S-300 missile system: Difference between revisions
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{{Infobox Weapon |
{{Infobox Weapon |
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|name=S-300 Family<br /><small>[[NATO reporting name]]:<br />SA-10 Grumble, SA-12 Giant/Gladiator, SA-20 Gargoyle</small> |
|name=S-300 Family<br /><small>[[NATO reporting name]]:<br />SA-10 Grumble, SA-12 Giant/Gladiator, SA-20 Gargoyle</small> |
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|image=[[File:MoscowParade2009 7.jpg| |
|image=[[File:MoscowParade2009 7.jpg|400px|thumb|center]] |
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|caption=S-300 anti-aircraft missile system at the Victory Parade, Red Square, 9 May 2009. |
|caption=S-300 anti-aircraft missile system at the Victory Parade, Red Square, 9 May 2009. |
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|origin={{flag|Soviet Union}} {{Flagu|Russia}} |
|origin={{flag|Soviet Union}} {{Flagu|Russia}} |
Revision as of 14:05, 23 February 2013
S-300 Family NATO reporting name: SA-10 Grumble, SA-12 Giant/Gladiator, SA-20 Gargoyle | |
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![]() S-300 anti-aircraft missile system at the Victory Parade, Red Square, 9 May 2009. | |
Type | long-range SAM system |
Place of origin | ![]() ![]() |
Service history | |
In service | 1978–present |
Used by | See list of operators |
Production history | |
Designer | Almaz-Antey:
|
Designed | 1967–2005[1] |
Manufacturer | MZiK[2] |
Produced | 1978–2011 |
Variants | see variants |
The S-300 (NATO reporting name SA-10 Grumble) is a series of Russian long range surface-to-air missile systems produced by NPO Almaz, all based on the initial S-300P version. The S-300 system was developed to defend against aircraft and cruise missiles for the Soviet Air Defence Forces. Subsequent variations were developed to intercept ballistic missiles.
The S-300 system was first deployed by the Soviet Union in 1979, designed for the air defense of large industrial and administrative facilities, military bases, and control of airspace against enemy strike aircraft.
The project-managing developer of the S-300 is Russian Almaz corporation (government owned, aka "KB-1") which is currently a part of "Almaz-Antei" Air Defense Concern. S-300 uses missiles developed by MKB "Fakel" design bureau (a separate government corporation, aka "OKB-2").
The S-300 is regarded as one of the most potent anti-aircraft missile systems currently fielded.[3] Its radars have the ability to simultaneously track up to 100 targets while engaging up to 12. S-300 deployment time is five minutes.[3] The S-300 missiles are sealed rounds and require no maintenance over their lifetime. An evolved version of the S-300 system is the S-400 (NATO reporting name SA-21 Growler), entering limited service in 2004.
Variations and upgrades
Numerous versions have since emerged with different missiles, improved radars, better resistance to countermeasures, longer range and better capability against short-range ballistic missiles or targets flying at very low altitude. There are currently three main variations.
S-300 system family tree
S-300 Family | |||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||
S-300V | S-300P | S-300F | |||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||
S-300V1 | S-300V2 | S-300PT | S-300PS | Fort | Rif | ||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||
S-300VM | S-300PT-1 | S-300PM | S-300PMU | Fort-M | Rif-M | ||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||
Favorit-S | |||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||
S-300VM1 | S-300VM2 | S-300PT-1A | S-300PM1 | S-300PMU1 | |||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||
Antey 2500 | S-300PM2 | S-300PMU2 | Russian Version | ||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||
Favorit | Export Version | ||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||
S-300VMD | S-400 | ||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||
S-300P
Land-based S-300P (SA-10)
The S-300P (transliterated from Russian С-300П, NATO reporting name SA-10 Grumble) is the original version of the S-300 system which became operational in 1978.[1] In 1987 over 80 of these sites were active, mainly in the area around Moscow. The P suffix stand for PVO-Strany (country air defence system). An S-300PT unit consists of a 36D6 (NATO reporting name TIN SHIELD) surveillance radar, a 30N6 (FLAP LID) fire control system and 5P85-1 launch vehicles. The 5P85-1 vehicle is a semi-trailer truck. Usually a 76N6 (CLAM SHELL) low altitude detection radar is also a part of the unit.[4]
This system broke substantial new ground, including the use of a phased array radar and multiple engagements on the same Fire-control system (FCS). Nevertheless, it had some limitations. It took over one hour to set up this semi-mobile system for firing and the hot vertical launch method employed scorched the TEL.[5]
![](http://upload.wikimedia.org/wikipedia/commons/thumb/7/7b/Dummy_S-300_vehicles.jpg/220px-Dummy_S-300_vehicles.jpg)
It was originally intended to fit the Track Via Missile (TVM) guidance system onto this model. However, the TVM system had problems tracking targets below 500 m. Rather than accept the limitation, the Soviets decided that the tracking of low altitude targets was a must and decided to use a pure command-guidance system until the TVM head was ready.[5] This allowed the minimum engagement altitude to be set at 25 m.
Improvements to the S-300P have resulted in several major subversions for both the internal and the export market. The S-300PT-1 and S-300PT-1A (SA-10b/c) are incremental upgrades of the original S300PT system. They introduce the 5V55KD missile and the cold launch method thereafter employed. Time to readiness was reduced to 30 minutes (broadly comparable to Patriot) and trajectory optimizations allowed the 5V55KD to reach a range of 75 km.[5]
![](http://upload.wikimedia.org/wikipedia/commons/thumb/3/3a/Sa-10c_b.jpg/220px-Sa-10c_b.jpg)
The S-300PS/S-300PM (Russian С-300ПC/С-300ПМ, NATO reporting name SA-10d/e) was introduced in 1985 and is the only version thought to have been fitted with a nuclear warhead. This model saw the introduction of the modern TEL and mobile radar and command-post vehicles that were all based on the MAZ-7910 8 × 8 truck.[1] This model also featured the new 5V55R missiles which increased maximum engagement range to 90 km (56 mi) and introduced a terminal semi-active radar homing (SARH) guidance mode. The surveillance radar of these systems was designated 30N6. Also introduced with this version was the distinction between self-propelled and towed TELs. The towed TEL is designated 5P85T. Mobile TELs were the 5P85S and 5P85D. The 5P85D was a "slave" TEL, being controlled by a 5P85S "master" TEL. The "master" TEL is identifiable thanks to the large equipment container behind the cabin; in the "slave" TEL this area is not enclosed and is used for cable or spare tyre storage.
The next modernisation, called the S-300PMU (Russian С-300ПМУ, US DoD designation SA-10f) was introduced in 1992 for the export market and featured the upgraded 5V55U missile which still utilised the intermediate SARH terminal guidance method and smaller warhead of the 5V55R but increased the engagement envelope to give this missile roughly the same range and altitude capabilities as the newer 48N6 missile (max. range 150 km/93 mi). The radars were also upgraded, with the surveillance radar for the S-300PMU being designated 64N6 (BIG BIRD) and the illumination and guidance radar being designated 30N6-1 in the GRAU index.[citation needed]
- S-300P Total produced: 3000 launchers, 28,000 missiles for the S-300P[6]
S-300F
Sea-based S-300F (SA-N-6)
The S-300F Fort (Russian С-300Ф Форт, DoD designation SA-N-6, F suffix for Flot, Russian for fleet) was introduced in 1984 as the original ship-based (naval) version of the S-300P system developed by Altair with the new 5V55RM missile with range extended to 7–90 km (4–56 mi, equal to 3.8–50 nautical miles) and maximum target speed up to Mach 4 while engagement altitude was reduced to 25–25,000 m (100-82,000 ft). The naval version utilises the TOP SAIL or TOP STEER, TOP PAIR and 3R41 Volna (TOP DOME) radar and utilises command guidance with a terminal semi-active radar homing (SARH) mode. Its first installation and sea trials were on a Kara class cruiser and it is also installed on Slava class cruisers and Kirov class battlecruisers. It is stored in eight (Slava) or twelve (Kirov) 8-missile rotary launchers below decks. The export version of this system is known as Rif (Russian Риф – reef). The NATO name, found also in colloquial use, is "Grumble".
Sea-based S-300FM (SA-N-20)
The S-300FM Fort-M (Russian С-300ФМ, DoD designation SA-N-20) is another naval version of the system, installed only on the Kirov class cruiser RFS Pyotr Velikiy, and introduced the new 48N6 missile. It was introduced in 1990 and increased missile speed to approximately Mach 6 for a maximum target engagement speed of up to Mach 8.5, increased the warhead size to 150 kg (330 lb) and increased the maximum engagement range yet again to 5–150 km (3–93 mi) as well as opening the altitude envelope to 10m-27 km (33–88500 ft). The new missiles also introduced the ultimate track-via-missile guidance method and brought with it the ability to intercept short-range ballistic missiles. This system makes use of the TOMB STONE MOD rather than TOP DOME radar. The export version is called the Rif-M. Two Rif-M systems were purchased by China in 2002 and installed on the Type 051C air-defence guided missile destroyers.
Both naval versions are believed to include a secondary infrared terminal seeker, similar to the newer US Standard missile system, probably to reduce the system's vulnerability to saturation. This also allows the missile to engage contacts over the radar horizon, such as warships or sea-skimming anti-ship missiles.
S-300V (SA-12)
![](http://upload.wikimedia.org/wikipedia/commons/thumb/7/7e/S-300V.jpg/220px-S-300V.jpg)
The 9K81 S-300V Antey-300 (Russian 9К81 С-300В Антей-300 – named after Antaeus, NATO reporting name SA-12 Gladiator/Giant) varies from the other designs in the series. It was built by Antey as opposed to Almaz.[7] The V suffix stands for Voyska (ground forces). It was designed to act as the top tier army air defence system, providing a defence against ballistic missiles, cruise missiles and aircraft, replacing the SA-4 'Ganef'. The "GLADIATOR" missiles have a maximum engagement range of around 75 km (47 mi) while the "GIANT" missiles can engage targets out to 100 km (62 mi) and up to altitudes of around 32 km (100,000 ft). In both cases the warhead is around 150 kg (331 lb).
While it was created from the same project (hence the common S-300 designation) different priorities resulted in a design quite different from the other versions. The S-300V system is carried on tracked MT-T transporters, which gives it better cross-country mobility than even the S-300Ps on 8 × 8 wheeled transporters. It is also somewhat more distributed than the S-300P's. For example, while both have mechanically-scanning radar for target acquisition (9S15 BILL BOARD A), the battery level 9S32 GRILL PAN has an autonomous search ability and SARH delegated to illumination radar on TELARs. The early 30N6 FLAP LID on the S-300P handles tracking and illumination, but is not equipped with an autonomous search capability (later upgraded).
![](http://upload.wikimedia.org/wikipedia/commons/thumb/e/ee/SA-12.jpg/220px-SA-12.jpg)
The S-300V places a greater emphasis on the ABM, with the dedicated 9M82 (SA-12B Giant) Anti-Ballistic missile. This missile is larger and only two can be held on each TELAR. It also has a dedicated ABM radar – the 9S19 HIGH SCREEN phased array radar at battalion level. A typical S-300V battalion is made up out of a target detection and designation unit, a guidance radar and up to 6 TELARs. The detection and designation unit consists of the 9S457-1 command post, a 9S15MV or 9S15MT BILL BOARD all-round surveillance radar and 9S19M2 HIGH SCREEN sector surveillance radar.[8] The S-300V uses the 9S32-1 GRILL PAN multi-channel guidance radar. Four types of missile-launcher vehicles can be used with the system:[9]
- Transporter erector and radar (TELAR) vehicles, which not only transport the missiles, but also fire and guide them. There are two models: the 9A83-1 TELAR holding four 9M83 GLADIATOR missiles and the 9A82 TELAR holding two 9M82 GIANT missiles.[9]
- Launcher/loader vehicles (LLV), which transport the missiles and can reload the TELARs, and also fire missiles under the control of a TELAR. There are two models: the 9A84 LLV holding two 9M83 GLADIATOR missiles and the 9A85 LLV holding two 9M82 GIANT missiles.[9]
S-300V system may be controlled by an upper level command post system 9S52 Polyana-D4 integrating it with Buk missile system into a brigade.
S-300PMU-1/2 (SA-20)[10]
![](http://upload.wikimedia.org/wikipedia/commons/thumb/3/3c/S-300PMU2_64N6E2.jpg/220px-S-300PMU2_64N6E2.jpg)
The S-300PMU-1 (Russian С-300ПМУ-1,US DoD designation SA-20A, NATO reporting name SA-20 Gargoyle) was also introduced in 1992 with the new and larger 48N6 missiles for the first time in a land-based system and introduced all the same performance improvements from the S300FM version including the increased speed, range, TVM guidance and ABM capability.[11] The warhead is slightly smaller than the naval version at 143 kg (315 lb). This version also saw the introduction of the new and more capable 30N6E TOMB STONE radar.
The S-300PMU-1 was introduced in 1999 and for the first time introduces several different kinds of missiles in a single system. In addition to the 5V55R and 48N6E missiles the S-300PMU-1 can utilise two new missiles, the 9M96E1 and 9M96E2. Both are significantly smaller than the previous missiles at 330 and 420 kg (728 and 926 lb respectively) and carry smaller 24 kg (53 lb) warhead. The 9M96E1 has an engagement range of 1–40 km (1–25 mi) and the 9M96E2 of 1–120 km (1–75 mi). They are still carried 4 per TEL. Rather than just relying on aerodynamic fins for manoeuvring, they use a gas-dynamic system which allows them to have an excellent probability of kill (Pk) despite the much smaller warhead. The Pk is estimated at 0.7 against a tactical ballistic missile for either missile. The S-300PMU-1 typically uses the 83M6E command and control system, although it is also compatible with the older Baikal-1E and Senezh-M1E CCS command and control systems. The 83M6E system incorporates the 64N6E (BIG BIRD) surveillance/detection radar. The fire control/illumination and guidance radar used is the 30N6E(1), optionally matched with a 76N6 low altitude detection radar and a 96L6E all altitude detection radar. The 83M6E command and control system can control up to 12 TELs, both the self-propelled 5P85SE vehicle and the 5P85TE towed launchers. Generally support vehicles are also included, such as the 40V6M tow vehicle, intended for lifting of the antenna post.[citation needed]
![](http://upload.wikimedia.org/wikipedia/commons/thumb/f/f5/S-300PMU2_complex.jpg/220px-S-300PMU2_complex.jpg)
The S-300PMU-2 Favorite (Russian С-300ПМУ-2 Фаворит – Favourite, DoD designation SA-20B), introduced in 1997, is an upgrade to the S-300PMU-1 with range extended once again to 195 km (121 mi) with the introduction of the 48N6E2 missile. This system is apparently capable against not just short range ballistic missiles, but now also medium range tactical ballistic missiles. It uses the 83M6E2 command and control system, consisting of the 54K6E2 command post vehicle and the 64N6E2 surveillance/detection radar. It employs the 30N6E2 fire control/illumination and guidance radar. Like the S-300PMU-1, 12 TELs can be controlled, with any mix of 5P85SE2 self-propelled and 5P85TE2 trailer launchers. Optionally it can make use of the 96L6E all altitude detection radar and 76N6 low altitude detection radar.[12]
S-400 (SA-21)
The S-400 Triumf (Russian С-400 «Триумф», formerly known as the S-300PMU-3/С-300ПМУ-3, NATO reporting name SA-21 Growler) was introduced in 1999 and features a new, much larger missile with 2 per TEL. The project has been encountering delays since its original announcement and deployment has only begun on a small scale in 2006. With an engagement range of up to 400 km (250 mi), depending on the missile variant used, and specifically designed to counter stealth it is by far the most advanced version.[citation needed] Little else is known about this version.
S-300VM (SA-X-23)
The S-300VM (Antey 2500) is an upgrade to the S-300V. It consists of a new command post vehicle, the 9S457ME and a selection of new radars. These consist of the 9S15M2, 9S15MT2E and 9S15MV2E all-round surveillance radars, and the 9S19ME sector surveillance radar. The upgraded guidance radar has the Grau index 9S32ME. The system can still employ up to six TELARs, the 9A84ME launchers (up to 4 × 9M83ME missile) and up to 6 launcher/loader vehicles assigned to each launcher (2 × 9M83ME missile each). An upgraded version, dubbed S-300V4 will be delivered to Russian army in 2011.[13]
Operators and other versions
This section needs additional citations for verification. (August 2010) |
The S-300 is mainly used in Eastern Europe and Asia although sources are inconsistent about the exact countries possessing the system.[14]
Algeria – 4 battalions of S-300PMU2 were ordered in 2006.[15]
Armenia[16] S-300PS (SA-10)
Azerbaijan bought 2 battalions of S-300PMU2 in 2009.[17]
Belarus – S-300PS systems delivered from Russia in 2007 to replace older S-300 model in Belarussian inventory.[18] Older S-300V sold to Turkey for testing and using on Anatolian Eagle exercises.[19]
Bulgaria has ten S-300 launchers, divided into two units with five launchers each.[20]
People's Republic of China: China is also the first customer of S-300PMU-2 and may be using the S-300V under the name Hongqi HQ-18.[21] China also built an upgraded version of the HQ-10 labelled the HQ-15 with the maximum range upgraded from 150 km (93 mi) to 200 km (120 mi). There are unconfirmed reports that claim this version is the Chinese manufactured S-300PMU-2.[22][23] The total number of the S-300PMU/1/2 and HQ-15/18 batteries in PLA are approximately 40 and 60 respectively, in the year 2008. The total number of the missiles is well above 1,600, with about 300 launcher platforms.[23] Five such SAM battalions are deployed and in active duty around Beijing region, six battalions in Taiwan strait region and rest battalions in other major cities like Shanghai, Chengdu and Dalian. Two Rif (SA-N-6) systems were purchased in 2002 for the Chinese Navy for the Type 051C Destroyers.
Cyprus &
Greece: Cyprus signed an agreement to buy S-300 systems in 1996. Eventually buying the S-300PMU-1 version, however due to political tension between Cyprus and Turkey and intense Turkish pressure (see Cyprus Missile Crisis), the system was instead transferred to the Greek Island of Crete. Later, Cyprus acquired Tor-M1 and Buk-M1 systems. Finally, on 19 December 2007 the missiles were officially transferred to the Greek government in return for further Tor-M1 and Buk-M1 systems.[20]
Kazakhstan[6][24]
North Korea On 10 October 2010 military parade a new SAM system, complete with Flap Lid radars, was displayed. North Korea announced it to be "an anti-ballistic defense system", capable of shooting down aircraft at distances of 90 kilometers and at altitudes of up to 30 kilometers. Japanese media reported the system to be a locally designed S-300 derivative, a fact that is corroborated by the presence of Flap Lid radars. However, this and the origin of the missiles have yet to be confirmed.[25]
Slovakia – Inherited from Czechoslovakia. Slovakian proposal to equip another battalion in mid '90 was canceled.[citation needed]
Syria announced an intention to buy the S-300P in 1991 and now seems to possess the system. During the Syrian revolution, Russia supplied the Syrian military with an array of S-300 missiles and sent Russian technical advisors with the missiles to provide the technical support for Syrian military to operate the missiles.[14][26][27] However, Russia withheld the sale in 2012.[28]
Russia: Has used all of the S-300 variations. The Russian Air Defense Forces, which are part of the Air Force, currently operates 768 S-300PMUs and 185 S-300Vs, meaning they operate 953 in total launchers.[29] All production in 1994 (actually 1990) or older, all the complexes S-300PM have been repairing and upgrading(Favorite-S).[30] S-300P/PT have been retired before 2008, some S-300PS in service, but will be retired in the near future(2012–2013), about 30 divisions is S-300V/S-300PM2, will be retired in ~2018.[31] By 2015 will be delivered over 3 S-300V4. Modernization of all S-300V to the version S-300V4 will end in 2012[32][33]
Ukraine – S-300PS, S-300PMU, S-300V and others.[34] Only six systems have been repaired since 2004; as a result only 40% of Ukrainian S-300 systems are in good condition.[35]
Venezuela ordered S-300VM "Antey-2500" to equip 12 Regiments. The missiles were delivered in May 2012.[36]
Vietnam has bought two S-300PMU-1 for nearly $300 million.[37]
Former operators
Croatia: Croatia no longer maintains an S-300 system. It was acquired from Ukraine in 1995 and was never complete and in operational state, but served the role of a psychological weapon. After much controversy, as of 2004 the system is no longer in Croatia and was presumably sold. According to some sources, including the court testimony of arms dealer Zvonko Zubak, the system was indeed shipped to the United States in 2004.[38]
Czechoslovakia – One battalion created in 1990. Passed on to Slovakia in 1993.
East Germany
Soviet Union
Possible future operators
Iran's status regarding the S-300 system remains controversial. Iran claimed to have signed a contract with Russia on 25 December 2007 on the sales of the S-300PMU-1 missile system.[39] Russian officials have denied this.[40] It has also been claimed that Croatia sold their S-300s to Iran.[41] Later, On 21 December, according to a senior Iranian lawmaker, Russia has started the supply of components for S-300 air defense systems to Iran. Esmaeil Kosari, deputy chairman of the parliamentary commission on national security and foreign policy, told the Iranian news agency IRNA that Iran and Russia had held negotiations for several years on the purchase of S-300 air defense systems and had finalized a deal. Kosari said the Islamic Republic would deploy S-300 surface-to-air missile systems to strengthen national defense on border areas.[42] On 28 October 2009, if asked when Russia would deliver the systems to Iran, Ivanov said: "There have been no such deliveries to date."[43] Yet on 23 December 2009, Russian Deputy Foreign Minister Alexei Borodavkin said Russia sees no reason to cancel a deal to provide S-300s to Iran. He said ""Exports of such weapons is subject to no UN treaty or other bilateral agreements, This is why we see no essential reason to make any change in the deal," indicating that there is a deal.[44] On 8 February 2010, Iran announced that it had a "domestically-made" system called Bavar 373 with the same capabilities as the S-300. In September 2012 Iran successfully tested Raad Air Defense System a partner for Bavar 373.[45] Alexander Fumin has said that the delay in the delivery is due to a technical problem with the radiowave system.[46] In 19 April 2010, Asr Iran (Iran's Era) website said that Iran could develop a similar air missiles system[47] On 11 June 2010 Russia has stopped sale of the S-300 air defense system to Iran in lieu of U.N. sanctions against Iran stating that the "S-300s fall under these sanctions".[48] On 4 August 2010 Iran claimed it has obtained two S-300PT (SA-10) from Belarus and two others from another unspecified source despite Russian refusal to deliver them.[49] The Belarusian government has denied rumors that Minsk had allegedly sold S-300 air defense systems to Iran. "The State Military-Industrial Committee can officially state that Belarus has never held talks with Iran on the deliveries of the S-300 air defense systems", said committee's spokesman Vladimir Lavrenyuk. "Belarus has never supplied S-300 systems or their components to Iran," he said, adding that Minsk strictly complied with international arms control regulations.[50] On 22 September 2010 Russian President Dmitry Medvedev signed a decree banning the sale of the S-300 and other military equipment to Iran.[51] The sale was canceled because of United Nations Security Council Resolution 1929 sanctions on Iran. On 10 November 2010 Iran announced that it had developed a version of the S-300 missile.[52] However Pieter Wezeman of the Stockholm International Peace Research Institute has questioned Iran's ability to duplicate the Russian missile system.[53] And by 2012 the Iranian position had softened to merely considering the production of such a system.[54] In April 2012, Iran filed a lawsuit for $4 billion in damages for failure to deliver the missiles.[55] Then Iran blamed foreign media for inflaming the situation when Russia threatened to reduce diplomatic support for Iran if the lawsuit continued.[56]
Libya: Tripoli also expressed interest in buying 10 Ka-52 Alligator assault helicopters, two advanced long range S-300PMU2 Favorit air defense missile systems, and 40 short range Pantsir-S1 air defense complexes, for a total cost over $1 billion.[57]
Serbia: During High level talks held in Belgrade on 2 December 2012, Russian delegation led by Foreign Minister and Members of Russian defense industry have proposed a Credit package to Serbian counterparts that included option of S-300PMU amongst other products.[58]
Turkey: Russia has offered the S-300VM to Turkey.[59]
Iraq : Iraq is negotioating a $4.2/5 Billion dollar deal with Russia, this deal may include the S300 PMU2.
Combat history
Although none of the S-300 versions have ever fired a missile in a real conflict, it is considered a very capable SAM system. In April 2005, NATO had a combat exercise in France and Germany called Trial Hammer 05 to practice Suppression of Enemy Air Defenses missions.[60] Participating countries were pleased that the Slovak Air Force brought a S-300PMU along, providing a unique opportunity for NATO to become familiar with the system.
Israel's purchase of F-35 Lightning II fighters was allegedly motivated in part to nullify the threat of S-300 missiles that were, at the time the fighters were initially sought, subject to a potential arms sale to Iran.[61][62]
In may 2012 a large exercise took place in Slovakia under the code name MACE XIII, where SA-300PMU was challenged by modern NATO ECM/ESM sets under complex SEAD procedures. Several NATO countries took part in this exercise, French Mirage and Raffale, danish F-16, Norway with DA-20, NATO E-3 AWACS, Turkish F-4, German Learjet with ECM/ESM set and approximately 4 others ground jammers with some partial success, with the result, that S-300PMU with professionally trained crew is capable of effective operations under complex ECM/ESM environment with high level of success.[citation needed]
Specifications
Missiles are guided by the 30N6 FLAP LID or naval 3R41 Volna (TOP DOME) radar using command guidance with terminal semi-active radar homing. Later versions use the 30N6 FLAP LID B or TOMB STONE radar to guide the missiles via command guidance/seeker-aided ground guidance (SAGG). SAGG is similar to the Patriot's TVM guidance scheme. The earlier 30N6 FLAP LID A can guide up to four missiles at a time to up to four targets, and can track up to 24 targets at once. The 30N6E FLAP LID B can guide up to two missiles per target to up to six targets simultaneously. Targets flying at up to Mach 2.5 can be successfully engaged or around Mach 8.5 for later models. One missile can be launched every three seconds. The mobile control centre is able to manage up to 12 TELs simultaneously.
The original warhead weighed 100 kg (220 lb), intermediate warheads weighed 133 kg (293 lb) and the latest warhead weighs 143 kg (315 lb). All are equipped with a proximity fuze and contact fuze. The missiles themselves weigh between 1,450 kg (3,200 lb) and 1,800 kg (3,970 lb). Missiles are catapulted clear of the launching tubes before their rocket motor fires, which can accelerate at up to 100 g (1 km/s²). They launch straight upwards and then tip over towards their target, removing the need to aim the missiles before launch. The missiles are steered with a combination of control fins and through thrust vectoring vanes. The sections below give exact specifications of the radar and missiles in the different S-300 versions. It should be noted that since the S-300PM most vehicles are interchangeable across variations.
Radar
The 30N6 FLAP LID A is mounted on a small trailer. The 64N6 BIG BIRD is mounted on a large trailer along with a generator and typically towed with the now familiar 8-wheeled truck. The 76N6 CLAM SHELL is mounted on a large trailer with a mast which is between 24 and 39 m (79 and 128 ft) tall.
The original S-300P utilises a combination of the 76N6 CLAM SHELL continuous-wave Doppler radar for target acquisition and the 30N6 FLAP LID A I/J-band phased array digitally steered tracking and engagement radar. Both are mounted on trailers. In addition there is a trailer-mounted command centre and up to twelve trailer-mounted erector/launchers with four missiles each. The S-300PS/PM is similar but uses an upgraded 30N6 tracking and engagement radar with the command post integrated and has truck-mounted TELs.
If employed in an anti-ballistic missile or anti-cruise missile role, the 64N6 BIG BIRD E/F-band radar would also be included with the battery. It is capable of detecting ballistic missile class targets up to 1,000 km (620 mi) away travelling at up to 10000 km/h (6200 mph) and cruise missile class targets up to 300 km (190 mi) away. It also employs electronic beam steering and performs a scan once every twelve seconds.
The 36D6 TIN SHIELD radar can also be used to augment the S-300 system to provide earlier target detection than the FLAP LID radar allows. It can detect a missile-sized target flying at an altitude of 60 meters (200 ft) at least 20 km (12 mi) away, at an altitude of 100 meters (330 ft) at least 30 km (19 mi) away, and at high altitude up to 175 km (109 mi) away. In addition a 64N6 BIG BIRD E/F band target acquisition radar can be used which has a maximum detection range of 300 km (190 mi).
The S-300 FC Radar Flap Lid can be mounted on a standard pylon.
GRAU index | NATO reporting name | Specialisation | Target detection range | Simultaneously detected targets | NATO frequency band | First used with | Notes |
---|---|---|---|---|---|---|---|
36D6 | TIN SHIELD | – | 180–360 km (112-224mile) | 120 | E/F | S-300P | Industrial designation: ST-68UM 350 kW to 1.23 MW signal strength |
76N6 | CLAM SHELL | Low altitude detection | I | S-300P | |||
76N6 | CLAM SHELL | Low altitude detection | 120 km (75mile) | 300 | I | S-300PMU | 1.4 kW FM continuous wave |
64N6 | BIG BIRD | – | 300 km (186mile) | C | S-300PMU-1 | ||
96L6E | CHEESE BOARD | All altitude detection | 300 km (186mile) | 300 | S-300PMU-1 | ||
9S15 | BILL BOARD | – | 250 km (155mile) | 200 | S-300V | ||
9S19 | HIGH SCREEN | Sector tracking | 16 | S-300V | |||
MR-75[63] | TOP STEER | Naval | 300 km (186mile) | D/E | S-300F | ||
MR-800 Voskhod[63] | TOP PAIR | Naval | 200 km (124mile) | C/D/E/F | S-300F |
GRAU index | NATO reporting name | NATO frequency band | Target detection range | Simultaneously tracked targets | Simultaneously engaged targets | First used with | Notes |
---|---|---|---|---|---|---|---|
30N6 | FLAP LID A | I/J | 4 | 4 | S-300P | ||
30N6E(1) | FLAP LID B | H-J | 200 km (124mile) | 12 | 6 | S-300PMU | Phased array |
30N6E2 | FLAP LID B | I/J | 200 km (124mile) | 72 | 36 | S-300PMU-2 | |
9S32-1 | GRILL PAN | Multi-band | 140–150 km (90mile) | 12 | 6 | S-300V | |
3R41 Volna | TOP DOME | I/J | 100 km (62mile) | S-300F |
Missiles
GRAU index | Year | Range | Maximum velocity | Maximum target Speed | Length | Diameter | Weight | Warhead | Guidance | First used with |
---|---|---|---|---|---|---|---|---|---|---|
5V55K/KD | 1978 | 47 km (29mile) | 1,700 m/s (3,800 mph) | 1,150 m/s (2572 mph) | 7 m (23 ft) | 450mm | 1,450 kg (3,200 lb) | 100 kg (220 lb) | Command | |
5V55R/RM | 1984 | 90 km (56mile) | 1,700 m/s (3,800 mph) | 1,150 m/s (2572 mph) | 7 m (23 ft) | 450mm | 1,450 kg (3,200 lb) | 133 kg (293 lb) | SARH | |
5V55U | 1992 | 150 km (93mile) | 2,000 m/s (4,470 mph) | 7 m (23 ft) | 450mm | 1,470 kg (3,240 lb) | 133 kg (293 lb) | SARH | ||
48N6/E | 1992 | 150 km (93mile) | 2,000 m/s (4,470 mph) | 2,800 m/s (6,415 mph) | 7.5 m (25 ft) | 500mm | 1,780 kg (3,920 lb) | ~150 kg (~330 lb) | TVM | |
48N6E2 | 1992 | 195 km (121mile) | 2,000 m/s (4,470 mph) | 2,800 m/s (6,415 mph) | 7.5 m (25 ft) | 500mm | 1,800 kg (3,970 lb) | 150 kg (330 lb) | TVM | |
9M82 | 1984 | 13–100 km (8.1–62.1 mi) 30 km (98,000 ft) alt |
2,400 m/s (5,400 mph) | 420 kg (926 lb) | 150 kg (330 lb) | SARH by TELAR | S-300V | |||
9M83 | 1984 | 6–75 km (3.7–46.6 mi) 25 km (82,000 ft) alt |
1,700 m/s (3,800 mph) | 150 kg (330 lb) | SARH by TELAR | S-300V | ||||
9M83ME | 1990 | 200 km (120mile) | SARH by TELAR | S-300VM | ||||||
9M96E1 | 1999 | 40 km (25mile) | 900 m/s[64] (2,010 mph) | 4,800–5,000 m/s (10,737–11,185 mph) |
330 kg (728 lb) | 24 kg (53 lb) | Active Radar Homing | S-400 | ||
9M96E2 | 1999 | 120 km (75mile) | 1,000 m/s[64] (2,240 mph) | 4,800–5,000 m/s (10,737–11,185 mph) |
420 kg (926 lb) | 24 kg (53 lb) | Active Radar Homing | S-400 | ||
40N6[64] | 2000 | 400 km (250mile) | Active Radar Homing | S-400 |
Comparable SAMs
References
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- ^ a b c S-300V, SA-12A GLADIATOR and SA-12B GIANT, HQ-18
- ^ 5P85SE Launcher unit S-300PMU2 Favorit Gargoyle
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- ^ ваше имя. "Политика. Казахстан получит бесплатно до десяти комплексов С-300". Vesti.kz. Retrieved 13 August 2012.
- ^ North Korea demonstrating advanced missiles at military parade (in Japanese), 12.10.2010
- ^ Russia Sent Syria Super-Advanced S-300 Missiles, Russia Sent Syria Super-Advanced S-300 Missiles.
- ^ "MissileThreat – "S-300P (SA-10 Grumble)"". Retrieved 5 September 2008.
- ^ Russian media reports: S-300 sale to Syria cancelled, Jerusalem Post 27 June 2012
- ^ Eugene Yanko, Copyright 1997 – warfare.ru (10 August 1995). "SA-20 GARGOYLE / S300PMU/2/3 | Russian Arms, Military Technology, Analysis of Russia's Military Forces". Warfare.ru. Retrieved 23 September 2010.
{{cite web}}
: CS1 maint: numeric names: authors list (link) - ^ "Новости NEWSru.com :: Россия прекращает выпуск ракетных комплексов С-300 и готовится участвовать в евроПРО с новейшими С-500". Newsru.com. Retrieved 13 August 2012.
- ^ "Прекращение производства ЗРС С-300 касается систем С-300ПС и С-300ПМ - ВПК.name". Vpk.name. Retrieved 13 August 2012.
- ^ "Модернизация до уровня ЗРС С-300В4 ПВО сухопутных войск полностью завершится в 2012 году — ОРУЖИЕ РОССИИ, Информационное агентство". Arms-expo.ru. Retrieved 13 August 2012.
- ^ "Минобороны РФ подписало трехлетний контракт на поставку ЗРС С-300В4 – Военный Обозреватель". Warsonline.info. Retrieved 13 August 2012.
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- ^
Gyürösi, Miroslav (11 March 2005). "Exclusive – NATO Aircraft Will 'Hunt' Russian Missile Systems During Defence-suppression Exercise". Jane's Information Group. The Internet Archive Wayback Machine. ISSN 1365-4187. Archived from the original on 10 June 2007. Retrieved 9 December 2010.
...the participants of Trial Hammer '05, particularly France, Germany, the UK and the US, were keen to have the Slovak Air Force S-300PMU system take part in the exercise...
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- ^ a b Not a GRAU index. GRAU indices only apply to land-based versions.
- ^ a b c German: http://www.dtig.org/docs/sa-21.pdf
External links
![](http://upload.wikimedia.org/wikipedia/en/thumb/4/4a/Commons-logo.svg/30px-Commons-logo.svg.png)
- http://www.almaz-antey.ru/ in Russian
- http://www.ausairpower.net/TE-Asia-Sams-Pt1.pdf and http://www.ausairpower.net/TE-Asia-Sams-Pt2.pdf, a two-part piece from Australian Air Power.
- www.dtig.org detailed overview of the S-300P & S-300V family.
- Almaz S-300 – China's "Offensive" Air Defense
- Soviet/Russian Missile Designations
- S-300PMU2 Favorit EnemyForces.com
- Almaz S-300P/PT/PS/PMU/PMU-1/PMU-2
- 76N6 Clam Shell Acquisition Radar
- Antey 9K81 S-300V – SA-12A/B Gladiator/Giant