S-300 missile system vs Sevom Khordad

See list of operators^[source]

See § Operators^[source]

Syrian Civil War Second Nagorno-Karabakh War Russo-Ukrainian war^[source]

2019–2020 Persian Gulf crisis Twelve-Day War 2026 Iran War^[source]

Almaz-Antey : NPO Almaz (lead designer) NIIP (radars) MKB Fakel (missile designer for S-300P series) NPO Novator (missile designer for S-300V series) MNIIRE Altair (Naval version designer)^[source]

1967–2005^[source]

MZiK^[source]

Export cost: US$120–150 million (FY 2010) for a battery^[source]

1975 –2011 (for PS and PM)^[source]

see variants^[source]

series of long-range surface-to-air missile systems^[source]

The system is fully automated, though manual observation and operation are also possible. Each targeting radar provides target designation for the central command post. The command post compares the data received from the targeting radars and filters out false targets. The central command post has both active and passive target detection modes. Missiles have a maximum range of 40 kilometres (25 mi) from the command post.^[source]S-300 missile system · Lead; only the objects and conditions stated in this passage

The S-300PT had a passive electronically scanned array radar and had the ability to engage multiple targets with a single fire-control system . Since the original system was semi-mobile, it took just over one hour to set up for firing. It ran the risk of the missile hot launch system scorching the transporter erector launcher (TEL).^[source]S-300 missile system · Variations and upgrades / S-300P (SA-10) / S-300P/S-300PT; only the objects and conditions stated in this passage

It was originally intended to use a track-via-missile (TVM) guidance system. However, the TVM system had problems tracking targets below 500 metres (1,600 ft), allowing incoming SEAD aircraft to effectively utilize terrain masking to avoid tracking. To improve tracking of low-altitude targets, a command-guidance system was added to guide the missile for the initial part of the flight. This allowed the minimum engagement altitude to be set to 25 metres (82 ft).^[source]S-300 missile system · Variations and upgrades / S-300P (SA-10) / S-300P/S-300PT; only the objects and conditions stated in this passage

Improvements to the S-300P resulted in several sub-versions for both domestic and international markets. The S-300PT-1 and S-300PT-1A are incremental upgrades of the original S-300PT system, using a new 5V55KD missile and a cold launch method. The time it took to set the system up was reduced to 30 minutes and trajectory optimizations allowed the 5V55KD to reach ranges up to 75 kilometres (47 mi).^[source]S-300 missile system · Variations and upgrades / S-300P (SA-10) / S-300P/S-300PT; only the objects and conditions stated in this passage

The S-300PS / S-300PM (Russian С-300ПC / С-300ПМ , NATO reporting name SA-10B Grumble B ) was introduced in 1985 (according to Russia) and is the only version thought to have been fitted with a nuclear warhead. This model saw the introduction of the modern TEL and mobile radar and command-post vehicles that were all based on the MAZ-7910 8×8 truck. This model also featured new 5V55R missiles, which increased the maximum engagement range to 75 km (47 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.^[source]S-300 missile system · Variations and upgrades / S-300P (SA-10) / S-300PS/S-300PM; only the objects and conditions stated in this passage

Development of a modernized variant for export, called the S-300PMU ( Russian : С-300ПМУ , NATO reporting name SA-10C Grumble C ), was completed in 1985. The PMU variant was fielded with the 5V55K (range 45–47 kilometres (28–29 mi)) and 5V55R (range 75–90 kilometres (47–56 mi)) missiles. Radars used for the S-300PMU complex included the 30N6 (NATO: "Flap Lid") target engagement radar, the 76N6 (NATO: "Clam Shell") low altitude detection radar, and the ST-68U (NATO: "Tin Shield") 3D search radar. In addition, the 64N6 (NATO: "Big Bird") radar was used as a search radar at the regimental command post (an S-300PMU regiment typically consisted of three missile batteries). The S-300PMU could engage targets with a radar cross section of at least 0.2 square metres (2.2 sq ft) and a maximum velocity of 1,300 metres per second (4,300 ft/s) at altitudes between 25 metres (82 ft) and 27,000 metres (89,000 ft). It could also engage surface targets at ranges up to 30 kilometres (19 mi).^[source]S-300 missile system · Variations and upgrades / S-300P (SA-10) / S-300PMU; only the objects and conditions stated in this passage

The S-300PMU-1 ( Russian : С-300ПМУ-1 , NATO reporting name SA-20A Gargoyle ) was also introduced in 1993, with the new and larger 48N6 missiles for the first time in a land-based system, and keeping all the same performance improvements from the S-300PM version, including the increased speed, range, SAGG guidance, and ABM capability. 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.^[source]S-300 missile system · Variations and upgrades / S-300P (SA-10) / S-300PMU-1/2 (SA-20A/B); only the objects and conditions stated in this passage

Both are significantly smaller than the previous missiles, at 330 and 420 kg (730 and 930 lb), respectively, and carry a smaller 24 kg (53 lb) warhead.^[source]S-300 missile system · Variations and upgrades / S-300P (SA-10) / S-300PMU-1/2 (SA-20A/B); only the objects and conditions stated in this passage

The 9M96E1 has an engagement range of 1–40 km (0.62–25 mi), and the 9M96E2 of 1–120 km (0.62–75 mi).^[source]S-300 missile system · Variations and upgrades / S-300P (SA-10) / S-300PMU-1/2 (SA-20A/B); only the objects and conditions stated in this passage

The S-300PMU-2 Favorit ( Russian : С-300ПМУ-2 Фаворит , NATO reporting name SA-20B Gargoyle ), introduced in 1997 (presented ready 1996), is an upgrade to the S-300PMU-1 with a range of 195 km (121 mi) with the introduction of the 48N6E2 missile. This system is apparently capable against not just short-range ballistic missiles , but also medium-range 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.^[source]S-300 missile system · Variations and upgrades / S-300P (SA-10) / S-300PMU-1/2 (SA-20A/B); only the objects and conditions stated in this passage

The S-300F Fort ( Russian : С-300Ф , DoD designation SA-N-6 , F suffix for Russian : Флотская or Naval ) 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 (4.3–56 mi; 3.8–49 nmi) and maximum target speed up to Mach 4, while the engagement altitude was reduced to 25–25,000 m (82–82,021 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 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 or reef ). The NATO name, found also in colloquial use, is Grumble .^[source]S-300 missile system · Variations and upgrades / S-300F / Sea-based S-300F (SA-N-6); only the objects and conditions stated in this passage

The S-300FM Fort-M ( Russian : С-300ФМ , DoD designation SA-N-20 ) is another naval version of the system, installed only on the Kirov -class cruiser Pyotr Velikiy , and introducing the new 48N6 missile. It was introduced in 1990 and has a missile speed of approximately Mach 6 for a maximum target engagement speed of up to Mach 8.5, a warhead size of 150 kg (330 lb), an engagement range of 5–150 km (3.1–93 mi), and an altitude envelope of 10–27 km (6.2–16.8 mi). The new missiles also introduced a track-via-missile guidance method and 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.^[source]S-300 missile system · Variations and upgrades / S-300F / Sea-based S-300FM (SA-N-20); only the objects and conditions stated in this passage

The 9K81 S-300V Antey-300 ( Russian : 9К81 С-300В Антей-300 – named after Antaeus , NATO reporting name SA-12 Gladiator/Giant ) varies from the other designs in the series. It was built by Antey rather than Almaz, and its 9M82 and 9M83 missiles were designed by NPO Novator . The V suffix stands for Voyska (ground forces). It was designed to be the top-tier army air defence system, replacing the 2K11 Krug , providing a defence against ballistic missiles, cruise missiles, and aircraft. The 9M83 (SA-12A Gladiator) missiles have a maximum engagement range of around 75 km (47 mi), while the 9M82 (SA-12B Giant) missiles can engage targets out to 100 km (62 mi) and up to altitudes of around 32 km (20 mi). In both cases the warhead is around 150 kg (330 lb).^[source]S-300 missile system · Variations and upgrades / S-300V (SA-12); only the objects and conditions stated in this passage

While it was created from the same project, hence sharing the common S-300 designation with the S-300P air defense family, the S-300V had different priorities that resulted in a different design. The S-300V system is carried on tracked MT-T transporters, which gives it better cross-country mobility than the S-300Ps moving on 8×8 wheeled transporters. Its search, tracking, and command systems are more distributed than the S-300P's. For example, while both have mechanically scanning radar for target acquisition (9S15 BILL BOARD A ), the battery level 9S32 GRILL PAN has an autonomous search ability and SARH delegated to illumination radar on transporter erector launcher and radar (TELAR) vehicles. The early 30N6 FLAP LID on the S-300P handles tracking and illumination, but is not equipped with an autonomous search capability (later upgraded). 9S15 can simultaneously carry out active (3 coordinates) and passive (2 positions) searches for targets.^[source]S-300 missile system · Variations and upgrades / S-300V (SA-12); only the objects and conditions stated in this passage

9S15M – 330 kilometres (210 mi) with a 10-square-metre (110 sq ft) cross section and 240 kilometres (150 mi) with a 3-square-metre (32 sq ft) cross section.^[source]S-300 missile system · Variations and upgrades / S-300V (SA-12); only the objects and conditions stated in this passage

9S19M2 – 175 kilometres (109 mi) with an unknown cross-section; it contains two passive electronically scanned arrays with a very high resistance to interference.^[source]S-300 missile system · Variations and upgrades / S-300V (SA-12); only the objects and conditions stated in this passage

9S32M (TELAR 9A82/9A83) – range is limited to 200 kilometres (120 mi), can work independently, or receive target designation from the S-300V, or a variety of other target designation data systems (AWACS aircraft and various ground-based radar). Targets with a radar cross-section of 0.1-square-metre (1.1 sq ft) are detected at ranges up to 140 kilometres (87 mi) and are locked on at 120 kilometres (75 mi). The 9S32 detection range against MGM-52 Lance missiles is 60 kilometres (37 mi), aircraft missiles 80 kilometres (50 mi), fighter or ballistic missile ( MGM-31 Pershing ) 140 kilometres (87 mi) (all of which the U.S. removed from service in 1991).^[source]S-300 missile system · Variations and upgrades / S-300V (SA-12); only the objects and conditions stated in this passage

The ability to hit a target with a cross section of 0.05 square metres (0.54 sq ft) at a distance of 30 kilometres (19 mi) (aiming system in the rocket (10/3 seconds before the missiles hit the target)). In addition, the guidance system inside the rocket supplements missile guidance systems commands from the 9A82 / 9A83 and 9S32, and the missile guidance systems to passively work with the radar illumination and radiation of the 9A82 / 9A83.^[source]S-300 missile system · Variations and upgrades / S-300V (SA-12); only the objects and conditions stated in this passage

The Antey-2500 complex is the export version developed separately from the S-300 family and has been exported to Venezuela for an estimated export price of US$1 billion. The system has one type of missile in two versions, basic and amended, with a sustainer stage that doubles the range (up to 200 km (120 mi), according to other data, up to 250 km (160 mi)), and can simultaneously engage up to 24 aircraft or 16 ballistic targets in various combinations.^[source]S-300 missile system · Variations and upgrades / S-300VM (SA-23); only the objects and conditions stated in this passage

The S-300V4 is also called S-300VMD. It was developed to target high-value airborne targets, such as AWACS aircraft, at long distances. Different versions of the NPO Novator 9M82MD S-300V4 missiles have a range of 400 kilometres (250 mi) at Mach 7.5 or a range of 350 kilometres (220 mi) at Mach 9, and can destroy maneuvering targets even at very high altitudes. An export version exists, marketed as the Antey-4000.^[source]S-300 missile system · Variations and upgrades / S-300V4; only the objects and conditions stated in this passage

The S-400 Triumf ( Russian : С-400 «Триумф» , formerly known as the S-300PMU-3/С-300ПМУ-3, NATO reporting name SA-21 Growler ) was introduced in 1999 and featured a new, larger missile and several upgrades and new features. The project encountered delays since its original announcement, and deployment only began on a small scale in 2006. With an engagement range of up to 400 km (250 mi), depending on the missile variant used, it was specifically designed to counter stealth aircraft. It is by far the most advanced version, incorporating the ability to survive PGM threats and counter advanced jammers by using automatic frequency hopping .^[source]S-300 missile system · Variations and upgrades / S-400 (SA-21); only the objects and conditions stated in this passage

S-300 variants will work together in various combinations, although interoperability between different variants is limited. Various higher-level mobile commands can coordinate certain variants at various locations into a single battery, and also integrate that battery with other air defence systems. A management system, consisting of command control and radars allows for fully automatic initiation and effective management of up to one hundred targets located up to 30–40 kilometres (19–25 mi) from the base station. Many tasks – detection, tracking, target setting, target designation, target acquisition, missile guidance, and assessment of results – can be dealt with automatically. The operator controls the target detection and the launch of rockets. In a complex environment, manual intervention is possible. Few of the previous systems possessed such capabilities.^[source]S-300 missile system · Specifications; only the objects and conditions stated in this passage

The S-300 is a multi-channel anti-aircraft missile system whose variants can engage ballistic missiles as well as aircraft and are able to allocate up to 12 missiles to up to 6 different targets. The system can destroy ground targets at a range of 120 kilometres (75 mi), and when launched on a ballistic trajectory, can reach up to 400 kilometres (250 mi). Its vertically-launched missiles allow for the engagement of flying targets in any direction without traversing the launcher.^[source]S-300 missile system · Specifications; only the objects and conditions stated in this passage

Early versions 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), similar to the U.S.-made 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. Early models can successfully engage targets flying at up to Mach 2.5, or around Mach 8.5 for later models, with one missile potentially being launched every three seconds. The mobile control centre is able to manage up to 12 TELs simultaneously.^[source]S-300 missile system · Specifications; only the objects and conditions stated in this passage

The original warhead weighed 100 kg (220 lb), intermediate warheads weighed 133 kg (293 lb), and the latest warhead weighs 143 kg (315 lb). Each warhead is equipped with a proximity fuse and a contact fuse . A warhead will expel from 19,000 to 36,000 metal fragments upon detonation, depending on missile type. The missiles themselves weigh between 1,450 and 1,800 kg (3,200 and 3,970 lb). Missiles are catapulted clear of the launching tubes before their rocket motors fire, and can accelerate at up to 100 g (1 km/s 2 ). 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 thrust vectoring vanes. The sections below give exact specifications of the radar and missiles in the different S-300 versions. Since the S-300PM, most vehicles are interchangeable across variations.^[source]S-300 missile system · Specifications; only the objects and conditions stated in this passage

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 is typically towed with an 8-wheeled truck. The 76N6 CLAM SHELL (5N66M etc.) is mounted on a large trailer with a mast that is between 24 and 39 m (79 and 128 ft) tall. It is usually used with a mast. With the mast, it has a target detection range of 90 kilometres (56 mi) if altitude of the target is 500 metres (1,600 ft) above the ground.^[source]S-300 missile system · Specifications / Radar; only the objects and conditions stated in this passage

If the battery was employed in an anti-ballistic-missile or anti-cruise-missile role, the 64N6 BIG BIRD E/F-band radar would also be included. It is capable of detecting ballistic missiles up to 1,000 km (620 mi) away, travelling at up to 10,000 km/h (6,200 mph), and cruise missiles up to 300 km (190 mi) away. It also employs electronic-beam steering and performs a scan once every twelve seconds.^[source]S-300 missile system · Specifications / Radar; only the objects and conditions stated in this passage

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 metres (200 ft) at least 20 km (12 mi) away, at an altitude of 100 m (330 ft) at least 30 km (19 mi) away, and at high altitude up to 175 km (109 mi) away. In addition a 64N6 BIG BIRD E/F band target-acquisition radar can be used, which has a maximum detection range of 300 km (190 mi).^[source]S-300 missile system · Specifications / Radar; only the objects and conditions stated in this passage

In 1995, it was the first system to destroy a R-17 Elbrus Scud missile in the air. China is to test the S-300PMU2's effectiveness in destroying targets in real exercises. The planned targets include a UAV (4.6 kilometres (2.9 mi)), a simulated strategic bomber (186 kilometres (116 mi)), tactical missiles (range of the system to the point of interception 34 kilometres (21 mi) and a height of 17.7 kilometres (11.0 mi)), and pinpoint missiles. In April 2005, NATO held a combat exercise in France and Germany called Trial Hammer 05 to practice Suppression of Enemy Air Defenses missions. The Slovak Air Force brought an S-300PMU along, providing an opportunity for NATO to become familiar with the system.^[source]S-300 missile system · Operational history; only the objects and conditions stated in this passage

On 14 April 2023, Sloviansk was hit by seven S-300 missiles, which killed at least 11 people. Russian S-300 strikes in Pokrovsk Raion on 6 January 2024 killed 11 and injured 8 according to local officials.^[source]S-300 missile system · Operational history / Russo-Ukrainian war; only the objects and conditions stated in this passage

Belarus – S-300PS systems delivered from Russia in 2007 to replace older S-300 model in the Belarusian inventory. Four divisions of S-300 missiles to be delivered in 2014.^[source]S-300 missile system · Operators and other versions; only the objects and conditions stated in this passage

China – China first acquired the S-300PMU-1 in 1993, and later became the first customer of the S-300PMU-2, in 2004. China also built the HQ-15 with the maximum range upgraded from 150 to 200 km (93 to 124 mi). The total number of the S-300PMU/1/2 and HQ-15/18 batteries in the PLA are approximately 40 and 60, respectively, as of 2008. The total number of the missiles is well above 1,600, with about 300 launcher platforms. Five such SAM battalions are deployed and in active duty around the Beijing region, six battalions are in the Taiwan strait region, and the rest are in major cities such as Shanghai, Chengdu, and Dalian. Two Rif (SA-N-6) systems were purchased in 2002 for the Chinese Navy's Type 051C destroyers. By 2011, China had obtained 15 battalions (4 systems) of the S-300PMU-2.^[source]S-300 missile system · Operators and other versions; only the objects and conditions stated in this passage

Russia – All variations. (1900 (S-300PT/PS/PMU, 200 S-300V/S-300V1 in 2010)), 2000 total launchers. All production in 1994 (actually 1990) or older, all the S-300PM complexes have been repairing and upgrading (Favorit-S). The S-300P/PT has been retired before 2008, some S-300PS are in service, but were to be retired in 2012–2013. Modernization of all S-300P units to the S-300PM1 version was to end in 2014. The useful life of each was increased by 5 years. PM 1 was upgraded to version PM 2. By 2015, the S-300V4 was to have been delivered. Modernization of all S-300Vs to S-300V4s was to end in 2012.^[source]S-300 missile system · Operators and other versions; only the objects and conditions stated in this passage

Ukraine – S-300PT, S-300PS, S-300PMU, S-300V1. Only six systems were kept in working order between 2004 and 2014; as a result, only 40% of Ukrainian S-300 systems were in good condition prior to 2014. Due to the war with Russia , Ukraine started repairing and bringing back to service several armaments, including several S-300 batteries, with at least 4 batteries overhauled in 2014–15. 34 launchers remained in Crimea after the 2014 Russian annexation of Crimea . Prior to the 2022 Russian invasion of Ukraine , the country had around 100 batteries. It received an additional battery from Slovakia in April 2022.^[source]S-300 missile system · Operators and other versions; only the objects and conditions stated in this passage

Slovakia – One S-300PMU battery and 48 5V55R missiles inherited from Czechoslovakia. 3 missiles were fired during an exercise in Bulgaria in 2015. The battery was donated to Ukraine in April 2022 in response to the 2022 Russian invasion of Ukraine .^[source]S-300 missile system · Operators and other versions / Former operators; only the objects and conditions stated in this passage

Though the S-300 variant was not specified, the stated range of the system was to be 250 kilometres (160 mi).^[source]S-300 missile system · Operators and other versions / Former operators; only the objects and conditions stated in this passage

Taer-2B^[source]

Sayyad-2^[source]

IVECO diesel^[source]

25–30 km^[source]

• Reported operator · Iran