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T38 Stilet Belarusian Short-Range Air Defense System

T38 Stilet

Short-Range Surface-to-Air Missile System
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Basic Information
Name
T38 Stilet Belarusian Short-Range Air Defense System
Designation
T38 Stilet
Alternate Designation
T38 Stilet
Equipment Type
Short-Range Surface-to-Air Missile System
Manufacturer
Tetraedr
Date of Introduction
2014
Description

The T38 STILET is a short-range air defence missile system (ADMS) designed and built by Tetraedr to provide enhanced combat and performance capabilities to air defence units. The system, which is a modernised version of OSA-1T ADMS, can be deployed to strike all types of aerial platforms moving at low and medium altitudes. It is integrated with radars to acquire and identify targets while on the move and at halt. Up to two missiles are used by the ADMS to engage a target from short halt or from stationary position. It can be lifted by an IL-76-class cargo aircraft and transported by rail. The development of T38 STILET missile system began in 2008. It was later exhibited at the IDEX 2011 (International Defence Exhibition and Conference) in Abu Dhabi as well as at the MILEX 2014 (Exhibition of Armaments and Military Equipment) in Republic of Belarus. The T38 STILET air defence missile system first performed five live firings at the 174 training test range of the Air Force and Air Defense of the Republic of Belarus in October 2010. It did this using the 9М33М3 missiles. During the tests, the weapons successfully destroyed high-velocity, small-sized IVTs-M1 aerial target simulators. A year later, in October 2011, the ADMS successfully engaged two small-sized high-velocity IVTs-M1 aerial target simulators and three angle reflectors. Tetraedr demonstrated combat mission readiness of the T38 STILET missile system with the 9M33M2(3) surface-to-air missiles during integration tactical military exercise conducted by the Ministry of Defence of the Republic of Belarus in February 2014. SHARE TYPE Short-range air defence missile system MANUFACTURER Tetraedr CREW Four NUMBER OF MISSILES CARRIED EightExpand T38 Stilet ADMS The T38 STILET is a short-range air defence missile system (ADMS) designed and built by Tetraedr to provide enhanced combat and performance capabilities to air defence units. The system, which is a modernised version of OSA-1T ADMS, can be deployed to strike all types of aerial platforms moving at low and medium altitudes. It is integrated with radars to acquire and identify targets while on the move and at halt. Up to two missiles are used by the ADMS to engage a target from short halt or from stationary position. It can be lifted by an IL-76-class cargo aircraft and transported by rail. The development of T38 STILET missile system began in 2008. It was later exhibited at the IDEX 2011 (International Defence Exhibition and Conference) in Abu Dhabi as well as at the MILEX 2014 (Exhibition of Armaments and Military Equipment) in Republic of Belarus. Test firings of T38 STILET ADMS S-125-2TM / Pechora-2TM Medium Range Air Defence Missile System S-125-2TM is an upgraded version of S-125 / Pechora air defence missile system (ADMS). The T38 STILET air defence missile system first performed five live firings at the 174 training test range of the Air Force and Air Defense of the Republic of Belarus in October 2010. It did this using the 9М33М3 missiles. During the tests, the weapons successfully destroyed high-velocity, small-sized IVTs-M1 aerial target simulators. A year later, in October 2011, the ADMS successfully engaged two small-sized high-velocity IVTs-M1 aerial target simulators and three angle reflectors. Tetraedr demonstrated combat mission readiness of the T38 STILET missile system with the 9M33M2(3) surface-to-air missiles during integration tactical military exercise conducted by the Ministry of Defence of the Republic of Belarus in February 2014. T38 missile system mounted on T381 CV The T38 STILET missile system is mounted on the T381 Combat Vehicle (CV), which is operated by a crew of four. The highly-mobile vehicle features MZKT-69222T self-propelled wheeled chassis driven by a powerful diesel engine. An electro-optical system is fitted on the vehicle, as is navigation and communication systems, map-positioning, air conditioning and a heating system. It also comes with an automatic launch system and launch device, electric power supply system and functional check and combat crew training equipment. A digital master computer and crew commander’s automated workstation can also be found on-board the CV. The combat vehicle is further fitted with target acquisition radar, target tracking radar, two-channel missile sighting radar and two-channel command-transmit radar. The T38 STILET air defence missile system can carry up to eight T382 surface-to-air guided missiles in the Transportation-and-Launch Container (TLC). The two-stage, bi-calibre and solid-propellant missile features a power unit consisting of a booster and a sustainer. A radio fuse installed in the missile ensures effective destruction of the target by actuating a non-contact explosion of the warhead. Targets flying at a maximum speed of 900m/s, at altitudes varying between 25m and 10km, can be destroyed by the missile system. It can also detect targets within a range of 40km, whilst the maximum slant range of target destruction is 20km. A maximum cross range of 10km can be achieved by the ADMS. The probability of killing the target with one missile is 90%. The system is also capable of detecting targets with minimal radar cross section of 0.03m² and has an emplacement / displacement time of five minutes. The T38 STILET air defence missile system uses the T383 Transportation and Loading Vehicle (TLV) for loading and unloading missiles to/from containers. It also provides transportation for missiles and temporary storage. The T385 maintenance vehicle is utililised to carry out maintenance of the combat vehicle. Other technical support assets of the missile system include T384 alignment vehicle, T386 automated mobile check-up and testing station along with the T387 Ground Equipment Kit (GEK).

Ground Specifications
Crew 4
Mobility Type Wheeled (6x6)
Main Weapon 9M33M2 and 9M33M3 missiles
Engine Diesel (420 hp)
Max Speed 80.0 km/h
Range 12.5 km
Variants
Note There was a variant of the T38 Stilet air defense system co-developed with Ukrainian Luch design bureau. This missile would use a new Belarusian missile, developed by the Tetraedr. However in 2014 this development was suspended due to ongoing military conflict in Ukraine.
System
Alternative Designation T38 Stilet
Type Short-Range Air Defense System
Crew 4 ea
Chassis The T38 uses new MZKT-6922 chassis
Displacement Time 5 minutes
Emplacement Time 5 minutes
Fire on the Move INA
Note Battery of the T38 Stilet comprises of TELAR vehicles, and is supported by 6 KamAZ trucks, that are used as a basis for mobile command center, reloading vehicle, maintenance vehicle and other support vehicles.
Dimensions
Length 9 m
Width 3.3 m
Height 5.1 m
Weight, Combat 30 tons
Automotive
Engine Name YaMZ-7513.10-04
Engine Type Diesel
Engine Power 420 hp
Operational Range 840 km
Speed, Maximum Road 80 km/h
Speed, Average Cross INA
Speed Maximum Swim Not Amphibious
Gradient INA
Side Slope INA
Vertical Step 0.58 m
Trench 0.6 m
Fording Depth INA
Missile System
Name T381 launcher vehicle
Launcher The Stileto TELAR vehicle carries 8 missiles arranged in 2 launcher pods with 4 missiles each.
Missile Types It can fire 9M33M2 and 9M33M3 missiles used by the Osa.
Max Elevation INA
Min Elevation INA
Traverse Range INA
Traverse Left INA
Traverse Right INA
Max Rate of Fire INA
Note The T38 STILET air defence missile system uses the T383 Transportation and Loading Vehicle (TLV) for loading and unloading missiles to/from containers. It also provides transportation for missiles and temporary storage.
Missile
Name 9M33M3 Missile
Type Surface-to-Air Missile
Length 3158 mm
Diameter 209.6 mm
Weight 170 kg
Warhead Frag-HE
Warhead Weight 16 Kg
Detonation Mechanism Contact and proximity
Propellant Solid propellant rocket motor
Operational Range 12.5 - 20 km
Flight Altitude 12,000 metres
Boost Time 2 s boost, then 15 s sustain
Speed 1020 m/s
Guidance System Command to Line-Of-Sight (CLOS)
Steering System dual-thrust rocket motor.
Accuracy 5 m
Fire Control
Fire Control System
Name INA
Computerized FCS Yes
Direct Fire Yes
Indirect Fire Yes
Fire Control Sensors INA
Probability of Kill 90%
Note he system is also capable of detecting targets with minimal radar cross section of 0.03m² and has an emplacement / displacement time of five minutes.
Radar
Note The combat vehicle is further fitted with target acquisition radar, target tracking radar, two-channel missile sighting radar and two-channel command-transmit radar.
Protection
Hull Armor INA
Turret Armor INA
Applique Armor No
Explosive Reactive Armor No
Active Protection System INA
Mine Clearing No
NBC Protection INA
Smoke Equipment INA
Details
Country of Origin Belarus
Category Short-Range Missile Systems (Less than 30 km)
Land > Air Defense > Short-Range Missile Systems (Less than 30 km)
Filter Label
T
Classification
Domain
Ground
Equipment Status
Active
Dimensions
Length
9 m
Width
3.3 m
Height
5.1 m
Weight
30000 kg
Operators (3)
China
Belarus
Azerbaijan
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