FIELD: military equipment, in particular, mobile antiaircraft guided missile systems, applicable for organization of air defense of troops and military objects against destruction by the aids of enemy air attack.
SUBSTANCE: the mobile antiaircraft guided missile system for detection and destruction of aerodynamic, ballistic and winged missiles in a composition of series-connected target detection stations, fighting control point containing a data receiving-transmitting equipment, whose second output is connected to the digital computer system of the fighting control point, illumination and guidance radar set, launcher containing a series-connected data receiving-transmitting equipment, digital computer system of the launcher, rotatable launcher, antiaircraft guided missiles with a semiactive or active guidance methods. The third input of the digital computer system of the launcher is connected to the output of the navigation, topographical survey and orientation system. Used in addition is an air carrier with an illumination and guidance radar, having a series-connected multifunctional radar, digital computer system and an air carrier data receiving and transmitting equipment, the output of the air carrier data receiving and transmitting equipment is connected to the input of the fighting control point data receiving and transmitting equipment. The second input of the air carrier digital computer system is connected to the output of the navigation processor, whose first input is connected to the output of the receiver of processing of radionavigational signals, and the second input is connected to the output of the inertial system, the fighting control point uses also a series-connected receiver of processing of radio-navigational signals and a navigation processor of the fighting control point, whose output is connected to the second input of the digital computer system of the fighting control point.
EFFECT: enlarged distant boundary of detection of low-altitude targets.
7 dwg, 1 tbl
| Title | Year | Author | Number |
|---|---|---|---|
| FIRING SECTION | 2003 |
|
RU2229668C1 |
| FIRING SECTION | 2003 |
|
RU2229085C1 |
| FIRING SECTION | 2003 |
|
RU2253821C1 |
| METHOD OF CONFIGURING INTEGRAL DESTRUCTION ZONE OF FIRE UNITS | 2010 |
|
RU2430384C1 |
| SPACED RADIOLOCATING SYSTEM FOR DETECTION, ESCORT AND ILLUMINATION OF TARGETS | 2008 |
|
RU2374596C1 |
| SELF-PROPELLED ANTIAIRCRAFT ROCKET MOUNT FOR DETECTION, TRACKING AND LIGHTING OF TARGETS, GUIDANCE AND LAUNCHING OF ROCKETS OF MEDIUM-RANGE ROCKET COMPLEX | 2002 |
|
RU2208213C1 |
| MOBILE FIRING UNIT FOR DETECTION, TRACKING AND ILLUMINATION OF TARGETS, DIRECTION AND MISSILE LAUNCHING OF AIR DEFENSE SYSTEM OF MEDIUM RANGE | 2007 |
|
RU2333450C1 |
| SELF-PROPELLED FIRING STATION FOR DETECTION TRACKING AND LIGHTING OF TARGETS, GUIDANCE AND LAUNCHING OF MISSILES OF MEDIUM-RANGE ANTI-AIRCRAFT MISSILE COMPLEX | 2002 |
|
RU2223459C1 |
| SELF-PROPELLED TURRET OF DETECTION, TRACKING AND ILLUMINATION OF TARGETS, OF ORIENTING AND LAUNCHING MISSILES OF MEDIUM RANGE AIR DEFENCE MISSILE SYSTEM | 2012 |
|
RU2518389C1 |
| TARGET INDICATION RECEPTION AND REALIZATION EQUIPMENT | 2002 |
|
RU2236666C2 |
