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Long Range SAM System For PAF To Counter Indian MRCA+PAK-FA

Super Falcon

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I think best way to counter indian acusations of fighter jets every day growing with tejas pakfa and mrca and after that they will buy other 100+ fighter jet to take all jaguars out of IAF we all are talking what fighter jet paf buys to counter it buying fighter jet is a big headache to a country like pakistan and maintaning it is a big ask for pakistani think PAF should not waste its money after getting J 10B and than go for lattest SAM system which is on offer to PAF i know we are getting SPADA 2000 but it is medium range if we need to vounter IAF we need long range sam system of high quality and may be other one to if we have to defend pakistan from sea two sam system will do better low cost it will hit its targets 100 percent sure and twice the speed of fighter jet what paf needs more but with it paf has to look for state of the art jamming system to jam the radars of fighter jets of IAF who want to destroy pakistan's SAM system batteries with anti radiation misssiles and harpy drone and our fighter jets should be in border of pakistan and india looking for air threats if they cant bring them down than sam system will make them grounded so i bellieve that S-300 copy from china is going to be priority for PAF but other sam system has to be from europe of high quality what it should be S-400 willl be out of reach of PAF
 
The THAAD (theatre high-altitude area defence) missile system is an easily transportable defensive weapon system to protect against hostile incoming threats such as tactical and theatre ballistic missiles at ranges of 200km and at altitudes up to 150km.

The THAAD system provides the upper tier of a 'layered defensive shield' to protect high value strategic or tactical sites such as airfields or populations centres. The THAAD missile intercepts exo-atmospheric and endo-atmospheric threats.

The sites would also be protected with lower and medium-tier defensive shield systems such as the Patriot PAC-3 which intercepts hostile incoming missiles at 20 to 100 times lower altitudes.

THAAD programme
The US Army is expected to acquire 80 to 99 THAAD launchers, 18 ground-based radars and a total of 1,422 THAAD missiles. Two THAAD battalions are planned, each with four batteries.

"The target object data and the predicted intercept point are downloaded to the missile prior to launch."In 1992 Lockheed Martin Missiles and Space and other industrial team partners were awarded a $689m contract to develop the THAAD system. Raytheon was selected as sub-contractor to develop the ground-based radar.

Raytheon is responsible for the solid-state receiver / transmitter modules. TRW is responsible for software development. The other main contractors are Raytheon for the traveling wave tubes, Datatape for the data recorders and EBCO for radar turrets.

The THAAD programme entered the engineering and manufacturing development (EMD) phase in 2000. In May 2004, production of 16 flight test missiles began at Lockheed Martin's new production facilities in Pike County, Alabama.

Flight testing, at White Sands Missile Range, New Mexico, of the EMD system began in 2005. The first flight test of the entire system including missile, launcher, radar and fire control system took place in May 2006. Flight testing began at Pacific Missile Range, Kauai, Hawaii in January 2007 with a successful intercept test in the high endo-atmosphere.

A second successful test took place in April 2007 with intercept in the mid endo-atmosphere. The final White Sands test took place in June 2007, with a low endo-atmosphere test. In October 2007, THAAD performed a successful intercept of a unitary target outside the atmosphere (exo-atmospheric). In June 2008, THAAD successfully intercepted a separating target in mid-endo-atmosphere. Tests will continue at PMR till 2009.

In January 2007, Lockheed Martin was awarded a contract for the first two production THAAD systems, to include six launchers, 48 missiles, two radars and two tactical operations centers. Initial operating capability (IOC) is expected in 2009.

In May 2008, the US Army activated the first THAAD battery unit at Fort Bliss, Texas, which will receive 24 missiles, three launchers, one fire control and one radar unit for initial fielding. This is in preparation for full system fielding in 2009.

In August 2007, Lockheed Martin announced that THAAD launcher, fire control and communications units will be built at its Camden, Arkansas facility. The THAAD interceptor is built at its Pike County facility in Troy, Alabama.

In September 2008, the United Arab Emirates requested the sale of three THAAD fire units, 147 missiles, four THAAD radars, six fire control stations and nine launchers.

Battery
The THAAD battery will typically operate nine launch vehicles each carrying eight missiles, with two mobile tactical operations centres (TOCs) and a ground-based radar (GBR).

THAAD missile information
The target object data and the predicted intercept point are downloaded to the missile prior to launch. The updated target and intercept data are also transmitted to the missile in flight.

The missile is 6.17m in length and is equipped with a single stage solid fuel rocket motor with thrust vectoring. The rocket motor is supplied by Pratt & Whitney Rocketdyne. The launch weight is 900kg.

"The THAAD (theatre high-altitude area defence) missile system is an easily transportable defensive weapon."A separation motor is installed at the interstage at the forward end of the booster section. The separation motor assists in the separation of the kinetic kill vehicle (KKV) and the spent boost motor.

The shroud separates from the KV before impact. The KV is equipped with a liquid-fuelled divert and attitude control system (DACS), developed by Pratt & Whitney Rocketdyne, for the terminal maneuvering towards the target intercept point.

A gimbal-mounted infrared seeker module in the nose section provides terminal homing to close in on the target missile in the terminal phase of approach.

During the initial fly-out phase of flight, the seeker window is covered with a two-piece clamshell protection shroud. Metal bladders installed in the shroud are inflated to eject the protective shroud before the seeker initiates target acquisition. The infrared seeker head, developed by BAe Systems, is an indium antimonide (InSb) staring focal plane array operating in the mid infrared 3 to 5 micron wavelength band.

M1075 truck-mounted launcher
There are nine M1075 truck mounted launchers in a typical THAAD battery. Launch vehicle is a modified Oshkosh Truck Corporation heavy expanded mobility tactical truck with load-handling system (HEMTT-LHS). The 12m-long by 3.25m-wide launch vehicle carries ten missile launch containers. While on the launcher, lead acid batteries provide the primary power. The batteries are recharged with a low-noise generator.

After firing, reloading the launch vehicle takes 30 minutes.

Ground-based radar
The cueing for the THAAD system is provided by the Raytheon Systems AN/TPY-2 ground-based radar (GBR) for surveillance, threat classification and threat identification. THAAD can also be cued by military surveillance satellites such as Brilliant Eyes.

The ground based radar units are C-130 air transportable. The AN/TPY-2 radar uses a 9.2m² aperture full field of view antenna phased array operating at I and J bands (X band) and containing 25,344 solid-state microwave transmit and receive modules. The radar has the capability to acquire missile threats at ranges up to 1,000km.

The first production radar is being tested at the White Sands Missile Range in New Mexico. In September 2004, the THAAD radar tracked a tactical ballistic missile, cueing a successful intercept by a Patriot PAC-3 missile. A second radar was delivered to White Sands in June 2007.

Tactical operations centre

Each THAAD battery has two tactical operations centres (TOC). The TOC has been developed by Northrop Grumman, formerly Litton Data Systems Division. The TOC accommodates two operator stations and is equipped with three Hewlett-Packard HP-735 data processors.

"The THAAD missile uses kinetic energy, hit-to-kill technology."Mobile BMC3I units
The THAAD system is able to 'hand over' targets to other defence systems and can cue the targets to other weapons. THAAD is able to interface to other US or allied air defence data information networks and to the battle management and command control and communications centre.

Northrop Grumman has been contracted to develop the THAAD BMC3I. The battle management and command, control, computers and intelligence (BMC3I) units are installed in hardened shelters mounted on high-mobility multi-wheeled vehicles (HMMWVs).

The THAAD communications system can use JTIDS, mobile subscriber equipment, SINCGARS and the joint tactical terminal for voice and data communications and for intelligence data transfer.


THAAD is my personal favourite but it comes from USA it will be 50 50 to get it but the probleum is we are not sure of USA
 
Seriously our think tanks need to rework their war doctrine.

These Aircraft deals are getting expensive day by day.We need missiles instead of Jets.SAM's for Air defense and Cruise,Ballistic Missiles for Offense.

But then Again nothing can replace an Aircraft.
 
all option works, if have money. Money talks. But need huge budget for R&D, that would help future.
 
Surface to Air Missile (SAM) or ground-to-air missile (GTAM) is a missile designed to be launched from the ground to destroy aircraft. Development of surface-to-air missiles began in Nazi Germany (hard pressed by Allied air superiority) during late World War II with missiles like the Wasserfall. It is one part of the anti-aircraft system. Surface to air missiles are classified by their guidance, mobility, altitude and range


but sir it is better to buy SAM system to counter IAF and cheapest way if we buy more fighter jet it will cost twice the price of SAM system
 
Targets for non-ManPAD SAMs will usually be acquired by air-search radar, then tracked before/while a SAM is "locked-on" and then fired. Potential targets, if they are military aircraft, will be identified as friend or foe before being engaged.
 
modern BUK M1 (NATO: SA-11 Gadfly) anti-aircraft missile system
 
The Buk missile system (Russian: "Бук"; English: beech) is a family of self-propelled, medium-range surface-to-air missile systems developed by the former Soviet Union and Russian Federation and designed to engage cruise missiles, smart bombs, fixed- and rotary-wing aircraft, and unmanned aerial vehicles [2].

The Buk missile system is the successor to the NIIP/Vympel 2K12 Kub (NATO reporting name SA-6 "Gainful")[3]. The first version of Buk adopted into service carried the GRAU designation 9K37 and was identified in the west with the NATO reporting name "Gadfly" as well as the US Department of Defense designation SA-11. Since its initial introduction into service the Buk missile system has been continually upgraded and refined with the latest incarnation carrying the designation 9K37M2 "Buk-M2"[4].

Contents [hide]
1 Development
2 Description
2.1 3S-90 "Uragan"
2.2 Missiles
2.2.1 9М38 and 9М38M1 missile
2.2.2 9M317 missile
2.2.3 9M317M and 9M317A missile projects
2.3 Other variants
3 Structure
3.1 9K37 Buk (Beech)
3.2 2K12M4 Kub-M4 (9K37-1 Buk-1)
3.3 9K37M1 Buk-M1 (Ganges)
3.3.1 Technical service division
3.4 9K37M1-2 Buk-M1-2 (Ural)
3.4.1 Technical service division
3.5 9K37M2/9K317 Buk-M2
4 Service
4.1 Operators
4.2 Combat service
5 References
6 Sources
6.1 Russian sources
6.1.1 Vestnik PVO
6.2 Video


[edit] Development
Development of the 9K37 "Buk" was started on the January 17, 1972 at the request of the Central Committee of the CPSU[5]. The development team comprised many of the same institutions that had been responsible for the development of the previous 2K12 "Kub" (NATO reporting name "Gainful", SA-6). These included the Tikhomirov Scientific Research Institute of Instrument Design (NIIP) as the lead designer and the Novator design bureau who were responsible for the development of the missile armament[5]. In addition to the land based missile system a similar system was to be produced for the naval forces, the result being the 3S-90 "Uragan" (Russian: "Ураган"; English: hurricane) which also carries the SA-N-7 and "Gadfly" designations[6].

Kub



Kub-M1 Kub-M



Kub-M3



Kub-M4



Buk



Buk-M1 Buk-1



Buk-M2 Buk-M1-1[citation needed] Buk-1M



Buk-M1-2 Buk-M2E

Russian Version

Buk-M1-2A Buk-M3 Export Version


The Buk missile system was designed to surpass the 2K12 Kub in all parameters and its designers including its chief designer Ardalion Rastov visited Egypt in 1971 to see Kub in operation[7]. Both the Kub and Buk used self-propelled launchers developed by Ardalion Rastov. As a result of this visit the developers came to the conclusion that each Buk transporter erector launcher (TEL) should have its own fire control radar rather than being reliant on one central radar for the whole system as in Kub[7]. The result of this move from TEL to transporter erector launcher and radar (TELAR) was a system able to engage multiple targets from multiple directions at the same time.

During development in 1974 it was identified that although the Buk missile system is the successor to the Kub missile system both systems could share some interoperability, the result of this decision was the 9K37-1 Buk-1 system[5]. The advantage of interoperability between Buk TELAR and Kub TEL was an increase in the number of fire control channels and available missiles for each system as well as a faster service entry for Buk system components. The Buk-1 was adopted into service in 1978 following completion of state trails while the complete Buk missile system was accepted into service in 1980[7] after state trails took place between 1977 and 1979[5].

External images
Photo of one of the Buk prototype, based on Kub components
Photo of one of the Buk prototype, based on Kub components (sideview)
The naval variant of the 9K37 "Buk", the 3S-90 "Uragan" was developed by the Altair design bureau under the direction of chief designer G.N. Volgin[8]. The 3S-90 used the same 9M38 missile as the 9K37 though the launcher and associated guidance radars were exchanged for naval variants. The system was tested between 1974-1976 using a project 61 large anti-submarine ship, 3S-90 being accepted into service in 1983 equipping the project 956 "sovremmeny" class of destroyers[8].

No sooner than the 9K37 "Buk" had started to enter service than the next phase of its development was put into operation, in 1979 the Central Committee of the CPSU authorised the development of a modernised 9K37 which would become the 9K37M1 Buk-M1, adopted into service in 1983[5]. The modernisation improved the performance of the systems radars, kill probability and resistance to electronic countermeasures (ECM). Additionally a non-cooperative threat classification system was installed, allowing targets to be classified without IFF via analysis of return radar signals[7]. The export version of Buk-M1 missile system is known as "Gang" (Russian: "Ганг"; English: Ganges)[citation needed].


A Buk-M1-2 SAM system 9A310M1-2 TELAR at 2005 MAKS AirshowAnother modification to the Buk missile system was started in 1992 with work carried out between 1994 and 1997 to produce the 9K37M1-2 Buk-M1-2[5], which was accepted into service in in 1998[9]. This modification introduced a new missile, the 9M317 which offered improved kinematic performance over the previous 9M38 which could still be used by the Buk-M1-2. Such sharing of the missile type caused a transition to a different GRAU designations - 9K317 which has been used independently for all later systems. The previous 9K37 series name was also preserved for the complex as was the "Buk" name. The new missile as well as a variety of other improvements allowed the system to intercept ballistic missiles and surface targets as well as offering improved performance and engagement envelope against more traditional targets like aircraft and helicopters[5]. The 9K37M1-2 Buk-M1-2 also received a new NATO reporting name distinguishing it from previous generations of the Buk system, this new reporting name was the SA-17 Grizzly. The export version of the 9K37M1-2 system is called "Ural" (Russian: "Ганг"; English: Ganges)


Shtil-1 SA missile systemThe introduction of the 9K37M1-2 system for the land forces also marked the introduction of a new naval variant, the 9K37 "Ezh" which carries the NATO reporting name SA-N-12 "Grizzly"[6] and was exported under the name "Shtil-1". The 9K37 incorporates the 9M317 missile to replace the 9M38 used by the previous system. A further advancement of the system was unveiled as a concept at EURONAVAL 2004, a vertical launch variant of the 9M317, the 9M317M[8].

The Buk-M1-2 modernisation was based on a previous far more advanced developmental system referred to as the 9K37M2 Buk-M2[5]. This modernisation not only featured new missiles but also included a new third generation phased array fire control radar allowing engagement of up to four targets while tracking a further 24. A new radar system was also developed which carried a fire control radar on a 24 meter extending boom, improving performance against targets flying at low altitude[10]. This new generation of Buk missile systems was stalled due to the poor economic conditions after the fall of the Soviet Union, however the system was recently presented as a static display at 2007 MAKS Airshow. The export version of the Buk-M2 missile system Buk-M2E is also known as Ural (Russian: Урал; English: Ural)[citation needed].

In October 2007, Russian General Nikolaï Frolov, commander of the Ground Forces' air defense, declared that the Russian Army would receive the brand new Buk-M3 to replace the Buk-M1. He stipulated that the M3 would feature advanced electronic components and enter in service in 2009.[11]

[edit] Description
A standard Buk battalion consists of a command vehicle, target acquisition radar (TAR), six transporter erector launcher and radar (TELAR) and three transporter erector launcher reloads. A Buk missile battery consists of two TELAR and TEL vehicle. The battery requires 5 minutes to set up before it is ready for engagement and can be ready for transit again in 5 minutes. The reaction time of the battery from target tracking to missile launch is around 22 seconds[citation needed].

The Buk-M1-2 TELAR uses the GM-569 chassis designed and produced by JSC Metrowagonmash (former MMZ)[12] onto which is mounted a turret containing the fire control radar of the TELAR at the front and a launcher with four ready to fire missiles on top. Each TELAR is operated by a crew of 3 and is equipped with NBC protection. The radar fitted to each TELAR is referred to as the 'Fire Dome' by NATO, it is a monopulse type radar and can begin tracking at the missile's maximum range (32 km/20 mi) and can track aircraft flying at between 15,000 and 22,000 m (50,000 to 72,000 ft) altitudes. It can guide up to three missiles against a single target. The 9K37 system supposedly has much better ECCM characteristics (i.e. is more resistant to ECM/jamming) than the 3M9 Kub system that it replaces. An optical tracking system with laser rangefinder can be fitted for passive tracking of the target. The 9K37 system can also utilise the same 1S91 Straight Flush 25 kW G/H band continuous wave radar as the 3M9 Kub system.


A Buk-M1-2 SAM system 9S18M1-1 Tube Arm target acquisition radar (TAR) on 2005 MAKS AirshowThe 9K37 utilises the 9S18 "Tube Arm" or 9S18M1 (which carries the NATO reporting name "Snow Drift") (Russian: СОЦ 9C18 "Купол"; English: dome) target acquisition radar in combination with the 9S35 or 9S35M1 "Fire Dome" H/I band tracking and engagement radar which is mounted on each TELAR. The Snow Drift target acquisition radar has a maximum detection range of 85 km (53 miles) and can detect an aircraft flying at 100 m (330 ft) from 35 km (22 mi) away and even lower flying targets at ranges of around 10–20 km (6-12 mi). Snow Drift is mounted on a chassis similar to that of the TELAR, as is the command vehicle. The control post which coordinates communications between the surveillance radar(s) and the launchers is able to communicate with up to six TELs at once.

The TEL reload vehicle for the Buk battery resembles the TELAR but instead of a radar they have a crane for loading missiles. They are capable of launching missiles directly but require the cooperation of a Fire Dome-equipped TELAR for missile guidance. A reload vehicle can transfer its missiles to a TELAR in around 13 minutes and can reload itself from stores in around 15 minutes.

[edit] 3S-90 "Uragan"
The 3S-90 "Uragan" (Russian: Ураган; English: hurricane) is the naval variant of the 9K37 "Buk" and has the NATO reporting name "Gadfly" and US DoD designation SA-N-7, it also carries the designation M-22. The export version of this system is known as "Shtil" (Russian: Штиль; English: still). The 9М38 missiles from the 9K37 "Buk" are also used on the 3S-90 "Uragan". The launch system is different with missiles being loaded vertically onto a single arm trainable launcher, this launcher is replenished from an under-deck magazine with a 24 round capacity, loading takes 12 seconds to accomplish[8]. The Uragan utilises the MR-750 Top Steer D/E band as a target acquisition radar (naval analogue of the 9S18 or 9S18M1) which has a maximum detection range of 300 km (186 miles) depending an the variant. The radar performing the role of the 9S35 the 3R90 Front Dome H/I band tracking and engagement radar with a maximum range of 30 km (19 mi).

The modernised version the 3S-90 the 9K37 "Ezh" which carries the NATO reporting name "Grizzly" or SA-N-12 and the export designation "Shtil-1" was developed which uses the new 9M317 missile. This variant was supposed to be installed on Soviet Ulyanovsk-class nuclear aircraft carriers, and has been retrofitted to the Sovremenny class destroyers.[citation needed] The latest variant of the system uses a vertical launch missile the 9M317M which is fired from under-deck silos clustered into groups of twelve.

[edit] Missiles
9М38

Comparison of 9M38M1 and 9M317 surface-to-air missiles of the Buk missile system
Type Surface-to-air missile
Place of origin Soviet Union
Production history
Variants 9М38, 9М38M1, 9M317
Specifications (9М38, 9M317)
Weight 690 kg, 715 kg
Length 5.55 m
Diameter 0.4 m (wingspan 0.86 m)

--------------------------------------------------------------------------------

Warhead Frag-HE
Warhead weight 70 kg
Detonation
mechanism Radar proximity fuse

--------------------------------------------------------------------------------

Propellant solid propellant rocket
Operational
range 30 kilometres (19 mi)
Flight altitude 14,000 metres (46,000 ft)
Speed Mach 3
Guidance
system Semi-active radar homing
Launch
platform see structure
[edit] 9М38 and 9М38M1 missile
The 9M38 uses a single stage X-winged design without any detachable parts, its exterior design is similar to the American Tartar and Standard surface-to-air missile series. The design had to conform to strict naval dimension limitations, allowing the missile to be adapted for the M-22 SAM system in the Soviet Navy. Each missile is 5.55 m (18 feet) long, weighs 690 kg (1521 lb) and carries a relatively large 70 kg (154 lb) warhead which is triggered by a radar proximity fuze. In the forward compartment of the missile a semi-active homing radar head, autopilot equipment, power source and a warhead is located. The homing method chosen was proportional navigation. Some elements of the missile were compatible with the Kub's 3M9, for example it's forward compartment diameter (33 cm), which was lesser than the backward compartment diameter.


9M317 surface-to-air missile the Buk-M2 quadruple launcher.
9M317ME SA missile of Shtil-1The 9M38 surface-to-air missile utilizes a two-mode solid fuel rocket engine with total burn time of about 15 seconds, the combustion chamber is reinforced by metal. For the purpose of reducing the centering dispersion while in flight the combustion chamber is located close to the center of the missile and includes a longer gas pipe. Rejection of a direct-flow engine type was explained by its instability on a large angle of attack and by a larger air resistance on a passive trajectory section as well as by some technical difficulties[citation needed]. Those difficulties already wrecked the plans to create the missile for Kub[citation needed]. The design of 9M38 ensures its readiness without inspection for at least 10 years of service and is delivered to the army in the 9Ya266 (9Я266) transport container.

It has been suggested that the Novator KS-172 AAM-L, an extremely-long range air-to-air missile and possible anti-satellite weapon, is a derivative of the 9M38.[citation needed]

[edit] 9M317 missile
9M317 missile was developed as a common missile for the Ground Forces PVO (Buk-M1-2) as well as for ship-based PVO of the Russian Navy (Ezh)

The unified multi-functional missile 9M317 (export designation 9M317E) can be used to engage modern and perspective aerodynamic, ballistic, above-water and radiocontrast targets with the air defence complexes of land and naval forces. It was designed by OJSC Dolgoprudny Scientific Production Plant (DNPP) and passed the full cycle of ground and flight testing on different complexes and weapon systems. Testing included targets analogues of tactical ballistic missiles, strategic cruise missiles, anti-ship missiles, tactical, strategic and army aircraft and helicopters. The maximum engagable target speed was 1200 m/s, the missile could tolerate an acceleration overload of 24G. Missile was first used with Buk-M1-2 system of the land forces and the Shtil-1 system of the naval forces.

It may engage the tactical ballistic missiles, strategic and tactical aircraft manoeuvring up to 12G, cruise missiles, fire support helicopters (including hovering low above the ground), remotely-controlled aircraft, anti-ship missiles in a heavy anti-radiation environment and radiocontrast targets above water and above the ground.

In comparison with 9M38M1, the 9M317 missile has a larger defeat area, which is up to 45 km of range and 25 km of altitude and of lateral parameter, and a larger target classification. On the outer view 9M317 differs from 9M38M1 by a smaller wing chord. It uses the inertial correction control system with semi-active radar homing, utilizing the proportional navigation (PN) targeting method.

[edit] 9M317M and 9M317A missile projects
Currently, several modernized versions are in development, including the 9M317M, it's export version the 9M317ME and the active radar homing (ARH) missile project 9M317A with its export version the 9M317MAE. They were scheduled for completion in two years since May 2007.[13] The lead developer, NIIP also reported about the 9M317A missile testing within Buk-M1-2A "OKR Vskhod" (Sprout in English) program in 2005.[14] Range is reported as being up to 50 km (31 miles), maximum altitude around 25 km (82,000ft) and maximum target speed around Mach 4. The weight of the missiles has increased slightly to 720 kg (1587 lb).

Missile
(GRAU designation) 3M9 9М38 9М38
9М38M1 9М38
9М38M1 9М38
9М38M1
9M317 9M317
Complex
(GRAU and NATO designation) 2K12 "Kub"
(SA-6) 9K37
"Buk"
(SA-11) 9K37M
"Buk-M1"
(SA-11) 9K37M1
"Buk-SAR"[citation needed]
(SA-11) 9K37M1-2
"Buk-M1-2"
(SA-17) 9K37M2E
"Buk-M2E" [15]
(SA-17)
Introduced 1966 1980 1984 1995 1998 2008?
Missiles per TEL 3 4 4 4 4 4
Missile Weight 599 kg
(1321 lb) 690 kg
(1521 lb) 690 kg
(1521 lb) 690 kg
(1521 lb) 9М38M1: - 690 kg
(1521 lb);
9M317: - 3710-720 kg
(1565-1587 lb) 710-720 kg
(1565-1587 lb)
Engagement range 3–24 km
(2–15 miles) 4–30 km
(3–19 miles) 3–35 km
(2–22 miles) 3–42 km
(2–26 miles) 9М38M1: - 3–42 km
(2–26 miles);
9M317: 3–50 km
(2–31 miles) 3–50 km
(2–31 miles)
Engagement altitude 800-11000 m
(2,600-36,000 ft) 30-14000 m
(100-46,000 ft) 30-22000 m
(100-72,000 ft) 30-25000 m
(100-82,000 ft) 30-25000 m
(100-82,000 ft) 30-25000 m
(100-82,000 ft)
Missile speed
(Mach) 2.8 3 3 3 3 3
Maximum target
speed (Mach) 2 2.5 4 4 4 4
Simultaneous
engagements 1 2 6 6 6[16] 6[16]

[edit] Other variants
9K37-1 'Buk-1' - First Buk missile system variant accepted into service, incorporating a 9A38 TELAR within a 2K12M3 Kub-M3 battery.
9K37 'Buk'- The completed Buk missile system with all new system components, back-compatible with Kub.
9K37M1 'Buk-M1' - An improved variant of the original 9K37 which entered into service with the then Soviet armed forces.
9K37M1-2 'Buk-M1-2' - An improved variant of the 9K37M1 'Buk-M1' which entered into service with the Russian armed forces.
In May on the MILEX-2005 exposition in Minsk, Belarus presented their own modification of 9K37 Buk called Buk-MB.[17]
9K37M2/9K317 'Buk-M2'[4]

Backside of the 9A317 TELAR of Buk-M2E (export version) at 2007 MAKS Airshow
9A317 TELAR of Buk-M2E (export version) at 2007 MAKS Airshow9K37M3/9K317M Buk-M3 - In Russian some active work is being conducted, aimed at the new perspective complex of Buk-M3. A zenith-rocket division of it will have 36 target channels in total. It will feature advanced electronic components. It is reported that the Buk-M3, a modernized version of the Buk-M1 system and will be deployed in 2009.[18]
3S-90/M-22 'Uragan' - Naval version of the 9K37 Buk missile system.
SA-N-12 - NATO reporting name of the naval version of the 9K37M1-2.
HQ-16 (Hongqi-16) - Joint People's Republic of China/Russian project to upgrade the naval 9K37M1-2 system 'Shtil' (SA-N-12).[19] Other sources also indicate the project involved some Buk technology.[20]



[edit] Structure
Composition
Complex
(GRAU and NATO designation) 9K37
"Buk"
(SA-11) 9K37-1
"Buk-1"
(SA-11) 9K37M1
"Buk-M1"
(SA-11) 9K37M1-2
"Buk-M1-2"
(SA-17) 9K37M2E
"Buk-M2E" (?)
Command Post 9S470 N/A 9S470M1 9S470M1-2 9S510
Surveillance Radar
(SURN, SOTs or TAR) 9S18 Kupol 1S91M3 9S18M1 Kupol-M1 9S18М1-1 9S112,
9S36
TELAR 9А310,
9А38 9A38 9A310M1 9A310M1-2 9A317
TEL 9А39 2P25M3 9A39M1 9A39M1,
9A39M1-2 9A316




[edit] 9K37 Buk (Beech)
Upper level CP (PBU of the zrbr - zenith-rocket brigade) from the structure of ASU Polyana-D4
4 x zrdn (zenith-rocket division)
CP 9S470
SOTs 9S18 Kupol
3 x zrbat (zenith-rocket battery)
2 x TELAR 9А310
1 x TEL 9А39
Technical service division
Сommunication service platoon
[edit] 2K12M4 Kub-M4 (9K37-1 Buk-1)
1 x SURN 1S91M3 (from the structure of 2K12M3 Kub-M3)
4 x TEL 2P25M3 (from the structure of 2K12M3 Kub-M3)
1 x TELAR 9A38 (from the structure of 9K37 Buk)
[edit] 9K37M1 Buk-M1 (Ganges)
[edit] Technical service division
9V95M1E - mobile automatized control and test station vehicle based on a ZiL-131 with a trailer
9V883, 9V884, 9V894 - repair and technical service vehicles based on Ural-43203-1012
9V881E - technical service workshop based on Ural-43203-1012
9T229 - transporter vehicle for 8 missiles or 6 containers with missiles based on a KrAZ-255Б
9T31M - autocrane
MTO-ATG-M1 - technical service workshop based on ZiL-131
[edit] 9K37M1-2 Buk-M1-2 (Ural)
A command post vehicle 9S470M1-2 may took control over 4 batteries, each has 1 TELAR 9A310M1-2 with 1 x TEL 9A39M1/9A39M1-2 or 2 batteries, each has 1 target acquisition radar 9S18М1-1 and 2 x TELs 9A39M1

Additionally, the TELAR 9A310M1-2 may take control over the Kub vehicles - just the TEL 2P25 or the SURN 1S91 with a TEL 2P25.

[edit] Technical service division
Technical service vehicle MTO 9V881M1-2 with a trailer ZIP 9T456
Technical service workshop MTO AGZ-M1
Technical service and maintenance vehicles MRTO: MRTO-1 9V883M1, MRTO-2 9V884M1, MRTO-3 9V894M1
transport vehicle (TM) 9T243 with a technological equipment set KTO 9T3184
automated control and test mobile station AKIPS 9V95M1
workshop vehicle for the missile maintenance 9T458
unified compressor station UKS-400V
mobile power plant PES-100-T/400-AKP1
[edit] 9K37M2/9K317 Buk-M2
There was an experimental 9А320 TEL (with 8 missiles).

Some works were conducted to utilize a wheeled vehicles for Buk-M2-1 on a KrAZ-260 chassis, but they were not completed. Proposed structure of Buk-M2-1 was the 9S512 CP, 9S112-1 TAR, 9S36-1 TAR and 9А318 TEL with 8 missiles.[21]

[edit] Service
[edit] Operators

Current operators of the Buk missile system. Russia is shown in dark red. Serbia only has the Kub - M system (currently upgrading to SA17) Russia Primary Builder and constructer, unndetermined number of units.
Belarus - 12 batteries[22]
Cyprus - 21 units[citation needed]
Egypt [23]
Finland - 3 batteries (9+9 firing units)[22]
Georgia
India[24]
North Korea[25]
People's Republic of China - Copied as the HQ-16 [26]
Myanmar - 48 delivered in 2008.
Russia - 250[22]
Syria[27]
Ukraine[27]
Venezuela- Buk-M2 buy in progress
Saudi Arabia- Buk-M2e( 20 Batteries)[28] According to Suomen Kuvalehti, Finland is planning to accelerate the replacement of the missile system due to concerns about its susceptibility to electronic warfare,[29].
[edit] Combat service
Abkhaz authorities claimed that Buk air defense system was used to shoot down four Georgian drones at the beginning of May 2008. [30]

Analysts stipulated that Georgian Buk and Tor missile systems were responsible for downing four Russian aircraft, 3 Su-25s close air support aircrafts and 1 Tu-22M strategic bomber in the 2008 South Ossetia war[31][32] U.S. officials have said Georgia's SA-11 Buk-1M was certainly the cause of the Tu-22M Backfire bomber's loss and contributed to the losses of the 3 Su-25s.[33] According to some analysts, the loss of four aircraft is surprising and a heavy toll for Russia given the small size of Georgia's military.[34][35] Some have also pointed out, that Russian electronic counter-measures systems were apparently unable to jam and suppress enemy SAMs in the conflict[36] and that Russia was, surprisingly, unable to come up with effective countermeasures against missile systems they had designed.[32]
 
The Lavochkin OKB S-75 (Russian: С-75; NATO reporting name SA-2 Guideline) is a Soviet designed high-altitude, command guided, surface-to-air missile (SAM) system. Since its first deployment in 1957, it has become the most widely deployed and used air defense missile in history.

This system first gained fame when an S-75 battery shot down a CIA U-2 overflying the Soviet Union in 1960. Later, North Vietnamese forces used the S-75 extensively during the Vietnam War to defend Hanoi and Haiphong. It has also been locally-produced in the People's Republic of China using the names HQ-1 and HQ-2. Other nations have produced so many local variants combining portions of the S-75 system with both indigenously developed components or third party systems, that it has become virtually impossible to find a pure S-75 system today
 
OH no not again waist of forum bandwidth.
look superfalcon
we all know how to use wikipedia and we are all informed about longrange SAMs in world market. for the sake of forum please stop copy and pasting everything so wildly.
unless you have something else on your own to share... like your opinion about which long range SAM pak should buy etc... DONT JUST THROUGH ANY RANDOM SAMs..
 
The S-300 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[2]. 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][dead link] 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), entering service in 2004.

Contents [hide]
1 Variations and upgrades
1.1 S-300 system family tree
1.2 S-300P
1.2.1 Land-based S-300P (SA-10)
1.2.2 Sea-based S-300F (SA-N-6)
1.3 S-300V (SA-12)
1.4 S-300PMU-1/2 (SA-20)
1.5 S-400 (SA-21)
1.6 S-300VM (SA-X-23)
2 Operators and other versions
3 Former operators
4 Possible future operators
5 Combat history
6 Specifications
6.1 Radar
6.2 Missiles
7 References
8 External links


[edit] 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.

[edit] 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


[edit] S-300P
[edit] Land-based S-300P (SA-10)

Two S-300-PM missile TEL and a 'Flap Lid' radarThe 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]

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]

The S-300PS/S-300PM (Russian C-300ПC/C-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 8x8 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.


A side-on close-up, ready to launch. Photo from Field Artillery Magazine.The next modernisation, called the S-300PMU (Russian C-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.[6]

[edit] Sea-based S-300F (SA-N-6)

Close up view of SA-N-6 launchers on Marshal Ustinov.The S-300F Fort (Russian C-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 S-300FM Fort-M (Russian C-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.

[edit] S-300V (SA-12)

S-300V (SA-12a Gladiator)The 9K81 S-300V Antey-300 (Russian 9К81 С-300В Антей-300 - named after Antaeus, NATO reporting name SA-12 Gladiator/Giant) is a bit different from the other versions. 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 miles) while the "GIANT" missiles can engage targets out to 100 km (62 miles) 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 8x8 wheeled transporters. It is also somewhat more distributed than the S-300P's. For example, while both have mechanically-scanned radar for target acquisition (9S15 BILL BOARD A), the battery level 9S32 GRILL PAN has 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 autonomous search (later upgraded).


SA-12 high altitude surface-to-air missile systemsThe S-300V places a greater emphasis on ABM, with the dedicated 9M83 (SA-12B Giant). 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 TELARs can be used with the system. The 9A83-1 which holds 4 9M83 GLADIATOR missiles and the 9A82 which holds 2 9M82 GIANT missiles are pure launchers, while the 9A84 (4× 9M83 GLADIATOR missile) and 9A85 (2× 9M82 GIANT missile) are loaders/launchers.

S-300V system may be controlled by a upper level command post system 9S52 Polyana-D4 integrating it with Buk missile system into a brigade.

[edit] S-300PMU-1/2 (SA-20)

S-300PMU-2 64N6E2 acquisition radar (part of 83M6E2 command post)The S-300PMU-1 (Russian C-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.[9] 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, 48N6E and 48N6E2 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.[10]


S-300PMU-2 vehicles. From left to right: 64N6E2 detection radar, 54K6E2 command post and 5P85 TEL.The S-300PMU-2 Favorite (Russian C-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, just like the S-300PMU-1.[3]

[edit] S-400 (SA-21)
Main article: S-400
The S-400 Triumf (Russian С-400 «Триумф», formerly known as the S-300PMU-3/C-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 claimed to be able to detect stealth targets it is by far the most advanced version.[11][dead link] Little else is known about this version.

[edit] S-300VM (SA-X-23)
Main article: S-300VM
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. As all-round surveillance radar the 9S15M2, 9S15MT2E or 9S15MV2E are possible, and the sector surveillance radar was upgraded to 9S19ME. The upgraded guidance radar has Grau index 9S32ME. The system can still employ up to 6 TELARs, the 9A84ME launchers (up to 4 × 9M83ME missile) and up to 6 launcher/loader vehicles assigned to each launcher (2 × 9M83ME missile each).

[edit] Operators and other versions

Producers and users of the S-300 and its main competitor MIM-104 PatriotThe S-300 is mainly used in Eastern Europe and Asia although sources are inconsistent about the exact countries possessing the system.[12]

Armenia Deployed in Armenia by Russia in 102nd Military Base[13][14]
Belarus - S-300PS systems delivered from Russia in 2007 to replace older S-300 model in Belarussian inventory,Older S-300V sold to Turkey for testing and using on Anatolian Eagle exercises.
Bulgaria has ten S-300 launchers, divided into two units with five launchers each.[15]
People's Republic of China: China has bought the S-300PMU-1 and are licensed to manufacture it under the name Hongqi-10 (HQ-10). China is also the first customer of S-300PMU-2 and may be using the S-300V under the name Hongqi HQ-18.[16] 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 (124 mi). There are unconfirmed reports that claim this version is the Chinese manufactured S-300PMU-2.[17][18] 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.[18] 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 bought the S-300PMU-1 version, but due to political tension between Cyprus and Turkey and intense Turkish pressure, the system was transferred to the Greek Island of Crete. Later, Cyprus acquired the Tor-M1 system and the Buk-M1 system. Finally, on 19/12/07 the missiles passed officially to Greek government in return for more Tor-M1 systems and Buk-M1 systems.[15]
India has bought six S-300 batteries in August 1995 for $1 billion, probably the S-300PMU-2 version, believed to consist of 48 missiles per system. These will most likely be used in the short-range ballistic-missile defence (BMD) role against Pakistan's M-11 missiles.[19]
Iran 's status regarding the S-300 system remains controversial. They seem to have acquired an unknown number of S-300PMU-1 missiles in 1993, maybe even 300 recently from Belarus.[20] Iran claimed to have signed a contract with Russia on 25 December 2007 on the sales of the S-300PMU-2 missile system.[21] Russian officials have denied this.[22] According to senior Israeli defence sources Iran is to receive S-300s by 2009, deliveries will take place from September until begin 2009.[23][24][25] It has also been claimed that Croatia sold their S-300s to Iran.[26] Later, another claim was made saying Libya transferred S-300s to Iran.[27]. On December 21, 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.[28] On 28 October 2009, When asked when Russia would deliver the systems to Iran, Ivanov said: "There have been no such deliveries to date."[29] 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.[30]
Kazakhstan
Serbia Serbia bought 6-10 s-300PMU prior to 1999 NATO bombing campaign. At the time 20 misilles were delivered but without Clam Shell radar unit.[31]
Slovakia - Inherited from Czechoslovakia. Slovakian proposal to equip another battalion in mid '90 was canceled.
Syria announced an intention to buy the S-300P in 1991 and now seems to possess the system.[12][20]
Russia: Has used all of the S-300 variations. The Russian Air Defense Forces, which are part of the Air Force, currently deploy more than 30 regiments equipped with S-300 missile complexes, which are gradually being replaced with S-400 systems.[32] More than 20 Russian battalions will be equipped with S-400 anti-missile systems by 2015 said General of the Army Yury Baluyevsky, Chief of the General Staff of the Armed Forces of the Russian Federation.[33]
Ukraine - S-300PS, S-300PMU, S-300V and others.[34]
United States has bought an S-300V system for evaluation, to aid upgrading US Patriot missile systems.
Venezuela Venezuela has ordered S-300VM "Antey-2500" to equip 12 Regiments. Deleveries are expected to be completed by 2010-2011.[35]
Vietnam has bought two S-300PMU-1 batteries (12 launchers) for nearly $300 million.[36]
[edit] Former operators
Croatia: Croatia no longer maintains an S-300 system. It was acquired from Ukraine or Belarus in 1995 and was never 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.
Czechoslovakia - One battalion created in 1985. Passed on to Slovakia in 1992.
East Germany
Soviet Union
[edit] Possible future operators
Venezuela Venezuelan government has recently confirmed a contract with the Russian government to buy one S-300 missile system.[37]
Libya - 4 S-300PMU-2 systems will be ordered
Indonesia - Indonesian air force has shown interest of acquiring several S-300PMU-2 systems
Algeria - 8 S-300PMU2 was ordered in 2006.
Saudi Arabia - Saudi Arabia is in talks to purchase the newest system S-400.[38]
[edit] 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 SEAD missions.[6] Participating countries were pleased that the Slovak Air Force brought a S-300PMU along, providing a unique opportunity for NATO to get familiar with the system.

Israel has sought F-35 Lightning II fighters to nullify the threat of S-300 missiles being provided to Iran.[39][40]

[edit] 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.

[edit] 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 1000 km (620 mi) away travelling at up to 10000 km/h (6200 mph) and cruise missile class targets up to 300 km (185 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 (12.5 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 (108 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 (186 mi).

The S-300 FC Radar Flap Lid can be mounted on a standard pylon.

Surveillance radar 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[41] TOP STEER Naval 300 km (186mile) D/E S-300F
MR-800 Voskhod[41] TOP PAIR Naval 200 km (124mile) C/D/E/F S-300F
Target tracking/missile guidance 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

[edit] Missiles

two types of missiles for the Russian SA-20 anti-air complexMissile specifications GRAU index Year Range Maximum velocity Length Diameter Weight Warhead Guidance First used with
5V55K/KD 1978 47 km (29mile) 1,700m/s (3,800 mph) 7 m (23 ft) 450mm 1,450 kg (3,200 lb) 100 kg (220 lb) Command
5V55R/RM 1984 90 km (56mile) 1,700m/s (3,800 mph) 7 m (23 ft) 450mm 1,450 kg (3,200 lb) 133 kg (293 lb) SARH
5V55U 1992 150 km (93mile) 2,000m/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) 2,000m/s (4,470 mph) 7.5 m (25 ft) 500mm 1,780 kg (3,920 lb) ~150 kg (~330 lb) TVM
48N6E2 1992 195 km (121mile) 2,000m/s (4,470 mph) 7.5 m (25 ft) 500mm 1,800 kg (3,970 lb) 150 kg (330 lb) TVM
9M82 1984 40 km (25mile) 2,500m/s (5,600 mph) 150 kg (330 lb) SARH by TELAR S-300V
9M83 1984 100 km (60mile) 1,800m/s (4,030 mph) 420 kg (926 lb) 150 kg (330 lb) SARH by TELAR S-300V
9M83ME 1990 200 km (120mile) SARH by TELAR S-300VM
9M96E1 1999 40 km (25mile) 900m/s[42] (2,010 mph) 330 kg (728 lb) 24 kg (53 lb) Active Radar Homing S-400
9M96E2 1999 120 km (75mile) 1,000m/s[42] (2,240 mph) 420 kg (926 lb) 24 kg (53 lb) Active Radar Homing S-400
40N6[42] 2000 400 km (250mile) Active Radar Homing S-400

[edit] References
^ a b c "Almaz/Antei Concern of Air Defence S-300P (NATO SA-10 'Grumble') family of low to high-altitude surface-to-air missile systems". Jane's. 2008-01-16. Jane's Login. Retrieved 2008-08-04.
^ "Big Russian flotilla led by Admiral Kuznetsov carrier heads for Syrian port". DEBKAfile. 21 August 2008. http://www.debka.com/headline.php?hid=5526. Retrieved 2008-08-22.
^ a b "Almaz Scientific Industrial Corporation - "FAVORIT S-300 PMU2 SURFACE-TO-AIR MISSILE SYSTEM"". http://www.raspletin.ru/eng/lists/favorit.html. Retrieved 2006-06-23.
^ "Encyclopedia Astronautica - "S-300"". S-300. Retrieved 2008-09-05.
^ a b c German: http://www.dtig.org/docs/sa-10.pdf
^ a b Miroslav Gyürösi (11 March 2005). "Slovak SA-10 radar set to participate in NATO exercise" ([dead link] – Scholar search). Jane's Missiles and Rockets. ISSN 1365-4187. http://www.janes.com/press/articles/pc050317_1.shtml. Retrieved 2006-07-19.
^ "S-300V/Antey 2500 (SA-12 'Gladiator/Giant')". Jane's. 2008-02-13. Jane's Login. Retrieved 2008-08-04.
^ "Federation of American Scientists - "S-300V SA-12A Gladiator and SA-12B Giant - Russia/Soviet Nuclear Forces"". S-300V SA-12A GLADIATOR and SA-12B GIANT - Russia / Soviet Nuclear Forces. Retrieved 2008-09-05.
^ "S-300/Favorit (SA-10 'Grumble'/SA-20 'Gargoyle')". Jane's. 2008-02-08. Jane's Login. Retrieved 2008-08-04.
^ "Rosoboronexport's customer information catalogue for air defence equipment. Click S-300 at the top of the list on the second page." (PDF). http://www.rusarm.ru/p_prod/tmp_proba/airdef_cataloque.html. Retrieved 2006-06-25. [dead link]
^ "New family of Russian missiles will create major problems for air-strike planning in years to come, says leading defence expert". Jane's. 2000-03-08. http://www.janes.com/press/pc000308.shtml. Retrieved 2006-07-25.
^ a b "Center for Nonproliferation Studies - "The Russian S-300PMU-1 TMD System"". http://cns.miis.edu/research/cyprus/s300tdms.htm. Retrieved 2008-09-05.
^ Russia has officially admitted that its sophisticated S-300 air-defense missiles are being deployed in Armenia to upgrade the weaponry of its military base and ward off "threats from Turkey," Snark news agency reported on Thursday quoting Russian officials.
^ Arménie, notre amie...
^ a b "Balkananalysis.com - "Balkan Defense Overview: Developments and Prospects "". Balkanalysis.com Balkan Defense Overview: Developments and Prospects. Retrieved 2008-09-05.
^ "MissileThreat - "Hongqi-10 (HQ-10)"". MissileThreat ::. Retrieved 2008-09-05.
^ "MissileThreat - "Hongqi-15 (HQ-15)"". MissileThreat ::. Retrieved 2008-09-05.
^ a b "Sino Defence Today - "S-300 (SA-10) Surface-to-Air Missile"". S-300PMU (SA-10) Air Defence Missile System - SinoDefence.com. Retrieved 2008-09-05.
^ "Federation of American Scientists - "S-300PMU SA-10 Grumble"". S-300PMU SA-10 GRUMBLE - Russia / Soviet Nuclear Forces. Retrieved 2008-09-05.
^ a b "MissileThreat - "S-300P (SA-10 Grumble)"". MissileThreat :: S-300P (SA-10 Grumble). Retrieved 2008-09-05.
^ Fars News Russia to Deliver S-300 Missile System to Iran 26 December 2007
^ CNN.com [1] 28 December 2007
^ Reuters Iran to get new Russian air defences by '09 -Israel 23 July 2008
^ Presstv 'Iran to be equipped with S-300 by 09' 23 July 2008
^ "BBC News- "Iran and Washington's Israeli option"". 2008-08-28. BBC NEWS | Middle East | America's Israeli option on Iran. Retrieved 2008-07-03.
^ Croatia Suspected of Selling S-300 Antiaircraft Missiles to Iran - Kommersant Moscow
^ Libya Said To Transfer S-300 To Iran, October 28, 2008
^ Russia starts S-300 missile supplies to Iran - Iranian MP | Top Russian news and analysis online | 'RIA Novosti' newswire
^ To date, Russia has not supplied S-300 SAM systems to Iran
^ Press TV Russia: No reason to cancel S-300 deal with Iran, 23 Dec 2009
^ The lessons and non-lessons of the air and missile campaign in Kosovo Аутор: Anthony H. Cordesman, page 350
^ S-400 system deployment postponed - Russian AF commander -1
^ Russia to equip 20 battalions with S-400 air defense systems -1
^ Ukraine - Air Force Equipment
^ Venezuela to build strong air defenses with Russian aid | Top Russian news and analysis online | 'RIA Novosti' newswire
^ "Asia Times - "Russian missiles to guard sky over Vietnam"". Asia Times - Russian missiles to guard skies over Vietnam. Retrieved 2008-09-05.
^ Chavez in $2bn Russian arms deal
^ S-300 missile deliveries to Iran under review — Russian official
^ Israel 'close to deal on F-35'
^ Israel orders U.S. stealth planes to counter Iran, Syria threat
^ 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
 
The S-300 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[2]. 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][dead link] 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), entering service in 2004.

Contents [hide]
1 Variations and upgrades
1.1 S-300 system family tree
1.2 S-300P
1.2.1 Land-based S-300P (SA-10)
1.2.2 Sea-based S-300F (SA-N-6)
1.3 S-300V (SA-12)
1.4 S-300PMU-1/2 (SA-20)
1.5 S-400 (SA-21)
1.6 S-300VM (SA-X-23)
2 Operators and other versions
3 Former operators
4 Possible future operators
5 Combat history
6 Specifications
6.1 Radar
6.2 Missiles
7 References
8 External links


[edit] 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.

[edit] 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


[edit] S-300P
[edit] Land-based S-300P (SA-10)

Two S-300-PM missile TEL and a 'Flap Lid' radarThe 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]

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]

The S-300PS/S-300PM (Russian C-300ПC/C-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 8x8 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.


A side-on close-up, ready to launch. Photo from Field Artillery Magazine.The next modernisation, called the S-300PMU (Russian C-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.[6]

[edit] Sea-based S-300F (SA-N-6)

Close up view of SA-N-6 launchers on Marshal Ustinov.The S-300F Fort (Russian C-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 S-300FM Fort-M (Russian C-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.

[edit] S-300V (SA-12)

S-300V (SA-12a Gladiator)The 9K81 S-300V Antey-300 (Russian 9К81 С-300В Антей-300 - named after Antaeus, NATO reporting name SA-12 Gladiator/Giant) is a bit different from the other versions. 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 miles) while the "GIANT" missiles can engage targets out to 100 km (62 miles) 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 8x8 wheeled transporters. It is also somewhat more distributed than the S-300P's. For example, while both have mechanically-scanned radar for target acquisition (9S15 BILL BOARD A), the battery level 9S32 GRILL PAN has 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 autonomous search (later upgraded).


SA-12 high altitude surface-to-air missile systemsThe S-300V places a greater emphasis on ABM, with the dedicated 9M83 (SA-12B Giant). 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 TELARs can be used with the system. The 9A83-1 which holds 4 9M83 GLADIATOR missiles and the 9A82 which holds 2 9M82 GIANT missiles are pure launchers, while the 9A84 (4× 9M83 GLADIATOR missile) and 9A85 (2× 9M82 GIANT missile) are loaders/launchers.

S-300V system may be controlled by a upper level command post system 9S52 Polyana-D4 integrating it with Buk missile system into a brigade.

[edit] S-300PMU-1/2 (SA-20)

S-300PMU-2 64N6E2 acquisition radar (part of 83M6E2 command post)The S-300PMU-1 (Russian C-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.[9] 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, 48N6E and 48N6E2 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.[10]


S-300PMU-2 vehicles. From left to right: 64N6E2 detection radar, 54K6E2 command post and 5P85 TEL.The S-300PMU-2 Favorite (Russian C-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, just like the S-300PMU-1.[3]

[edit] S-400 (SA-21)
Main article: S-400
The S-400 Triumf (Russian С-400 «Триумф», formerly known as the S-300PMU-3/C-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 claimed to be able to detect stealth targets it is by far the most advanced version.[11][dead link] Little else is known about this version.

[edit] S-300VM (SA-X-23)
Main article: S-300VM
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. As all-round surveillance radar the 9S15M2, 9S15MT2E or 9S15MV2E are possible, and the sector surveillance radar was upgraded to 9S19ME. The upgraded guidance radar has Grau index 9S32ME. The system can still employ up to 6 TELARs, the 9A84ME launchers (up to 4 × 9M83ME missile) and up to 6 launcher/loader vehicles assigned to each launcher (2 × 9M83ME missile each).

[edit] Operators and other versions

Producers and users of the S-300 and its main competitor MIM-104 PatriotThe S-300 is mainly used in Eastern Europe and Asia although sources are inconsistent about the exact countries possessing the system.[12]

Armenia Deployed in Armenia by Russia in 102nd Military Base[13][14]
Belarus - S-300PS systems delivered from Russia in 2007 to replace older S-300 model in Belarussian inventory,Older S-300V sold to Turkey for testing and using on Anatolian Eagle exercises.
Bulgaria has ten S-300 launchers, divided into two units with five launchers each.[15]
People's Republic of China: China has bought the S-300PMU-1 and are licensed to manufacture it under the name Hongqi-10 (HQ-10). China is also the first customer of S-300PMU-2 and may be using the S-300V under the name Hongqi HQ-18.[16] 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 (124 mi). There are unconfirmed reports that claim this version is the Chinese manufactured S-300PMU-2.[17][18] 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.[18] 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 bought the S-300PMU-1 version, but due to political tension between Cyprus and Turkey and intense Turkish pressure, the system was transferred to the Greek Island of Crete. Later, Cyprus acquired the Tor-M1 system and the Buk-M1 system. Finally, on 19/12/07 the missiles passed officially to Greek government in return for more Tor-M1 systems and Buk-M1 systems.[15]
India has bought six S-300 batteries in August 1995 for $1 billion, probably the S-300PMU-2 version, believed to consist of 48 missiles per system. These will most likely be used in the short-range ballistic-missile defence (BMD) role against Pakistan's M-11 missiles.[19]
Iran 's status regarding the S-300 system remains controversial. They seem to have acquired an unknown number of S-300PMU-1 missiles in 1993, maybe even 300 recently from Belarus.[20] Iran claimed to have signed a contract with Russia on 25 December 2007 on the sales of the S-300PMU-2 missile system.[21] Russian officials have denied this.[22] According to senior Israeli defence sources Iran is to receive S-300s by 2009, deliveries will take place from September until begin 2009.[23][24][25] It has also been claimed that Croatia sold their S-300s to Iran.[26] Later, another claim was made saying Libya transferred S-300s to Iran.[27]. On December 21, 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.[28] On 28 October 2009, When asked when Russia would deliver the systems to Iran, Ivanov said: "There have been no such deliveries to date."[29] 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.[30]
Kazakhstan
Serbia Serbia bought 6-10 s-300PMU prior to 1999 NATO bombing campaign. At the time 20 misilles were delivered but without Clam Shell radar unit.[31]
Slovakia - Inherited from Czechoslovakia. Slovakian proposal to equip another battalion in mid '90 was canceled.
Syria announced an intention to buy the S-300P in 1991 and now seems to possess the system.[12][20]
Russia: Has used all of the S-300 variations. The Russian Air Defense Forces, which are part of the Air Force, currently deploy more than 30 regiments equipped with S-300 missile complexes, which are gradually being replaced with S-400 systems.[32] More than 20 Russian battalions will be equipped with S-400 anti-missile systems by 2015 said General of the Army Yury Baluyevsky, Chief of the General Staff of the Armed Forces of the Russian Federation.[33]
Ukraine - S-300PS, S-300PMU, S-300V and others.[34]
United States has bought an S-300V system for evaluation, to aid upgrading US Patriot missile systems.
Venezuela Venezuela has ordered S-300VM "Antey-2500" to equip 12 Regiments. Deleveries are expected to be completed by 2010-2011.[35]
Vietnam has bought two S-300PMU-1 batteries (12 launchers) for nearly $300 million.[36]
[edit] Former operators
Croatia: Croatia no longer maintains an S-300 system. It was acquired from Ukraine or Belarus in 1995 and was never 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.
Czechoslovakia - One battalion created in 1985. Passed on to Slovakia in 1992.
East Germany
Soviet Union
[edit] Possible future operators
Venezuela Venezuelan government has recently confirmed a contract with the Russian government to buy one S-300 missile system.[37]
Libya - 4 S-300PMU-2 systems will be ordered
Indonesia - Indonesian air force has shown interest of acquiring several S-300PMU-2 systems
Algeria - 8 S-300PMU2 was ordered in 2006.
Saudi Arabia - Saudi Arabia is in talks to purchase the newest system S-400.[38]
[edit] 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 SEAD missions.[6] Participating countries were pleased that the Slovak Air Force brought a S-300PMU along, providing a unique opportunity for NATO to get familiar with the system.

Israel has sought F-35 Lightning II fighters to nullify the threat of S-300 missiles being provided to Iran.[39][40]

[edit] 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.

[edit] 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 1000 km (620 mi) away travelling at up to 10000 km/h (6200 mph) and cruise missile class targets up to 300 km (185 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 (12.5 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 (108 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 (186 mi).

The S-300 FC Radar Flap Lid can be mounted on a standard pylon.

Surveillance radar 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[41] TOP STEER Naval 300 km (186mile) D/E S-300F
MR-800 Voskhod[41] TOP PAIR Naval 200 km (124mile) C/D/E/F S-300F
Target tracking/missile guidance 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

[edit] Missiles

two types of missiles for the Russian SA-20 anti-air complexMissile specifications GRAU index Year Range Maximum velocity Length Diameter Weight Warhead Guidance First used with
5V55K/KD 1978 47 km (29mile) 1,700m/s (3,800 mph) 7 m (23 ft) 450mm 1,450 kg (3,200 lb) 100 kg (220 lb) Command
5V55R/RM 1984 90 km (56mile) 1,700m/s (3,800 mph) 7 m (23 ft) 450mm 1,450 kg (3,200 lb) 133 kg (293 lb) SARH
5V55U 1992 150 km (93mile) 2,000m/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) 2,000m/s (4,470 mph) 7.5 m (25 ft) 500mm 1,780 kg (3,920 lb) ~150 kg (~330 lb) TVM
48N6E2 1992 195 km (121mile) 2,000m/s (4,470 mph) 7.5 m (25 ft) 500mm 1,800 kg (3,970 lb) 150 kg (330 lb) TVM
9M82 1984 40 km (25mile) 2,500m/s (5,600 mph) 150 kg (330 lb) SARH by TELAR S-300V
9M83 1984 100 km (60mile) 1,800m/s (4,030 mph) 420 kg (926 lb) 150 kg (330 lb) SARH by TELAR S-300V
9M83ME 1990 200 km (120mile) SARH by TELAR S-300VM
9M96E1 1999 40 km (25mile) 900m/s[42] (2,010 mph) 330 kg (728 lb) 24 kg (53 lb) Active Radar Homing S-400
9M96E2 1999 120 km (75mile) 1,000m/s[42] (2,240 mph) 420 kg (926 lb) 24 kg (53 lb) Active Radar Homing S-400
40N6[42] 2000 400 km (250mile) Active Radar Homing S-400

[edit] References
^ a b c "Almaz/Antei Concern of Air Defence S-300P (NATO SA-10 'Grumble') family of low to high-altitude surface-to-air missile systems". Jane's. 2008-01-16. Jane's Login. Retrieved 2008-08-04.
^ "Big Russian flotilla led by Admiral Kuznetsov carrier heads for Syrian port". DEBKAfile. 21 August 2008. http://www.debka.com/headline.php?hid=5526. Retrieved 2008-08-22.
^ a b "Almaz Scientific Industrial Corporation - "FAVORIT S-300 PMU2 SURFACE-TO-AIR MISSILE SYSTEM"". http://www.raspletin.ru/eng/lists/favorit.html. Retrieved 2006-06-23.
^ "Encyclopedia Astronautica - "S-300"". S-300. Retrieved 2008-09-05.
^ a b c German: http://www.dtig.org/docs/sa-10.pdf
^ a b Miroslav Gyürösi (11 March 2005). "Slovak SA-10 radar set to participate in NATO exercise" ([dead link] – Scholar search). Jane's Missiles and Rockets. ISSN 1365-4187. http://www.janes.com/press/articles/pc050317_1.shtml. Retrieved 2006-07-19.
^ "S-300V/Antey 2500 (SA-12 'Gladiator/Giant')". Jane's. 2008-02-13. Jane's Login. Retrieved 2008-08-04.
^ "Federation of American Scientists - "S-300V SA-12A Gladiator and SA-12B Giant - Russia/Soviet Nuclear Forces"". S-300V SA-12A GLADIATOR and SA-12B GIANT - Russia / Soviet Nuclear Forces. Retrieved 2008-09-05.
^ "S-300/Favorit (SA-10 'Grumble'/SA-20 'Gargoyle')". Jane's. 2008-02-08. Jane's Login. Retrieved 2008-08-04.
^ "Rosoboronexport's customer information catalogue for air defence equipment. Click S-300 at the top of the list on the second page." (PDF). http://www.rusarm.ru/p_prod/tmp_proba/airdef_cataloque.html. Retrieved 2006-06-25. [dead link]
^ "New family of Russian missiles will create major problems for air-strike planning in years to come, says leading defence expert". Jane's. 2000-03-08. http://www.janes.com/press/pc000308.shtml. Retrieved 2006-07-25.
^ a b "Center for Nonproliferation Studies - "The Russian S-300PMU-1 TMD System"". http://cns.miis.edu/research/cyprus/s300tdms.htm. Retrieved 2008-09-05.
^ Russia has officially admitted that its sophisticated S-300 air-defense missiles are being deployed in Armenia to upgrade the weaponry of its military base and ward off "threats from Turkey," Snark news agency reported on Thursday quoting Russian officials.
^ Arménie, notre amie...
^ a b "Balkananalysis.com - "Balkan Defense Overview: Developments and Prospects "". Balkanalysis.com Balkan Defense Overview: Developments and Prospects. Retrieved 2008-09-05.
^ "MissileThreat - "Hongqi-10 (HQ-10)"". MissileThreat ::. Retrieved 2008-09-05.
^ "MissileThreat - "Hongqi-15 (HQ-15)"". MissileThreat ::. Retrieved 2008-09-05.
^ a b "Sino Defence Today - "S-300 (SA-10) Surface-to-Air Missile"". S-300PMU (SA-10) Air Defence Missile System - SinoDefence.com. Retrieved 2008-09-05.
^ "Federation of American Scientists - "S-300PMU SA-10 Grumble"". S-300PMU SA-10 GRUMBLE - Russia / Soviet Nuclear Forces. Retrieved 2008-09-05.
^ a b "MissileThreat - "S-300P (SA-10 Grumble)"". MissileThreat :: S-300P (SA-10 Grumble). Retrieved 2008-09-05.
^ Fars News Russia to Deliver S-300 Missile System to Iran 26 December 2007
^ CNN.com [1] 28 December 2007
^ Reuters Iran to get new Russian air defences by '09 -Israel 23 July 2008
^ Presstv 'Iran to be equipped with S-300 by 09' 23 July 2008
^ "BBC News- "Iran and Washington's Israeli option"". 2008-08-28. BBC NEWS | Middle East | America's Israeli option on Iran. Retrieved 2008-07-03.
^ Croatia Suspected of Selling S-300 Antiaircraft Missiles to Iran - Kommersant Moscow
^ Libya Said To Transfer S-300 To Iran, October 28, 2008
^ Russia starts S-300 missile supplies to Iran - Iranian MP | Top Russian news and analysis online | 'RIA Novosti' newswire
^ To date, Russia has not supplied S-300 SAM systems to Iran
^ Press TV Russia: No reason to cancel S-300 deal with Iran, 23 Dec 2009
^ The lessons and non-lessons of the air and missile campaign in Kosovo Аутор: Anthony H. Cordesman, page 350
^ S-400 system deployment postponed - Russian AF commander -1
^ Russia to equip 20 battalions with S-400 air defense systems -1
^ Ukraine - Air Force Equipment
^ Venezuela to build strong air defenses with Russian aid | Top Russian news and analysis online | 'RIA Novosti' newswire
^ "Asia Times - "Russian missiles to guard sky over Vietnam"". Asia Times - Russian missiles to guard skies over Vietnam. Retrieved 2008-09-05.
^ Chavez in $2bn Russian arms deal
^ S-300 missile deliveries to Iran under review — Russian official
^ Israel 'close to deal on F-35'
^ Israel orders U.S. stealth planes to counter Iran, Syria threat
^ 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
 
PAF will take J-10B, and enhance its capabilities further so that it can compete with Typhoon and Rafale. Range and payload may be a limiting aspect, but PAF can certainly resolve issues surrounding radar, ECM/EW, avionics and weapon-systems. In other words, FC-20 will be the PAF's key against MRCA, and if things go well, we can see 150 FC-20s in service.

As for long-range SAMs, Pakistan will likely adopt an export version of HQ-9A, and then modify it with a mix of indigenous and Western technology in certain areas. I suspect we may see cooperation with Turkey in this regard.
 
The S-300 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[2]. 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][dead link] 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), entering service in 2004.

Contents [hide]
1 Variations and upgrades
1.1 S-300 system family tree
1.2 S-300P
1.2.1 Land-based S-300P (SA-10)
1.2.2 Sea-based S-300F (SA-N-6)
1.3 S-300V (SA-12)
1.4 S-300PMU-1/2 (SA-20)
1.5 S-400 (SA-21)
1.6 S-300VM (SA-X-23)
2 Operators and other versions
3 Former operators
4 Possible future operators
5 Combat history
6 Specifications
6.1 Radar
6.2 Missiles
7 References
8 External links


[edit] 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.

[edit] 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


[edit] S-300P
[edit] Land-based S-300P (SA-10)

Two S-300-PM missile TEL and a 'Flap Lid' radarThe 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]

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]

The S-300PS/S-300PM (Russian C-300ПC/C-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 8x8 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.


A side-on close-up, ready to launch. Photo from Field Artillery Magazine.The next modernisation, called the S-300PMU (Russian C-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.[6]

[edit] Sea-based S-300F (SA-N-6)

Close up view of SA-N-6 launchers on Marshal Ustinov.The S-300F Fort (Russian C-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 S-300FM Fort-M (Russian C-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.

[edit] S-300V (SA-12)

S-300V (SA-12a Gladiator)The 9K81 S-300V Antey-300 (Russian 9К81 С-300В Антей-300 - named after Antaeus, NATO reporting name SA-12 Gladiator/Giant) is a bit different from the other versions. 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 miles) while the "GIANT" missiles can engage targets out to 100 km (62 miles) 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 8x8 wheeled transporters. It is also somewhat more distributed than the S-300P's. For example, while both have mechanically-scanned radar for target acquisition (9S15 BILL BOARD A), the battery level 9S32 GRILL PAN has 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 autonomous search (later upgraded).


SA-12 high altitude surface-to-air missile systemsThe S-300V places a greater emphasis on ABM, with the dedicated 9M83 (SA-12B Giant). 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 TELARs can be used with the system. The 9A83-1 which holds 4 9M83 GLADIATOR missiles and the 9A82 which holds 2 9M82 GIANT missiles are pure launchers, while the 9A84 (4× 9M83 GLADIATOR missile) and 9A85 (2× 9M82 GIANT missile) are loaders/launchers.

S-300V system may be controlled by a upper level command post system 9S52 Polyana-D4 integrating it with Buk missile system into a brigade.

[edit] S-300PMU-1/2 (SA-20)

S-300PMU-2 64N6E2 acquisition radar (part of 83M6E2 command post)The S-300PMU-1 (Russian C-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.[9] 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, 48N6E and 48N6E2 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.[10]


S-300PMU-2 vehicles. From left to right: 64N6E2 detection radar, 54K6E2 command post and 5P85 TEL.The S-300PMU-2 Favorite (Russian C-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, just like the S-300PMU-1.[3]

[edit] S-400 (SA-21)
Main article: S-400
The S-400 Triumf (Russian С-400 «Триумф», formerly known as the S-300PMU-3/C-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 claimed to be able to detect stealth targets it is by far the most advanced version.[11][dead link] Little else is known about this version.

[edit] S-300VM (SA-X-23)
Main article: S-300VM
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. As all-round surveillance radar the 9S15M2, 9S15MT2E or 9S15MV2E are possible, and the sector surveillance radar was upgraded to 9S19ME. The upgraded guidance radar has Grau index 9S32ME. The system can still employ up to 6 TELARs, the 9A84ME launchers (up to 4 × 9M83ME missile) and up to 6 launcher/loader vehicles assigned to each launcher (2 × 9M83ME missile each).

[edit] Operators and other versions

Producers and users of the S-300 and its main competitor MIM-104 PatriotThe S-300 is mainly used in Eastern Europe and Asia although sources are inconsistent about the exact countries possessing the system.[12]

Armenia Deployed in Armenia by Russia in 102nd Military Base[13][14]
Belarus - S-300PS systems delivered from Russia in 2007 to replace older S-300 model in Belarussian inventory,Older S-300V sold to Turkey for testing and using on Anatolian Eagle exercises.
Bulgaria has ten S-300 launchers, divided into two units with five launchers each.[15]
People's Republic of China: China has bought the S-300PMU-1 and are licensed to manufacture it under the name Hongqi-10 (HQ-10). China is also the first customer of S-300PMU-2 and may be using the S-300V under the name Hongqi HQ-18.[16] 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 (124 mi). There are unconfirmed reports that claim this version is the Chinese manufactured S-300PMU-2.[17][18] 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.[18] 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 bought the S-300PMU-1 version, but due to political tension between Cyprus and Turkey and intense Turkish pressure, the system was transferred to the Greek Island of Crete. Later, Cyprus acquired the Tor-M1 system and the Buk-M1 system. Finally, on 19/12/07 the missiles passed officially to Greek government in return for more Tor-M1 systems and Buk-M1 systems.[15]
India has bought six S-300 batteries in August 1995 for $1 billion, probably the S-300PMU-2 version, believed to consist of 48 missiles per system. These will most likely be used in the short-range ballistic-missile defence (BMD) role against Pakistan's M-11 missiles.[19]
Iran 's status regarding the S-300 system remains controversial. They seem to have acquired an unknown number of S-300PMU-1 missiles in 1993, maybe even 300 recently from Belarus.[20] Iran claimed to have signed a contract with Russia on 25 December 2007 on the sales of the S-300PMU-2 missile system.[21] Russian officials have denied this.[22] According to senior Israeli defence sources Iran is to receive S-300s by 2009, deliveries will take place from September until begin 2009.[23][24][25] It has also been claimed that Croatia sold their S-300s to Iran.[26] Later, another claim was made saying Libya transferred S-300s to Iran.[27]. On December 21, 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.[28] On 28 October 2009, When asked when Russia would deliver the systems to Iran, Ivanov said: "There have been no such deliveries to date."[29] 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.[30]
Kazakhstan
Serbia Serbia bought 6-10 s-300PMU prior to 1999 NATO bombing campaign. At the time 20 misilles were delivered but without Clam Shell radar unit.[31]
Slovakia - Inherited from Czechoslovakia. Slovakian proposal to equip another battalion in mid '90 was canceled.
Syria announced an intention to buy the S-300P in 1991 and now seems to possess the system.[12][20]
Russia: Has used all of the S-300 variations. The Russian Air Defense Forces, which are part of the Air Force, currently deploy more than 30 regiments equipped with S-300 missile complexes, which are gradually being replaced with S-400 systems.[32] More than 20 Russian battalions will be equipped with S-400 anti-missile systems by 2015 said General of the Army Yury Baluyevsky, Chief of the General Staff of the Armed Forces of the Russian Federation.[33]
Ukraine - S-300PS, S-300PMU, S-300V and others.[34]
United States has bought an S-300V system for evaluation, to aid upgrading US Patriot missile systems.
Venezuela Venezuela has ordered S-300VM "Antey-2500" to equip 12 Regiments. Deleveries are expected to be completed by 2010-2011.[35]
Vietnam has bought two S-300PMU-1 batteries (12 launchers) for nearly $300 million.[36]
[edit] Former operators
Croatia: Croatia no longer maintains an S-300 system. It was acquired from Ukraine or Belarus in 1995 and was never 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.
Czechoslovakia - One battalion created in 1985. Passed on to Slovakia in 1992.
East Germany
Soviet Union
[edit] Possible future operators
Venezuela Venezuelan government has recently confirmed a contract with the Russian government to buy one S-300 missile system.[37]
Libya - 4 S-300PMU-2 systems will be ordered
Indonesia - Indonesian air force has shown interest of acquiring several S-300PMU-2 systems
Algeria - 8 S-300PMU2 was ordered in 2006.
Saudi Arabia - Saudi Arabia is in talks to purchase the newest system S-400.[38]
[edit] 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 SEAD missions.[6] Participating countries were pleased that the Slovak Air Force brought a S-300PMU along, providing a unique opportunity for NATO to get familiar with the system.

Israel has sought F-35 Lightning II fighters to nullify the threat of S-300 missiles being provided to Iran.[39][40]

[edit] 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.

[edit] 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 1000 km (620 mi) away travelling at up to 10000 km/h (6200 mph) and cruise missile class targets up to 300 km (185 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 (12.5 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 (108 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 (186 mi).

The S-300 FC Radar Flap Lid can be mounted on a standard pylon.

Surveillance radar 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[41] TOP STEER Naval 300 km (186mile) D/E S-300F
MR-800 Voskhod[41] TOP PAIR Naval 200 km (124mile) C/D/E/F S-300F
Target tracking/missile guidance 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

[edit] Missiles

two types of missiles for the Russian SA-20 anti-air complexMissile specifications GRAU index Year Range Maximum velocity Length Diameter Weight Warhead Guidance First used with
5V55K/KD 1978 47 km (29mile) 1,700m/s (3,800 mph) 7 m (23 ft) 450mm 1,450 kg (3,200 lb) 100 kg (220 lb) Command
5V55R/RM 1984 90 km (56mile) 1,700m/s (3,800 mph) 7 m (23 ft) 450mm 1,450 kg (3,200 lb) 133 kg (293 lb) SARH
5V55U 1992 150 km (93mile) 2,000m/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) 2,000m/s (4,470 mph) 7.5 m (25 ft) 500mm 1,780 kg (3,920 lb) ~150 kg (~330 lb) TVM
48N6E2 1992 195 km (121mile) 2,000m/s (4,470 mph) 7.5 m (25 ft) 500mm 1,800 kg (3,970 lb) 150 kg (330 lb) TVM
9M82 1984 40 km (25mile) 2,500m/s (5,600 mph) 150 kg (330 lb) SARH by TELAR S-300V
9M83 1984 100 km (60mile) 1,800m/s (4,030 mph) 420 kg (926 lb) 150 kg (330 lb) SARH by TELAR S-300V
9M83ME 1990 200 km (120mile) SARH by TELAR S-300VM
9M96E1 1999 40 km (25mile) 900m/s[42] (2,010 mph) 330 kg (728 lb) 24 kg (53 lb) Active Radar Homing S-400
9M96E2 1999 120 km (75mile) 1,000m/s[42] (2,240 mph) 420 kg (926 lb) 24 kg (53 lb) Active Radar Homing S-400
40N6[42] 2000 400 km (250mile) Active Radar Homing S-400

[edit] References
^ a b c "Almaz/Antei Concern of Air Defence S-300P (NATO SA-10 'Grumble') family of low to high-altitude surface-to-air missile systems". Jane's. 2008-01-16. Jane's Login. Retrieved 2008-08-04.
^ "Big Russian flotilla led by Admiral Kuznetsov carrier heads for Syrian port". DEBKAfile. 21 August 2008. http://www.debka.com/headline.php?hid=5526. Retrieved 2008-08-22.
^ a b "Almaz Scientific Industrial Corporation - "FAVORIT S-300 PMU2 SURFACE-TO-AIR MISSILE SYSTEM"". http://www.raspletin.ru/eng/lists/favorit.html. Retrieved 2006-06-23.
^ "Encyclopedia Astronautica - "S-300"". S-300. Retrieved 2008-09-05.
^ a b c German: http://www.dtig.org/docs/sa-10.pdf
^ a b Miroslav Gyürösi (11 March 2005). "Slovak SA-10 radar set to participate in NATO exercise" ([dead link] – Scholar search). Jane's Missiles and Rockets. ISSN 1365-4187. http://www.janes.com/press/articles/pc050317_1.shtml. Retrieved 2006-07-19.
^ "S-300V/Antey 2500 (SA-12 'Gladiator/Giant')". Jane's. 2008-02-13. Jane's Login. Retrieved 2008-08-04.
^ "Federation of American Scientists - "S-300V SA-12A Gladiator and SA-12B Giant - Russia/Soviet Nuclear Forces"". S-300V SA-12A GLADIATOR and SA-12B GIANT - Russia / Soviet Nuclear Forces. Retrieved 2008-09-05.
^ "S-300/Favorit (SA-10 'Grumble'/SA-20 'Gargoyle')". Jane's. 2008-02-08. Jane's Login. Retrieved 2008-08-04.
^ "Rosoboronexport's customer information catalogue for air defence equipment. Click S-300 at the top of the list on the second page." (PDF). http://www.rusarm.ru/p_prod/tmp_proba/airdef_cataloque.html. Retrieved 2006-06-25. [dead link]
^ "New family of Russian missiles will create major problems for air-strike planning in years to come, says leading defence expert". Jane's. 2000-03-08. http://www.janes.com/press/pc000308.shtml. Retrieved 2006-07-25.
^ a b "Center for Nonproliferation Studies - "The Russian S-300PMU-1 TMD System"". http://cns.miis.edu/research/cyprus/s300tdms.htm. Retrieved 2008-09-05.
^ Russia has officially admitted that its sophisticated S-300 air-defense missiles are being deployed in Armenia to upgrade the weaponry of its military base and ward off "threats from Turkey," Snark news agency reported on Thursday quoting Russian officials.
^ Arménie, notre amie...
^ a b "Balkananalysis.com - "Balkan Defense Overview: Developments and Prospects "". Balkanalysis.com Balkan Defense Overview: Developments and Prospects. Retrieved 2008-09-05.
^ "MissileThreat - "Hongqi-10 (HQ-10)"". MissileThreat ::. Retrieved 2008-09-05.
^ "MissileThreat - "Hongqi-15 (HQ-15)"". MissileThreat ::. Retrieved 2008-09-05.
^ a b "Sino Defence Today - "S-300 (SA-10) Surface-to-Air Missile"". S-300PMU (SA-10) Air Defence Missile System - SinoDefence.com. Retrieved 2008-09-05.
^ "Federation of American Scientists - "S-300PMU SA-10 Grumble"". S-300PMU SA-10 GRUMBLE - Russia / Soviet Nuclear Forces. Retrieved 2008-09-05.
^ a b "MissileThreat - "S-300P (SA-10 Grumble)"". MissileThreat :: S-300P (SA-10 Grumble). Retrieved 2008-09-05.
^ Fars News Russia to Deliver S-300 Missile System to Iran 26 December 2007
^ CNN.com [1] 28 December 2007
^ Reuters Iran to get new Russian air defences by '09 -Israel 23 July 2008
^ Presstv 'Iran to be equipped with S-300 by 09' 23 July 2008
^ "BBC News- "Iran and Washington's Israeli option"". 2008-08-28. BBC NEWS | Middle East | America's Israeli option on Iran. Retrieved 2008-07-03.
^ Croatia Suspected of Selling S-300 Antiaircraft Missiles to Iran - Kommersant Moscow
^ Libya Said To Transfer S-300 To Iran, October 28, 2008
^ Russia starts S-300 missile supplies to Iran - Iranian MP | Top Russian news and analysis online | 'RIA Novosti' newswire
^ To date, Russia has not supplied S-300 SAM systems to Iran
^ Press TV Russia: No reason to cancel S-300 deal with Iran, 23 Dec 2009
^ The lessons and non-lessons of the air and missile campaign in Kosovo Аутор: Anthony H. Cordesman, page 350
^ S-400 system deployment postponed - Russian AF commander -1
^ Russia to equip 20 battalions with S-400 air defense systems -1
^ Ukraine - Air Force Equipment
^ Venezuela to build strong air defenses with Russian aid | Top Russian news and analysis online | 'RIA Novosti' newswire
^ "Asia Times - "Russian missiles to guard sky over Vietnam"". Asia Times - Russian missiles to guard skies over Vietnam. Retrieved 2008-09-05.
^ Chavez in $2bn Russian arms deal
^ S-300 missile deliveries to Iran under review — Russian official
^ Israel 'close to deal on F-35'
^ Israel orders U.S. stealth planes to counter Iran, Syria threat
^ 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
 
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