance on target. 1 dwg
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|---|---|---|---|
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|
RU2223459C1 |
| FIRING SECTION | 2003 |
|
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| FIRING SECTION | 2003 |
|
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| MOBILE ANTIAIRCRAFT GUIDED MISSILE SYSTEM | 2003 |
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|
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| SELF-PROPELLED COMPLEX WITH SURFACE-TO-AIR MEAN-RANGE SEMIACTIVE-HOMING RF-CONTROL MISILES | 2008 |
|
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| MOBILE FIRING UNIT FOR DETECTION, TRACKING AND ILLUMINATION OF TARGETS, DIRECTION AND MISSILE LAUNCHING OF AIR DEFENSE SYSTEM OF MEDIUM RANGE | 2007 |
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| SELF-PROPELLED TURRET OF DETECTION, TRACKING AND ILLUMINATION OF TARGETS, OF ORIENTING AND LAUNCHING MISSILES OF MEDIUM RANGE AIR DEFENCE MISSILE SYSTEM | 2012 |
|
RU2518389C1 |
| MULTIPURPOSE RADAR STATION OF TARGET DETECTION, ILLUMINATING OF TRACED TARGETS AND PROMPTING OF ROCKETS OF SURFACE-TO-AIR MISSILE SYSTEM OF AVERAGE OPERATING RANGE | 2007 |
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