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SA-20C (S-300PMU-2) Iranian-Long Range Air Defense Missile System

SA-20C

Long-Range Air Defense Missile System
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Basic Information
Name
SA-20C (S-300PMU-2) Iranian-Long Range Air Defense Missile System
Designation
SA-20C
Alternate Designation
SA-20C; S-300PMU-2
Equipment Type
Long-Range Air Defense Missile System
Manufacturer
MZiK
Date of Introduction
1997
Description

The SA-20C is an exported version of the S-300PMU-2 The S-300PMU-2 or SA-20B Favorit air defense missile system was developed especially for export. It evolved from the S-300PM-2, which was developed for the Russian Armed Forces. The S-300PMU-2 has the highest capabilities in the S-300P family. It was introduced in 1997. As of 2016, this system is 19 years old. The S-300PMU-2 is referred in the West as SA-20B Gargoyle. It uses a 30N6E1 (Tomb Stone) radar. This radar has a range of 300 km, can detect 100 targets, track and engage 36 of them and guide 72 missiles. It is worth noting that earlier radars of the S-300 family could simultaneously engage only 6 targets and guide 12 missiles. The S-300PMU-2 Favourite (DoD designation SA-20B), introduced in 1997 (presented ready 1996), 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 of not just short-range ballistic missiles, but now 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. A version titled HQ-15 is currently in Chinese service.

Ground Specifications
Mobility Type Wheeled (8x8)
Main Weapon 4 x 48N6E2 Surface-to-Air Missiles
Active Protection None
NBC Protection Yes
Max Speed 65.0 km/h
Range 200.0 km
Variants
S-300PMU2 Favorit/SA-20B This is an upgraded variant with larger 9M96E and 9M96E2 missiles developed for the S-400. It can also fire the previous 5V55K, 5V55R, 48N6E, and 48N6E2 missiles. It is equipped with an improved guidance system. Unveiled in 1997, the system has an increased range of 124 mi (200 km). The 48N6E2 missile features a warhead designed to destroy ballistic missiles.
System
Alternative Designation SA-20C; S-300PMU-2
Type Long-Range Air Defense Missile System
Manufacturer MZiK
Family S-300 Family
Chassis MAZ-543 Special Wheeled Chassis
In Service 1997-Present
Crew INA
Displacement Time Less than 5 Minutes
Emplacement Time Less than 5 Minutes
Reload Vehicle 5T58 reload vehicle
Maximum Range of Fire 165 km
Maximum Altitude 27 km
Number of Targets Engaged Simultaneously 6 ea
Note #1 Capable of hitting ballistic and aerodynamic targets. Became the first multi-channel anti-aircraft missile system, is able to accompany each system (ADMS) to 6 goals and build them up to 12 missiles.
Note #2 A typical SA-20 battery consists of 48 missiles on 12 mobile launchers. Each battery can launch a 48N6 missile every three seconds.
Dimensions (MAZ-543 Special Wheeled Chassis)
Length 11.7 m
Width 3.07 m
Height 2.92 m
Maximum Load 15 tons
Ground Pressure INA
Automotive (MAZ-543 Special Wheeled Chassis)
Engine Name D12A-525 38.9-liter Diesel
Engine Type Diesel
Engine Power 525 hp
Cruising Range 650 km
Speed, Maximum Road 65 km/h
Speed, Average Cross INA
Speed Maximum Swim Not Amphibious
Configuration 8x8
Gradient 60 %
Side Slope 40 %
Vertical Step 0.6 m
Trench 2 m
Fording Depth 1.3 m
Communications
Note See Fire Control.
Missile System
Note #1 The S-300 family missiles have four clipped folding triangular moving control fins at the rear and four thrust vector control vanes in the motor efflux.
Note #2 Missiles are vertically launched by a hot gas cartridge in the canister base. The motor ignites once the missile reaches an altitude of 25 m.
Missile Launcher
Name 4 x 5P85S or 5P85D launchers
Type Tube Launcher
Anti-Ballistic Missile (ABM) Capability Yes
Note The missiles can be fired in a salvo with an interval between 3 and 5 seconds.
Missile (Option 1)
Name 4 x 48N6E2 Surface-to-Air Missiles
Type Surface-to-Air Missiles
Length 7.5 m
Width 0.5 m
Weight 1,780 kg
Warhead Weight 70-100 kg
Maximum Range 200 km
Engine Type Single-stage, solid-fuel-propelled
Guidance System Track-via-missile
TVM Guidance Capable Yes
ABM Capable Yes
Maximum Velocity 2,000 m/s
Speed Mach 6
Kill Probability 0.70 to 0.93 single shot
Ballistic Targets Range 5-40 km
Maximum Altitude 28 km
Minimum Altitude 10 m
Basic Load 4 x 48N6E2 Surface-to-Air Missiles per TEL
Note The 48N6E2 can engage targets with a maximum speed of Mach 8.
Missile (Option 2)
Name 4 x 5V55R/5V55KD Surface-to-Air Missiles
Type Surface-to-Air Missiles
Length 7 m
Diameter 450 mm
Weight 1,450 kg
Engine Single-stage, solid-fuel-propelled
Guidance System SARH
Warhead Weight 100 kg
Maximum Range 90 km
Maximum Velocity 1,900 m/s
Maximum Target Speed 1,150 m/s
Basic Load 4 x 5V55R/5V55KD Surface-to-Air Missiles per TEL
Missile (Option 3)
Name 4 x 9M96E1 Surface-to-Air Missiles
Type Surface-to-Air Missiles
Length INA
Width INA
Weight 330 kg
Warhead Weight 24 kg
Engine Single-stage, solid-fuel-propelled
Guidance System Active radar homing
Maximum Range 40 km
Maximum Velocity 900 m/s
Maximum Target Speed 4,800–5,000 m/s
Probability of Kill 0.7 against a tactical ballistic missile
Basic Load 4 x 9M96E1 Surface-to-Air Missiles per TEL
Missile (Option 4)
Name 4 x 9M96E2 Surface-to-Air Missiles
Type Surface-to-Air Missiles
Width INA
Weight 420 kg
Warhead Weight 24 kg
Engine Single-stage, solid-fuel-propelled
Guidance System Active radar homing
Maximum Range 120 km
Maximum Velocity 1,000 m/s
Maximum Target Speed 4,800–5,000 m/s
Probability of Kill 0.7 against a tactical ballistic missile
Basic Load 4 x 9M96E2 Surface-to-Air Missiles
Fire Control
Command Post Vehicle 1 x 54K6E2 Command Post Vehicle.
Fire Control System
Name 1 x 83M6E2 Command and Control System
Computerized FCS Yes
Direct Fire Yes, no less than 1km
Indirect Fire Yes
Fire Control Sensors Yes
IADS Integration INA
Number of Targets Engaged Simultaneously 6 ea
GPS/GLONASS Enabled Yes
Loran-C Capable Yes
Fiber-optic Gyros Yes
Note #1 The vehicle lowers four hydraulic jacks for launch.
Note #2 The S-300PMU2 air defense missile system can simultaneously engage up to 36 air targets by 72 missiles.
Radar #1
Name 1 x 64N6 (NATO:BIG BIRD) Surveillance and Target Acquisition Radar
Type Surveillance and Target Acquisition Radar
Frequency/Band 3D S-band radar
Target Detection Range 600 km
Simultaneously Detected Targets +300 targets
Note #1 It has 3 400 elements on each side (a total of 7 800), which is a great number for a radar in this band.
Note #2 Regiment Radar
Radar #2
Name 1 x 30N6E2 (NATO: Tomb Stone) Illumination and Guidance Radar
Type Illumination and Guidance Radar
Mission primarily designed to be used as an engagement radar and to track targets and guide missiles to impact using a command link channel
NATO Reporting Name FLAP LID B
NATO Frequency Band I-J
Target Detection Range 300 km
Azimuth Detection 360 deg
Number of Tragets Detection 100 ea
Simultaneously Engaged Targets 6 ea
Maximum Target Speed 30 - 2,800 m/s
Antenna Antenna RPN 30N6E2 may rise to a special mobile tower 40V6M.
Chassis The 30N6E2 Tomb stone radar is mounted on the high mobility truck chassis 8x8 MAZ-7910 vehicle derived from the MAZ-543.
Missile Control 72 km
Time Ready to Work 5 min
Maximum Elevation +60 deg
Minimum Elevation -3 deg
Radar #3
Name 1 x 96L6E (NATO: CHEESE BOARD 3D early-warning and acquisition radar.
Type 3D early-warning and acquisition radar
NATO Reporting Name CHEESE BOARD
Introduction Date 1997
NATO Frequency Band INA
Target Detection Range 300 km
Simultaneously Tracked Targets 100 ea
Works in Conjunction with The 83M6E2 control post and S-300MPU2 launchers.
Chassis MAZ-7930 (8x8) truck chassis and is intended for use with the S-300PMU and S-300PMU1 air defence systems as an upgrade to replace several existing radar's with a single more capable system.
Band C-Band
Crew Three operators are needed to run the set. Up to five operator consoles are provided.
Antenna The phased-array antenna with 96 radiating rows employs mechanical beam steering in azimuth and electronic beam steering in elevation.
Antenna Rotation 5-10 rpm
Mean Time Betweeen Critical Failure 10,000 hours
High Jam Resistance Yes
Frequency Hoppying Yes
High Clutter Rejection Yes
Operation Modes There are two operation modes implemented: Low altitude targets can be acquired by constraining the mainlobe elevation angle between -3° and +1.5° using an antenna rotation of 5 rpm.
Note The 96L6E “Cheese Board” is designed to replace the 36D6 “Tin Shield B” and 76N6 “Clam Shell”.
Protection
Hull Armor INA
Turret Armor INA
Applique Armor INA
Explosive Reactive Armor No
Active Protection System No
Mine Clearing No
Self-Entrenching Blade No
NBC Protection Yes
Smoke Equipment INA
Camouflage Nets Yes, Standard
Note Protection. Additional elements of protection are the placement of components of C-300 in the trenches (practiced as placing on the hills for a better view and more rapid care of the horizon, and in the trenches for stealth and protection against fragments of explosions).
Details
Country of Origin Iran
Category Radar Guided Missile Systems
Land > Air Defense > Radar Guided Missile Systems
Filter Label
S
Classification
Domain
Ground
Equipment Status
Active
Dimensions
Length
11.7 m
Width
3.07 m
Height
2.92 m
Weight
Operators (2)
China
Iran
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