Warhammer Syndicate
17-02-2004, 19:20
I will be selling surplus military supplies that are no longer in use by my nations military.
FOR SALE:
http://www.globalsecurity.org/military/world/russia/images/moskva-DNST9007636.JPG
This unit is a Moskva type Heli-carrier.
Unit Price: 25 million each.
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FOR SALE:
http://www.globalsecurity.org/military/world/russia/images/kiev-DDST8606695.JPG
This unit is a Kiev Class Heli-Carrier.
Unit Price: 35 million each.
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http://www.globalsecurity.org/military/world/russia/images/nk68bis.jpg
This unit is a Sverdlov Class Cruiser, I'm getting rid of these b/c they are just too old and out-dated to prefrom required tasks. They are a great training ship...Dirt Cheap
Unit Cost: $850,000
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Land Units:
http://www.globalsecurity.org/military/world/russia/images/t-62-11_iraq.jpg
T-62 Main Battle Tank, These are great trainers and second line battle tanks, dirt cheap.
Unit Price: 250,000 Per Vehical.
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http://www.globalsecurity.org/military/world/russia/images/bmp2_2.jpg
This is a BMP-2 APC.
Unit Price: $100,000
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http://www.globalsecurity.org/military/world/russia/images/btr60-002.jpg
BTR-60 Wheeled APC. These units are great training vechicals, easy to operate and produce.
Unit Price: $150,000
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http://www.fas.org/nuke/guide/russia/icbm/gr-1_1.jpg
GR-1 Scrag ICBM...Highest Bidder Wins!
2.2 Megaton Yeild. These are great nuclear weapons for new nations to experiment with and study. They are easy to produce and deploy, however a full background check will be preformed before this nuke is actually give to the high bidder.
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http://www.fas.org/nuke/guide/russia/icbm/ss-24-DDST8506522.jpg
RT-23 / SS-24 SCALPEL
Comparable in size and concept to the US Peacekeeper, the SS-24 is cold-launched with 10 warheads. The missile is deployed both as rail-mobile and silo-based. The silo-based SS-24 was intended to replace the SS-19 Stilletto in the Russian strategic inventory. The SS-24 rail missile systems is subject to elimination under the provisions of the START-II Treaty.
The RT-23UTTh is a solid-propellant missile with three stages within a constant diameter body. The first stage of the silo-based missile uses a rotating nozzle, whereas the railway–based version is equipped with a fixed nozzle partially inserted in the motor combustion chamber. The engines of the second and third stages deploy extendable nozzles during flight to increase the motor's specific impulse without the need to increase of the overall dimensions of the missile. During the first stage flight control is attained through deflection of the sustainer nozzle, and during the second and third stage by deflecting the combat stage and by fairing-mounted aerodynamic vanes.
Both silo-based and rail-mobile missiles have an autonomous inertial guidance system using an onboard digital computer. The silo-based system uses a two-package block of control instruments made of radiation-resistant electronic elements. The railway-based missile has only one-package block of control instruments.
A total of 10 warheads [each with a yield of 550 KT], a post-boost vehicle with a guidance/control system and a propulsion system are inside the nose cone. The guidance/control system provides a CEP of 500 meters according to unofficial Russian estimates, which gives the missile a hard-target-kill capability. The missile is deployed in a transport-launching canister from which it is launched through the mortar start technique. To conduct a railway launch the sliding roof of the car opens, the container is erected and the missile is launched with the help of a solid propellant gas generator. The missile can be launched from any point of the route.
The length of the two versions are the missile were determined by the dimensions of the silo or the railway launcher. The silo-based missile therefore has a nose cone tip flap that is activated when the launch is initiated while the railroad based missile has a folded nose cone that is extended when the launch is conducted.
The creation of the RT-23 UTTh was the culmination of a long-term effort to create a solid-propellant ICBM for multiple basing modes which was initiated on 13 January 1969.
Unit Price: 150 billion (limited supply)
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http://www.fas.org/nuke/guide/russia/icbm/rt-20p_1.jpg
RT-20P / SS-15 SCROOGE
The RT-20P missile was the first Soviet mobile ICBM, although Western sources generally viewed the SS-X-15 as a theater-range ballistic missile. Western intelligence correctly determined that the missile had a storable liquid-propellant second stage, but uncertainty remained as to whether the first stage used either a liquid or solid propellants. Western sources were also puzzled as to whether the missile was a two- or three-stage system.
The RT-20P was a two-stage missile which was unique in using dis-similar solid and liquid propellants in the first and second stages -- the first stage used solid propellant while the second stage used liquid propellants. The engine of the first stage featured four rotating nozzles to conduct flight control. The second stage had a single chambered sustainer using asymmetrical dimethylhydrazine and nitrogen tetraoxide. The flight control of the missile was attained by injecting spent turbine gas into the diverging part of the four sustainer nozzle.
With a launch weight of 30.2 tons, according to Russian sources the missile could either carry a payload of 545 kg delivering a single warhead with a yield of 550 Kt up to 11,000 km, or a payload of 1410 kg and a 1.5 Mt warhead up to 8,000 km. Western sources believed that the missile was capable of delivering a 1000-lb reentry vehicle to a range of 5,300 nm with a CEP of 1.0 to 1.5 nm.
During the development of the RT-20P three different basing modes were considered: road-mobile, railway and silo, but only the road-mobile basing mode was actually developed realized. The missile was placed in a transport-launch canister and fired from a automotive launcher created on the basis of a heavy T-YUM tank. The launch from the container was conducted using the mortar launch technique.
A new command structure substantially increased the time the missile could be maintained in an operational mode. The missile had an inertial guidance system, and the application of new high-precision gyroscopic devices allowed improved accuracy. Additionally, an improved capability for remote input of mission data implemented.
The missile was designed by KB Yuzhnoye (OKB-586) which finished the design in December 1964. On 24 August 1965 its development was officially approved. Although the missile was first displayed in the Moscow parade of November 1965, the flight test program did not begin until October 1967. Apparently the first test associated by Western intelligence with this program was detected on 12 February 1968. This test was a failure. A total of nine test launches were conducted from the Plesetsk test site. After a total of eight detected flight tests, the program apparently was abandoned following a successful flight on 07 August 1967. The development of the RT-20P missile was officially halted in October 1969, and the SS-X-15 was not deployed operationally.
Unit Price: 90 billion (limited)
------------------------------------------------------------------------------------http://www.fas.org/nuke/guide/russia/airdef/sa-1-2.jpg
SA-1 GUILD
The S-25 SA-1 GUILD was the first surface-to-air strategic air defense system deployed by the Soviet Union These R-113 missiles were deployed in a ring around Moscow, and remained in service through the mid-1980s. The SA-1 system entered operational service in the late 1950s, and was deployed around Moscow in a dense complex of 56 sites arranged in two concentric rings. There were 22 sites in the inner ring at about 25 nm radius from the center of Moscow and 34 sites on the outer ring at about 45 nm radius. A typical site had 60 launch positions joined by a road network.
The V-301 missile, as originally designed for use with this system, was unboosted and employed a single liquid sustainer motor. Although its maximum speed was on the order of Mach 2.5, it had a low initial velocity which limited its engagement capability against supersonic targets. Its maximum intercept range varied depending upon the approach and type of target; for example, against a directly incoming, high-flying B-252 its range was on the order of 20 n.m. This missile ccould carry an HE or nuclear payload of 450-700 pounds and its CEP was estimated to be 65-120 feet. It was believed to be capable of interceptions from a minimum altitude of 3,000 feet up to 60,000 feet, with some additional capability up to about 80,000 feet, particularly if equipped with a nuclear warhead.
The B-200 guidance system at each site employed a track-while-scan radar (designated "Yo-Yo" by US intelligence) having about 54° coverage in both the vertical and horizontal planes. The system also incorporated fire control equipment which enabled each site to engage as many as 20 targets simultaneously. This capability, with the spacing of adjacent sites for mutual support and the inner ring of sites for backup, enables the system to direct an extremely high rate of fire against incoming targets.
Because of its' cost, immobility, and inflexibility, the SA-1 system was not deployed elsewhere in the Soviet Union apart from Moscow.
Unit Price: 100,000 each
-------------------------------------------------------------------------------------http://www.fas.org/nuke/guide/russia/airdef/sa-2-DFST8607556.jpg
SA-2 SAM
The V-75 (SA-2) surface-to-air missile system was designed for the defense of both fixed targets and field forces. The V-75 was designed to cope with the threat posed by small groups of aircraft rather than massed raids. Flexibility and mobility are its chief advantages over the SA-1. In contrast to the massive SA-1 sites, each of which is capable of defending only a limited sector around the target area, each SA-2 site is capable of 360° coverage. This flexibility is obtained at the expense of target handling capacity and rate of fire relative to the SA-1.
Although there are a variety of arrangement patterns, all sites consist of six launching positions -- usually revetted - deployed around a guidance radar and linked by service roads to facilitate loading. While the sites were permanent installations, all operating components of the system are mounted on wheeled vehicles and are capable of movement by road or raiL
The V-75 was the basic missile defense system for critical urban-industrial areas in the USSR, other than Moscow. The V-75 deployment began on a wide scale since early 1958, with sites located throughout the western part of the Soviet Union and Warsaw Pact countries. Deployment patterns and levels of concentration varied according to the geography, size, and shape of the target area, and the Soviet estimate of the worth of individual targets. Between mid-1958 and 1964 more than 600 SA-2 sites were identified by US intelligence in the USSR, mostly in defense of population centers, industrial complexes, and government control centers.
Most SA-2 sites defended major centers of population and industry. SA-2 defenses were also deployed for the special protection of nuclear materials production and storage facilities. In addition, some key Soviet field forces and long range bomber bases were included in the SA-2 deployment pattern. The construction of sites and the training and activation of firing units was seasonal, with activity at a minimum during the winter months.
The sites in the Moscow area, located within the inner ring of SA-1 sites, were intended to supplement the existing defenses. Deployment of SA-2 installations around Moscow included seven sites as of 1964 as part of a program to supplement the SA-1 system.
Missile defenses were provided for most of the Soviet cities with populations greater than 200,000. SA-2 sites were emplaced at some smaller urban areas which contained government control centers or other installations of critical importance. They were also deployed for defense of naval and port facilities, nuclear production and weapon storage Installations, missile test ranges, and Industrial facilities. Other major military installations, such as long-range missile sites and alrfields of the long-range air force, are also defended by SA-2. A number of sites in border areas, which were unrelated to specific targets, were part of the deployment of peripheral defenses which eventually extended from the Kola Peninsula along the western and southern borders of the USSR into central Asia. Deployment in the Baltic coastal area was particularly dense. In mid-1962 about 750 sites were operational in defense of more than 200 target areas in the USSR. The Soviets eventually deployed roughly a thousand SA-2 sites in the USSR, with the major portion of the deployment completed by the mid-1960s.
Some SA-2 units were deployed in support of Soviet field forces in East Germany and in the USSR. Although SA-2 units assigned to Soviet field forces were normally emplaced at fixed installations, the system is transportable by road and SA-2 units were observed in field exercises. However, SA-2 units have a limited ability to follow a fast moving front because of the requirement for good roads and the time required to displace to new positions. SA-2 missile defenses for field forces were primarily assigned to such targets as major headquarters, logistic centers, and airfields.
Deployment of SA-2 sites for defense of Warsaw Pact targets began in 1960. The heaviest deployment has occurred in East Germany. About half of the sites were manned by East German troops, and the remainder by units of the Soviet field forces. The East German sites were located in the vicinity of Berlin and in the northern portion of East Germany. The Soviet sites were deployed to defend important Soviet military installations such as major headquarters and airfields.
Unit Price: 195,000 each
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http://www.fas.org/nuke/guide/russia/airdef/sa-3-b990503q-1.jpg
The S-125 SA-3 GOA medium altitude surface-to-air missile system uses a two-stage, solid-fuel missile built by the Isayev OKB. The S-125 missile includes a large 2.6 second burn-time solid propellant booster with rectangular fins that rotate through 90º at launch. The smaller main stage has an 18.7 second burn-time solid propellant sustainer motor, and has four aft fixed fins and four forward movable control. Following booster jettison the missile is tracked by the system's radar with guidance signals sent to an antenna on the rear fins.
US intelligence imagery at Kapustin Yar in late 1959 revealed two probable R&D sites, each of which consisted of four launch pads. A possible launcher on one of the pads held two missile-like objects about 20 feet long. US intelligence subsequntly identified more than 35 sites of this type in the USSR between late 1961 and 1964, usually near SA-1 or SA-2 sites. The initial SA-3A GOA Mod 0, deployed in 1961, includes command guidance throughout the missile's flight. The subsequent SA-3B GOA Mod 1, first deployed in 1964, incorporated an improved guidance system. The missile's ability to dive allows it to be used against surface targets and naval vessels.
Long-range surveillance and target acquisition is handled by the van-mounted P-15 FLAT FACE) radar. The P-15 radar has been replaced in many S-125 units by the P-15M SQUAT EYE radar, which has the antenna mounted on a 20-30 m mast for improved low altitude coverage. The accompanying PRV-11 SIDE NET E-band height-finding radar has a range of 180 km covering targets at altitudes of up to 32000 meters.
Unit Price: 250,000 each
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FOR SALE:
http://www.globalsecurity.org/military/world/russia/images/moskva-DNST9007636.JPG
This unit is a Moskva type Heli-carrier.
Unit Price: 25 million each.
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FOR SALE:
http://www.globalsecurity.org/military/world/russia/images/kiev-DDST8606695.JPG
This unit is a Kiev Class Heli-Carrier.
Unit Price: 35 million each.
--------------------------------------------------------------------------------------
http://www.globalsecurity.org/military/world/russia/images/nk68bis.jpg
This unit is a Sverdlov Class Cruiser, I'm getting rid of these b/c they are just too old and out-dated to prefrom required tasks. They are a great training ship...Dirt Cheap
Unit Cost: $850,000
--------------------------------------------------------------------------------------
Land Units:
http://www.globalsecurity.org/military/world/russia/images/t-62-11_iraq.jpg
T-62 Main Battle Tank, These are great trainers and second line battle tanks, dirt cheap.
Unit Price: 250,000 Per Vehical.
------------------------------------------------------------------------------------
http://www.globalsecurity.org/military/world/russia/images/bmp2_2.jpg
This is a BMP-2 APC.
Unit Price: $100,000
---------------------------------------------------------------------------------
http://www.globalsecurity.org/military/world/russia/images/btr60-002.jpg
BTR-60 Wheeled APC. These units are great training vechicals, easy to operate and produce.
Unit Price: $150,000
---------------------------------------------------------------------------------
http://www.fas.org/nuke/guide/russia/icbm/gr-1_1.jpg
GR-1 Scrag ICBM...Highest Bidder Wins!
2.2 Megaton Yeild. These are great nuclear weapons for new nations to experiment with and study. They are easy to produce and deploy, however a full background check will be preformed before this nuke is actually give to the high bidder.
---------------------------------------------------------------------------------
http://www.fas.org/nuke/guide/russia/icbm/ss-24-DDST8506522.jpg
RT-23 / SS-24 SCALPEL
Comparable in size and concept to the US Peacekeeper, the SS-24 is cold-launched with 10 warheads. The missile is deployed both as rail-mobile and silo-based. The silo-based SS-24 was intended to replace the SS-19 Stilletto in the Russian strategic inventory. The SS-24 rail missile systems is subject to elimination under the provisions of the START-II Treaty.
The RT-23UTTh is a solid-propellant missile with three stages within a constant diameter body. The first stage of the silo-based missile uses a rotating nozzle, whereas the railway–based version is equipped with a fixed nozzle partially inserted in the motor combustion chamber. The engines of the second and third stages deploy extendable nozzles during flight to increase the motor's specific impulse without the need to increase of the overall dimensions of the missile. During the first stage flight control is attained through deflection of the sustainer nozzle, and during the second and third stage by deflecting the combat stage and by fairing-mounted aerodynamic vanes.
Both silo-based and rail-mobile missiles have an autonomous inertial guidance system using an onboard digital computer. The silo-based system uses a two-package block of control instruments made of radiation-resistant electronic elements. The railway-based missile has only one-package block of control instruments.
A total of 10 warheads [each with a yield of 550 KT], a post-boost vehicle with a guidance/control system and a propulsion system are inside the nose cone. The guidance/control system provides a CEP of 500 meters according to unofficial Russian estimates, which gives the missile a hard-target-kill capability. The missile is deployed in a transport-launching canister from which it is launched through the mortar start technique. To conduct a railway launch the sliding roof of the car opens, the container is erected and the missile is launched with the help of a solid propellant gas generator. The missile can be launched from any point of the route.
The length of the two versions are the missile were determined by the dimensions of the silo or the railway launcher. The silo-based missile therefore has a nose cone tip flap that is activated when the launch is initiated while the railroad based missile has a folded nose cone that is extended when the launch is conducted.
The creation of the RT-23 UTTh was the culmination of a long-term effort to create a solid-propellant ICBM for multiple basing modes which was initiated on 13 January 1969.
Unit Price: 150 billion (limited supply)
------------------------------------------------------------------------------------
http://www.fas.org/nuke/guide/russia/icbm/rt-20p_1.jpg
RT-20P / SS-15 SCROOGE
The RT-20P missile was the first Soviet mobile ICBM, although Western sources generally viewed the SS-X-15 as a theater-range ballistic missile. Western intelligence correctly determined that the missile had a storable liquid-propellant second stage, but uncertainty remained as to whether the first stage used either a liquid or solid propellants. Western sources were also puzzled as to whether the missile was a two- or three-stage system.
The RT-20P was a two-stage missile which was unique in using dis-similar solid and liquid propellants in the first and second stages -- the first stage used solid propellant while the second stage used liquid propellants. The engine of the first stage featured four rotating nozzles to conduct flight control. The second stage had a single chambered sustainer using asymmetrical dimethylhydrazine and nitrogen tetraoxide. The flight control of the missile was attained by injecting spent turbine gas into the diverging part of the four sustainer nozzle.
With a launch weight of 30.2 tons, according to Russian sources the missile could either carry a payload of 545 kg delivering a single warhead with a yield of 550 Kt up to 11,000 km, or a payload of 1410 kg and a 1.5 Mt warhead up to 8,000 km. Western sources believed that the missile was capable of delivering a 1000-lb reentry vehicle to a range of 5,300 nm with a CEP of 1.0 to 1.5 nm.
During the development of the RT-20P three different basing modes were considered: road-mobile, railway and silo, but only the road-mobile basing mode was actually developed realized. The missile was placed in a transport-launch canister and fired from a automotive launcher created on the basis of a heavy T-YUM tank. The launch from the container was conducted using the mortar launch technique.
A new command structure substantially increased the time the missile could be maintained in an operational mode. The missile had an inertial guidance system, and the application of new high-precision gyroscopic devices allowed improved accuracy. Additionally, an improved capability for remote input of mission data implemented.
The missile was designed by KB Yuzhnoye (OKB-586) which finished the design in December 1964. On 24 August 1965 its development was officially approved. Although the missile was first displayed in the Moscow parade of November 1965, the flight test program did not begin until October 1967. Apparently the first test associated by Western intelligence with this program was detected on 12 February 1968. This test was a failure. A total of nine test launches were conducted from the Plesetsk test site. After a total of eight detected flight tests, the program apparently was abandoned following a successful flight on 07 August 1967. The development of the RT-20P missile was officially halted in October 1969, and the SS-X-15 was not deployed operationally.
Unit Price: 90 billion (limited)
------------------------------------------------------------------------------------http://www.fas.org/nuke/guide/russia/airdef/sa-1-2.jpg
SA-1 GUILD
The S-25 SA-1 GUILD was the first surface-to-air strategic air defense system deployed by the Soviet Union These R-113 missiles were deployed in a ring around Moscow, and remained in service through the mid-1980s. The SA-1 system entered operational service in the late 1950s, and was deployed around Moscow in a dense complex of 56 sites arranged in two concentric rings. There were 22 sites in the inner ring at about 25 nm radius from the center of Moscow and 34 sites on the outer ring at about 45 nm radius. A typical site had 60 launch positions joined by a road network.
The V-301 missile, as originally designed for use with this system, was unboosted and employed a single liquid sustainer motor. Although its maximum speed was on the order of Mach 2.5, it had a low initial velocity which limited its engagement capability against supersonic targets. Its maximum intercept range varied depending upon the approach and type of target; for example, against a directly incoming, high-flying B-252 its range was on the order of 20 n.m. This missile ccould carry an HE or nuclear payload of 450-700 pounds and its CEP was estimated to be 65-120 feet. It was believed to be capable of interceptions from a minimum altitude of 3,000 feet up to 60,000 feet, with some additional capability up to about 80,000 feet, particularly if equipped with a nuclear warhead.
The B-200 guidance system at each site employed a track-while-scan radar (designated "Yo-Yo" by US intelligence) having about 54° coverage in both the vertical and horizontal planes. The system also incorporated fire control equipment which enabled each site to engage as many as 20 targets simultaneously. This capability, with the spacing of adjacent sites for mutual support and the inner ring of sites for backup, enables the system to direct an extremely high rate of fire against incoming targets.
Because of its' cost, immobility, and inflexibility, the SA-1 system was not deployed elsewhere in the Soviet Union apart from Moscow.
Unit Price: 100,000 each
-------------------------------------------------------------------------------------http://www.fas.org/nuke/guide/russia/airdef/sa-2-DFST8607556.jpg
SA-2 SAM
The V-75 (SA-2) surface-to-air missile system was designed for the defense of both fixed targets and field forces. The V-75 was designed to cope with the threat posed by small groups of aircraft rather than massed raids. Flexibility and mobility are its chief advantages over the SA-1. In contrast to the massive SA-1 sites, each of which is capable of defending only a limited sector around the target area, each SA-2 site is capable of 360° coverage. This flexibility is obtained at the expense of target handling capacity and rate of fire relative to the SA-1.
Although there are a variety of arrangement patterns, all sites consist of six launching positions -- usually revetted - deployed around a guidance radar and linked by service roads to facilitate loading. While the sites were permanent installations, all operating components of the system are mounted on wheeled vehicles and are capable of movement by road or raiL
The V-75 was the basic missile defense system for critical urban-industrial areas in the USSR, other than Moscow. The V-75 deployment began on a wide scale since early 1958, with sites located throughout the western part of the Soviet Union and Warsaw Pact countries. Deployment patterns and levels of concentration varied according to the geography, size, and shape of the target area, and the Soviet estimate of the worth of individual targets. Between mid-1958 and 1964 more than 600 SA-2 sites were identified by US intelligence in the USSR, mostly in defense of population centers, industrial complexes, and government control centers.
Most SA-2 sites defended major centers of population and industry. SA-2 defenses were also deployed for the special protection of nuclear materials production and storage facilities. In addition, some key Soviet field forces and long range bomber bases were included in the SA-2 deployment pattern. The construction of sites and the training and activation of firing units was seasonal, with activity at a minimum during the winter months.
The sites in the Moscow area, located within the inner ring of SA-1 sites, were intended to supplement the existing defenses. Deployment of SA-2 installations around Moscow included seven sites as of 1964 as part of a program to supplement the SA-1 system.
Missile defenses were provided for most of the Soviet cities with populations greater than 200,000. SA-2 sites were emplaced at some smaller urban areas which contained government control centers or other installations of critical importance. They were also deployed for defense of naval and port facilities, nuclear production and weapon storage Installations, missile test ranges, and Industrial facilities. Other major military installations, such as long-range missile sites and alrfields of the long-range air force, are also defended by SA-2. A number of sites in border areas, which were unrelated to specific targets, were part of the deployment of peripheral defenses which eventually extended from the Kola Peninsula along the western and southern borders of the USSR into central Asia. Deployment in the Baltic coastal area was particularly dense. In mid-1962 about 750 sites were operational in defense of more than 200 target areas in the USSR. The Soviets eventually deployed roughly a thousand SA-2 sites in the USSR, with the major portion of the deployment completed by the mid-1960s.
Some SA-2 units were deployed in support of Soviet field forces in East Germany and in the USSR. Although SA-2 units assigned to Soviet field forces were normally emplaced at fixed installations, the system is transportable by road and SA-2 units were observed in field exercises. However, SA-2 units have a limited ability to follow a fast moving front because of the requirement for good roads and the time required to displace to new positions. SA-2 missile defenses for field forces were primarily assigned to such targets as major headquarters, logistic centers, and airfields.
Deployment of SA-2 sites for defense of Warsaw Pact targets began in 1960. The heaviest deployment has occurred in East Germany. About half of the sites were manned by East German troops, and the remainder by units of the Soviet field forces. The East German sites were located in the vicinity of Berlin and in the northern portion of East Germany. The Soviet sites were deployed to defend important Soviet military installations such as major headquarters and airfields.
Unit Price: 195,000 each
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http://www.fas.org/nuke/guide/russia/airdef/sa-3-b990503q-1.jpg
The S-125 SA-3 GOA medium altitude surface-to-air missile system uses a two-stage, solid-fuel missile built by the Isayev OKB. The S-125 missile includes a large 2.6 second burn-time solid propellant booster with rectangular fins that rotate through 90º at launch. The smaller main stage has an 18.7 second burn-time solid propellant sustainer motor, and has four aft fixed fins and four forward movable control. Following booster jettison the missile is tracked by the system's radar with guidance signals sent to an antenna on the rear fins.
US intelligence imagery at Kapustin Yar in late 1959 revealed two probable R&D sites, each of which consisted of four launch pads. A possible launcher on one of the pads held two missile-like objects about 20 feet long. US intelligence subsequntly identified more than 35 sites of this type in the USSR between late 1961 and 1964, usually near SA-1 or SA-2 sites. The initial SA-3A GOA Mod 0, deployed in 1961, includes command guidance throughout the missile's flight. The subsequent SA-3B GOA Mod 1, first deployed in 1964, incorporated an improved guidance system. The missile's ability to dive allows it to be used against surface targets and naval vessels.
Long-range surveillance and target acquisition is handled by the van-mounted P-15 FLAT FACE) radar. The P-15 radar has been replaced in many S-125 units by the P-15M SQUAT EYE radar, which has the antenna mounted on a 20-30 m mast for improved low altitude coverage. The accompanying PRV-11 SIDE NET E-band height-finding radar has a range of 180 km covering targets at altitudes of up to 32000 meters.
Unit Price: 250,000 each
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