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Pantsir-S1 (SA-22 Greyhound) Russian Short-Range Air Defense Gun/Missile System

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Basic Information
Name
Pantsir-S1 (SA-22 Greyhound) Russian Short-Range Air Defense Gun/Missile System
Designation
Alternate Designation
96K6 Pantsir-S1 (SA-22 Greyhound) Russian Short-Range Air Defense Gun/Missile System Other spellings: Pantsyr, Pantzyr, Pantzir.
Equipment Type
Manufacturer
KBP Instrument Design Bureau
Date of Introduction
2012
Description

The Pantsir-S1 (SA-22 Greyhound) Russian Short-Range Air Defense Gun/Missile System is a self-propelled anti-aircraft gun and missile (SPAAGM) system designed by Russia. The Pantsir air defense system incorporates anti-aircraft guns and missiles to intercept tactical aircraft, precision-guided munitions (PGMs), and unmanned aerial vehicles (UAVs). Although each Pantsir launch vehicle is capable of functioning independently, they typically operate in batteries of six launcher vehicles and are occasionally accompanied by a separate command and control vehicle.

Ground Specifications
Crew 3
Mobility Type Wheeled (8x8)
Main Weapon two twin 30 mm 2A38M cannons
Engine Diesel (400 hp)
NBC Protection Yes
Max Speed 90.0 km/h
Range 1000.0 km
Variants
72V6 The prototype version of the Pantsir system, first displayed at the MAKS defence exhibition in 1994, had an alienate configuration to the production baseline Pantsir-S1 model, mounting two twin 30 mm 2A72 cannons and two six round SAM launchers containing 9M335 missiles, a development of the Tunguska’s 9K311 missile.
72V6-E1 Intermediary developmental version, evolving the 72V6 design toward a production ready version.
72V6-E2 Intermediary developmental version, evolving the 72V6 design toward a production ready version.
Pantsir-S1-O Sporadically referenced since 2005 as a ‘basic’ version of the Pantsir-S1, the Pantsir-S1-O is stated to be a version that forgoes radars, using only the AOP system for tracking and engagement and with an alternate armament that saw the 2A72 cannons from the early 72V6 rather than the standard 2A38M, and only four rather than six missiles mounted on each side of the turret.
Pantsir-S1 Pantsi-S1 is the baseline model of the Pantsir family. The system is a gun/missile VSHORAD air defence system, armed with two twin 30 mm 2A38M cannons and two six round surface to air missile launchers firing the 57E6 missile. The system is typically truck mounted but can be fitted to tracked and containerised mountings if desired.
Pantsir-S Pantsi-S is the baseline domestic model of the Pantsir family. The system is a gun/missile VSHORAD air defence system, armed with two twin 30 mm 2A38M cannons and two six round surface to air missile launchers firing the 57E6 missile. The system is typically truck mounted but can be fitted to tracked and containerized mountings if desired.
Pantsir-M Pantsir-M is a naval version of the Pantsir system, using an alternate armament configuration that changes the 2A39M cannons for two 30 mm GSh-6-30 gatling cannons, adds Hermes-K missiles as well as retaining the land-based system’s 57E6-series missiles.
Pantsir-ME Pantsir-ME is the export version of Pantsir-M, indicated by the standard Russian ‘E’ (Cyrillic ‘Э’) export designator in the name.
Pantsir-SA Pantsir-SA is an arctic oriented version of the Pantsir system, with the truck chassis replaced with the DT-30PM tracked carrier.
Pantsir-S1M An improved version of the S1, the S1M, has been shown in model form at several recent exhibitions by KBP.
Pantsir-SM This is a deeply modernised variant of the Pantsir-S system. It is stated to be the most advanced variant and claimed to improve target detection range from 40 to 75 km as well as engagement from 20 km to 40 km. The ability to detect low RCS targets Is also claimed to be much increased.
System
Alternative Designation 96K6 Pantsir-S1 (SA-22 Greyhound) Russian Short-Range Air Defense Gun/Missile System Other spellings: Pantsyr, Pantzyr, Pantzir.
Primary Components per Battery 6 ea
Manufacturer KBP Design Bureau, Tula, Russia (design) Ulyanovsk Mechanical Plant, Ulyanovsk, Russia (manufacturer)
Targets FW, heli, CM, ASM, UAV, guided bomb
Crew 3 ea
Chassis Kamaz-6560
Reaction Time 5-8 min
Time in Action 3 min
Deployment Time 5 min
Pantsir S-1 Battery Organization
96K6 Pantsir, Mounted on KAMAZ 6530 2-6 ea
2F77M missile transporter/transloader, Mounted on KAMAZ 43101 2-3 ea
9S737M Ranzhir-M Command Post, Mounted on MZKT/Volat truck 1 ea
1R10-1M Repair/Test Station, Mounted on Ural 43203-1012 ea
ITO-APG-M1 Mobile Workshop, Mounted on ZiL-131 1 ea
9V921 Repair/Test station, Mounted on GAZ-66 1 ea
2V110-1 Repair station, Mounted on Ural 43203-1012 1 ea
2F55-1 Missile preparation/assembly, Mounted on Ural 43203-1012 1 ea
Dimensions
Length 10.3 m
Width 2.5 m
Height 3.27 m
Curb Weight 14.85 tons
Maximum Load Weight 20 tons
Automotive
Engine Name KamAZ-740.35-400
Engine Type Diesel
Engine Power 400 hp
Maximum Speed 90 km/h
Range 1,000 km
Gradient 60%
Side Slope 40%
Vertical Step 0.6 m
Trench 2 m
Fording 1.8 m
Main Weapon System
Note Primary armament is a gun/missile armed turret, fitted with two twin 30 mm 2A38M cannons, one on each side of the turret, and two six-round missile launchers, one on each side of the turret, fitted with 57E6/57E6-E/23Ya6 surface to air missiles.
Missile (Option 1)
Name 57E6 Missile
Type Surface to Air Missile
Length 3.20 m
Diameter, 1st Stage 170 mm
Diameter, 2nd Stage 90 mm
Warhead Weight 16 kg
Missile Weight 75 kg
Guidance System Guidance is command guided using radio transponder and laser responder.
Propulsion System Two stage solid fuel propulsion of a bicaliber design, with the booster stage being of a thicker diameter than the unpowered terminal stage.
Seeker No seeker is fitted to keep per round costs at a minimum.
Maximum Range 12,000 m
Minimum Range 1,200 m
Maximum Altitude 15,000 m
Minimum Altitude 15 m
Warhead A contact and radar proximity fuzing system is fitted to the 16 kg HE-fragmentation continuous-rod warhead.
Basic Load 12 x 57E6 Missiles
Missile (Option 2)
Name 57E6-E Missile
Type Surface to Air Missile
Length 3.20 m
Diameter, 1st Stage 170 mm
Diameter, 2nd Stage 90 mm
Warhead Weight 20 kg
Missile Weight 76 kg
Guidance System Guidance is command guided using radio transponder and laser responder.
Propulsion System Two stage solid fuel propulsion of a bicaliber design, with the booster stage being of a thicker diameter than the unpowered terminal stage.
Seeker No seeker is fitted to keep per round costs at a minimum
Maximum Range 12,000 m
Minimum Range 1,200 m
Maximum Altitude 6,000 m
Minimum Altitude 5 m
Basic Load 12 x 57E6-E Missiles
Auxiliary Weapon System
Note Each side of the turret has twin barrel 30 mm 2A38M cannons on an elevating mount.
System
Name 2 x twin 2A38M Cannons
Type Twin Barrel Cannons
Caliber 30 mm
Maximum Range 4,000 m
Minimum Range 200 m
Maximum Altitude 3,000 m
Rate of Fire Each cannon consists of two 30 mm barrels that conduct fire in turns providing rapid firing with the rate of 1,950 to 2,500 rds/min.
Ammunition
Type HE-T or HE-I Ammunition
Caliber 30 mm
Cartridge 30 x 165 mm
Basic Load 1,400 Rounds
Fire Control
FCS Name INA
Computerized FCS Yes
Fire on the Move Yes, the Pantsir-S1 can fire whilst on the move as well as stationary, with the vehicle able to move as part of a convoy whilst in search and engagement operation, providing a mobile SHORAD umbrella.
Radar Systems
Surveillance Radar
Name VNIIRT 2RL80
Type Surveillance Radar
Band S-band
Location Mounted on the top of the turret.
Length 1,776 mm
Width 940 mm
Weight INA
Wavebands UHF and EHF wavebands
Number of Airborne Targets detection and tracking of up to 40 2m2 or larger RCS airborne targets
Maximum Range 36 km
IFF Interrogation Yes
Rate of Scan 15 to 30 rpm
Elevation 0˚ - 60 ˚
Traverse 360 deg
Note When not in use the radar fold forwards so that it is flat on the roof of the operator station
Target Tracking and Missile Guidance Radar
Name Phazotron 1RS2-1
Type Target Tracking and Missile Guidance Radar
Location mounted on the front face of the turret.
Length INA
Width INA
Weight INA
Band X/Ku band
Maximum Range 28 km
Number of Airborne Targets 9 simultaneously, with a velocity of 1,100 m/s
Optical Tracking and Engagement Radar
Name 1TPP1, AOP (Avtonomniy Opticheskiy Post – Autonomous Optical Post)
Type Optical Tracking and Engagement Radar
Location mounted on a small pedestal on the top of the turret, in front of the 2RL80E radar.
Length INA
Width INA
Weight INA
Thermal Imager Sagem MATIS LR longwave thermal imager (designated 1PN80)
Maximum Range, Aircraft 20 km
Maximum Range, Missiles 15 km
Elevation -5˚ to +82˚
Traverse 360˚
Azimuth Coverage ±90˚
Protection
Hull Armor The vehicle and system is unarmoured, barring some light protection to ensure the platform is not affected by debris from firing the weapons.
Applique Armor No
Explosive Reactive Armor No
NBC Protection Yes
Smoke Equipment INA
Details
Country of Origin Russia
Category Land
Land
Filter Label
P
Classification
Domain
Ground
Equipment Status
Active
Dimensions
Length
10.3 m
Width
2.5 m
Height
3.27 m
Weight
20000 kg
Operators (12)
Russia
Iran
Serbia
Algeria
Equatorial Guinea
Ethiopia
Iraq
Jordan
Oman
Syria
United Arab Emirates
Vietnam
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