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S-200 Dubna (SA-5 Gammon) Russian Surface-to-Air Missile (SAM) System

SA-5 Gammon

A very long range, medium-to-high altitude surface-to-air missile (SAM) system.
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Basic Information
Name
S-200 Dubna (SA-5 Gammon) Russian Surface-to-Air Missile (SAM) System
Designation
SA-5 Gammon
Alternate Designation
SA-5 Gammon; S-200 Angara (Russian system designation) S-200 Volga (Russian system designation) S-200 Vega (Russian system designation) V-860 (Russian missile designator) 5V28 (Russian missile designator)
Equipment Type
A very long range, medium-to-high altitude surface-to-air missile (SAM) system.
Manufacturer
Date of Introduction
1967
Description

The S-200 Volga (SA-5 Gammon**) is a Russian long-range, high-altitude strategic surface-to-air missile (SAM). It is a fixed-site, point defense SAM that relies on long-range early warning and ground control intercept radars (Big Back, Bar Lock, Tin Shield and Side Net ) for target tracking information and 5N62 series Square Pair** radar for fire control.

Ground Specifications
Active Protection None
NBC Protection Yes
Max Speed 4929.6 km/h
Range 7.0 km
Variants
SA-5a (S-200A Angara) This missile attained initial operating capability in 1962 on the "Tallinn line" with conventional warheads. System includes a V-860/5V21 or V-860P/5V21A missile; range, 88 mi (160 km); and ceiling, 66,000 ft (20 km).
SA-5b (S-200V Vega) This version reached initial operating capability in 1970 with nuclear warhead. Other versions include the S-200 Vega with a V-870 missile and range 186 mi (300 km). Also: S-200M Vega-M with a V-880E/5V28E missile, export version, high-explosive warhead only, with a range of 155 mi (250 km) and, ceiling of 95,000 ft (29 km).
SA-5c (S-200D Dubna) The SA-5c’s initial operating capability was attained in 1975 with a dual-capable (nuclear or conventional) warhead and upgraded terminal homing capability. Characteristics include a 5V25V, V-880M/5V28M or V-880MN/5V28MN2 missile, with a range of 248 mi (400 km) and a ceiling of 125,000 ft (40 km).
SA-5d This designation was briefly used for the SA-X-12 Gladiator missile.
SA-5e This variant attained initial operating capability in 1983 with a passive anti-radiation seeker. It was probably designed to be used against AWACS aircraft
System
Alternative Designation SA-5 Gammon; S-200 Angara (Russian system designation) S-200 Volga (Russian system designation) S-200 Vega (Russian system designation) V-860 (Russian missile designator) 5V28 (Russian missile designator)
Type A very long range, medium-to-high altitude surface-to-air missile (SAM) system.
Family SA-5 Series
In Service 1967-Present
Wars First Libyan Civil War Syrian Civil War
Crew INA
Displacement Time INA
Emplacement Time INA
Fire on the Move No
Guidance System Semi-active radar homing
Dimensions
Missile Length 10.72 m
Wingspan 2.85 m
Mainbody Diamter 0.85 m
Solid Propellant Booster Length 4.9 m
Solid Propellant Booster Width 0.48 m
Note Each Missile has four jettisonable, wraparound solid propellant boosters
Automotive
Engine 4 x solid-fuel boosters; solid-fuel second stage
Speed Mach 4
Maximum Range 7 km
Minimum Range 300 km
Maximum Altitude INA
Minimum Altitude 35 km
Missile System
Missile Launcher
Name INA
Type Rail
Maximum Effective Range 250 km
Minimum Effective Range The missile's minimum range of 60 km is due to the booster burn time and jettison requirements, limiting the system to engagements against relatively large unmaneuverable targets at ranges up to 250 km.
Note Each Missile has four jettisonable, wraparound solid propellant boosters
Missile (Option 1)
Name 5V21
Type HE-Frag
Variant Angara (A)
Length 10.5 m
Diameter 86 mm
Booster Length 4.9 m
Booster Diameter 0.48 m
Effective Range 150-180 km
Maximum Speed Mach 4
Guidance System Semi-active radar homing
Missile (Option 2)
Name 5V28
Type HE-Frag
Variant Vega (V)
Length 10.7 m
Diameter 86 mm
Booster Length 4.9 m
Booster Diameter 0.48 m
Effective Range 200 km
Maximum Speed Mach 4
Guidance System Semi-active radar homing
Missile (Option 3)
Name 5V28
Type HE-Frag, Nuclear
Variant Vega M (VM)
Length 10.7 m
Diameter 86 mm
Booster Length 4.9 m
Booster Diameter 0.48 m
Effective Range 250 km
Maximum Speed Mach 4
Guidance System Semi-active radar homing
Fire Control
Fire Control System
Name INA
Computerized FCS Yes
Direct Fire No, due to booster burn time and jettison requirements
Indirect Fire Yes
Fire Control Sensors Yes
IADS Integration INA
Guidance System Semi-active radar homing
Radar #1
Name P-15M(2)
Type Squat Eye
Function INA
Frequency C-band
Range 128 km
Associated Weapon System SA-3/5
Recognition Power 380kw
Radar #2
Name P-14
Type TALL KING
Function Electronic Warfare
Range 605 km
Frequency A Band
Associated Weapon System SA-5
Recongintion Scan 2-6rpm
Radar #3
Name PRV-11
Type SIDE NET
Function Height
Maximum Range 28 km
Maximum Altitude 32 km
Frequency E-band
Associated Weapon System SA-2/3/5
Recognition INA
Radar #4
Name INA
Type BACK NET
Function EW/GCI
Range 300 km
Frequency E-Band
Associated Weapon System SA-5
Recognition 3-6 rpm Scan
Radar #5
Name P-35/37
Type BAR LOCK
Function EW
Range 200 km
Frequency E/F-bands
Associated Weapon System SA-5
Recognition INA
Protection
Hull Armor INA
Applique Armor No
Explosive Reactive Armor No
Active Protection System No
Mine Clearing No
Self-Entrenching Blade INA
NBC Protection Yes
Smoke Equipment No
Details
Country of Origin Russia
Category Radar Guided Missile Systems
Land > Air Defense > Radar Guided Missile Systems
Filter Label
S
Classification
Domain
Ground
Equipment Status
Active
Dimensions
Length
10.72 m
Width
0.85 m
Height
Weight
Operators (14)
Russia
Ukraine
Poland
India
Iran
North Korea
Algeria
Azerbaijan
Bulgaria
Kazakhstan
Myanmar
Syria
Turkmenistan
Uzbekistan
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