roketsan product catalogthe laser seeker may be equipped with a proximity sensor. the teber tail...

PRODUCTCATALOG

ROKE

TSAN

PRO

DUCT

CAT

ALOG

ENG

2019 ENG-v2

Kemalpaşa Mahallesi Şehit Yüzbaşı Adem Kutlu Sokak No:21 06780 Elmadağ, ANKARA / TURKEYPhone : + 90 (312) 860 55 00Fax : + 90 (312) 863 42 08e-mail : [email protected] : www.roketsan.com.tr

ROKETSAN A.S. is an affiliated company of Turkish Armed Forces Foundation.

www.roketsan.com.tr

PRODUCT CATALOG

INDEXCİRİT 2.75” LASER GUIDED MISSILE 4

YATAĞAN® LASER GUIDED MINIATURE MISSILE SYSTEM 8

CİDA MISSILE 10

KARAOK MAN PORTABLE SHORT RANGE FİRE-AND-FORGET ANTİ-TANK GUIDED MISSILE 12

UMTAS LONG RANGE ANTI-TANK MISSILE SYSTEM 14

L-UMTAS LASER GUIDED LONG RANGE ANTI-TANK MISSILE SYSTEM 18

OMTAS MEDIUM RANGE ANTI-TANK WEAPON SYSTEM 22

TANOK 120 MM LASER GUIDED MISSILE 26

MAM-L SMART MICRO MUNITION 28

MAM-C SMART MICRO MUNITION 30

TEBER LASER GUIDANCE KIT 32

SOM STAND-OFF MISSILE 34

SOM-J JSF-COMPATIBLE STAND-OFF MISSILE 36

ATMACA ANTI-SHIP MISSILE 38

HİSAR AIR DEFENCE MISSILES 40

ARTILLERY ROCKETS 42

TRG-122 GUIDED ROCKET 44

TRG-230 MISSILE 46

TRGK-300 GUIDANCE KIT 48

TRG-300 TIGER MISSILE 50

T-107/122 MULTI-PURPOSE and MULTI BARREL ROCKET LAUNCHER (MBRL) SYSTEM 52

T-122 MULTI BARREL ROCKET LAUNCHER (MBRL) SYSTEM 56

MCL (MULTI-CALIBER LAUNCHER) WEAPON SYSTEM 58

KHAN MISSILE 62

ALKA DIRECTED ENERGY WEAPON SYSTEM 64

ASW ANTI-SUBMARINE WARFARE ROCKETAND LAUNCHER SYSTEM 68

BALLISTIC PROTECTION SYSTEMS 70

BASE BLEED UNIT 76

NAVIGATION SYSTEMS 78

PYROTECHNIC SYSTEMS 96

FUZE SYSTEMS 102


CİRİT 2.75”LASERGUIDED MISSILE

5

CİRİT 2.75” LASER GUIDED MISSILE

The 2.75” Laser Guided Missile CİRİT is a highly accurate and cost-effective solution for armed helicopters, optimized for use against stationary or moving lightly armored/unarmored targets. CİRİT has been designed to fill the tactical gap between 2.75” unguided rockets and anti-tank missiles.

CİRİT is stored in a canister to ease loading to the launcher and is fired from a “Smart Launcher”. The launcher is compatible with MIL-STD-8591, MIL-STD-1553 and MIL-STD-1760 interfaces.


*Multi-Purpose Warhead: Anti Armor, Anti-Personnel and Incendiary

* IMU: Inertial Measurement Unit

* MEMS: Micro Electro Mechanical Systems

* SAL: Semi-Active Laser Seeker

Technical Specifications

Diameter 2.75” (70 mm)

Length 1.9 m

Weight 15 kg (without Canister)

Range 1.5 - 8 km

Warhead Types Multi-Purpose Warhead*

High Explosive Warhead

Seeker Mid-course Guidance with MEMS-IMU*

Terminal Guidance with SAL*

Propulsion Min. Smoke Composite Solid Propellant

Target Types Light Armored/Unarmored Vehicles, Infantry Laser Designation

Laser Designators Compatible with STANAG 3733

6

Platforms

CİRİT’s versatile design permits easy integration with different platforms. It has already proven its capabilities in both air-to-surface and surface-to-surface engagement scenarios.

Its Smart Launcher allows for platform and target information to be transferred automatically to the missile prior to firing to enhance the performance envelope. Communication through the Smart Launcher MIL-STD-1760 Interface enables transfer of alignment, utilizing the position and status of the platform, environmental conditions, target coordinates and position of the target.

CİRİT can be integrated into various platforms such as helicopters, UAVs, land vehicles, fixed/towed land platforms, close air-support aircrafts, naval platforms, including coastguard vessels and fast patrol boats. Target designation can be carried out from the firing platform or from any other designator.

7

T-129 ATAK Attack H/C

AH-1W Cobra Attack H/C

Light Attack H/C

UH-60 Utility & Combat H/C

AT-802 Border Patrol Aircraft

HÜRKUŞ-C Light Attack A/C

ANKA-S

BAYRAKTAR TB2

Aerial Platforms

Corvettes

Fast Patrol Boats

Naval PlatformsWheeled/Tracked Armored Vehicle

Stationary Ground Based Launcher

Mobile/Towed Ground Based Launcher

Land Platforms


8

YATAĞAN®

LASER GUIDEDMINIATURE MISSILE

SYSTEM


9

YATAĞAN® Laser Guided Miniature Missile System can be fired using new generation man portable 40 mm grenade launcher and has a greater effective range than the maximum range of existing grenade launcher ammunition. Lightweight and small size missile enables integration of the system with mini unmanned aerial vehicles, ground and surface vehicles.

It brings precision, range and target oriented fire power to urban warfare.

YATAĞAN®

LASER GUIDEDMINIATURE MISSILESYSTEM

YATAĞAN® LASER GUIDEDMINIATURE MISSILE SYSTEM


Diameter 40 mm

Length ~40 cm

Weight ~1 kg

Maximum Range ~1,000 m

Seeker SAL*

Accuracy (CEP) 1 m

Platforms Grenade Launchers

Mini Unmanned Aerial Vehicles

Unmanned Ground Vehicles

Unmanned Surface Vehicles

*SAL: Semi-Active Laser Seeker

9

10

CİDA MISSILE


11

CİDA MISSILE

CİDA Weapon System, which can be classified as a weapon that stands between the advanced guided missiles and unguided rockets, has been designed taking into account the topographic uncertainties of the combat area and the rapid movement of threats during urban operations. It is a lightweight and cost-effective missile that can be guided to its target accurately while ensuring less collateral damage.

CİDA MISSILE


Diameter 90 mm

Length 1 m

Weight 7.5 kg

Range 50 - 750 m

Seeker Command to Line-of-Sight (CLOS)

SAL*

Warhead Types Thermobaric

Multi-Purpose Warhead*

High-Explosive Blast Fragmentation

*SAL: Semi-Active Laser

*Multi-Purpose Warhead: Blast Fragmentation, Incendiary and Armor Piercing

12ROKETSAN A.S. is an affiliated company of Turkish Armed Forces Foundation.

KARAOK MAN PORTABLE SHORT RANGE FİRE-AND

FORGET ANTİ-TANK GUIDED MISSILE

1313

Man Portable Short Range Fire-and-Forget Anti-Tank Guided Missile KARAOK is a portable system that is effective day or night with its Imaging Infrared Seeker.

KARAOK can effectively be used to stop, delay, canalize and neutralize enemy armored and mechanized units at short range during air assault, airborne and amphibious operations.

KARAOKMAN PORTABLE SHORT RANGE FİRE-AND-FORGET ANTİ-TANK GUIDED MISSILE

Missile Technical Specifications

Diameter 125 mm

Weight <16 kg (Missile + Launching Tube)

Range 1,000+ m

Warhead Type Armor Piercing Tandem

Attack Mode Direct/Top Attacks

Operating Mode Fire-and-Forget

KARAOK MAN PORTABLE SHORT RANGE FİRE-AND-FORGET ANTİ-TANK GUIDED MISSILE

14

UMTAS LONG RANGE ANTI-TANK MISSILE SYSTEM


15

Long range UMTAS is a anti-tank precision-guided missile system that has been developed for use primarily on attack helicopters.

The missile’s Imaging Infrared Seeker permits its use at day or night, and in adverse weather conditions, and its RF data link provides it with flexible operational capabilities. The missile can be used in fire-and-forget or fire-and-update mode with lock-on before launch or lock-on after launch capabilities. The hitting point on the target can also be updated during flight.

Its precision guidance and control capability, together with its tandem anti-armor warhead, make UMTAS an effective weapon system against armored targets.

UMTAS LONG RANGEANTI-TANK MISSILESYSTEM



Diameter 160 mm

Length 1.8 m

Weight 37.5 kg

Range 500 – 8,000 m

Seeker IIR*

Warhead Types Tandem Against Reactive Armor

High Explosive Blast Fragmentation

Attack Modes Direct/Top Attacks

Operating Modes Fire-and-Forget Fire-and-Update

Launcher

Missile Capacity 4

Weight 60 kg

Standard Interface MIL-STD-1760

*IIR: Imaging Infrared Seeker

16

System Specifications• Day-Night and All-Weather Operational

Capability

• Effective Against Stationary and Moving Targets

• Capability of Target Update Enables:

- Update of Aim Point on the Target

- Switching Targets During Flight

- Fire Behind Mask

• Insensitive Munition Characteristics Against Fuel Fire and Bullet Impact

17

Platforms

• T129 ATAK Attack H/C

• S70-B SEAHAWK H/C

• HÜRKUŞ-C Light Attack A/C

• Platforms that have MIL-STD-1760 and MIL-STD-1553 Interfaces

UMTAS can be integrated onto naval platforms with stabilized weapon systems, as well as armored vehicles and fixed/towed land platforms.


18

L-UMTAS LASER GUIDED LONG RANGE ANTI-TANK

MISSILE SYSTEM


19

L-UMTAS LASER GUIDED LONG RANGE ANTI-TANK MISSILE SYSTEM


Diameter 160 mm

Length 1.8 m

Weight 37.5 kg

Range 500 – 8,000 m

Seeker SAL*

Warhead Types Tandem Effective Against Reactive Armor

High Explosive Blast FragmentationLauncher

Missile Capacity 4

Weight 60 kg

Standard Interface MIL-STD-1760

L-UMTAS is a long range laser guided anti-tank precision missile system developed primarily for attack helicopter platforms. The laser guidance and tandem armor-piercing warhead features of L-UMTAS ensure its effectivity against both stationary and moving targets. The missile can lock onto the target before launch.



20

System Specifications

• Day-Night Operational Capability

• Lock-On Before Launch (LOBL) or Lock-On After Launch (LOAL)

• Fire Behind Mask



21

Platforms

• T129 ATAK Attack H/C

• S70-B SEAHAWK H/C

• HÜRKUŞ-C Light Attack A/C

• Platforms That Have MIL-STD-1760 and MIL-STD-1553 Interfaces


22

OMTAS MEDIUM RANGE ANTI-TANK WEAPON

SYSTEM


23

OMTAS is a medium range anti-tank weapon system, effective against armored threats on the battlefield. Its Imaging Infrared Seeker permits its use at day and night, and in adverse weather conditions. The OMTAS Weapon System is composed of a missile, launching platform and a fire control unit, carrying cases and training simulator.

The RF data link between the launcher and missile provides operational flexibility to the user. The missile can be used in fire-and-forget or fire-and-update mode. The hitting point on the target can also be updated during flight.

With precision guidance and its armor piercing tandem warhead, OMTAS ensures effectivity against armored threats.

OMTAS MEDIUM RANGE ANTI-TANK WEAPON SYSTEM


* IIR: Imaging Infrared Seeker


Diameter 160 mm

Length 1.8 m

Weight 35 kg (Missile + Launch Tube)

36 kg (Tripod Platform)

Range 200 – 4,000 m

Seeker IIR*, Uncooled Type

Warhead Type Tandem Against Reactive Armor

High Explosive Blast Fragmentation

Attack Modes Direct /Top Attacks

Operating Modes Fire-and-Forget

Fire-and-Update

Sight Unit TV/Thermal Camera

24

System Specifications• Day-Night and All-Weather Operational

Capabilities


• Capability of Target Update Enables:

- Update of Aim Point on the Target

- Switching Targets During Flight

- Fire Behind Mask


• Fire to the Target Coordinate

• Classroom and Embedded Simulators

• Modular Launching System

• TV/Thermal Camera Unit That Can Be Used Separately

25

Platforms

OMTAS can be used from its own tripod or integrated onto land platforms with open or closed turrets.


26

TANOK 120 MM LASER GUIDED MISSILE


27

TANOK 120 mm Laser Guided Missile has been developed as an innovative alternative to conventional munitions used in tanks and other artillery guns to have accurate, cost-effective fire power.

TANOK Missile is fulfilling the Armed Forces’ needs to have laser guided anti-tank artillery ammunition. The missile can be fired from land and portable platforms with low weight and soft launch motor.

TANOK 120 MM LASERGUIDED MISSILE

System Specifications• Use in Existing Tanks without any

Modification

• High Hit Probability Against Stationary and Moving Targets with Its Semi-Active Laser Guidance

• Direct/Top Attack Modes

• Effectiveness Against Heavy Armored Threats and Bunkers with Its Tandem Warhead

TANOK 120 MM LASER GUIDED MISSILE


Diameter 120 mm

Length 984 mm

Weight 11 kg

Range 1 - 6 km

Seeker SAL*

Warhead Type Armor Piercing Tandem

Targets Heavy and Lightly Armored Vehicles

Platforms Tank, Land Vehicles


28

MAM-LSMART MICRO MUNITION


Smart Micro Munition MAM-L has been developed for unmanned aerial vehicles (UAV), light attack aircrafts and air-ground missions for low payload capacity air platforms. MAM-L can engage both stationary and moving targets with high precision.

MAM-LSMART MICRO MUNITION

29

*INS: Inertial Navigation System *GPS: Global Positioning System *SAL: Semi-Active Laser


Diameter 160 mm

Length 1 m

Weight 22 kg

Range 8 km (14 km with INS/GPS* Option)

Seeker SAL*

Warhead Types Tandem Effective Against Reactive Armor


Thermobaric

Fuze Impact

Proximity

Platforms UAVs

Light Attack A/C

MAM-L SMART MICRO MUNITION

30

MAM-CSMART MICRO MUNITION


Smart Micro Munition MAM-C has been developed for unmanned aerial vehicles (UAV), light attack aircrafts and air-ground missions for low payload capacity air platforms. MAM-C can engage both stationary and moving targets with high precision.

MAM-CSMART MICRO MUNITION

31

MAM-C SMART MICRO MUNITION


Diameter 2.75” (70 mm)

Length 970 mm

Weight 6.5 kg

Range 8 km

Seeker SAL*

Warhead Types Multi-Purpose Warhead*


Platforms UAVs

Light Attack A/C

*Multi-Purpose Warhead: Blast Fragmentation, Incendiary and Armor Piercing *SAL: Semi-Active Laser

32

TEBERLASER GUIDANCE KIT


TEBER is a laser guidance kit for use on MK-81 and MK-82 general purpose bombs. TEBER converts these bombs into precision smart weapons using Inertial Navigation System (INS), Global Positioning System (GPS) and Semi-Active Laser (SAL) Seeker.

An add-on SAL Seeker, mounted on the front section, provides a precise hit capability against moving targets. The Laser Seeker may be equipped with a proximity sensor.

The TEBER tail section is composed of GPS and INS for precise guidance and can be integrated onto the bomb by user in the field. The tail section can also automatically identify the types of the bombs (MK-81/MK-82).

TEBERLASER GUIDANCE KIT

33

TEBER LASER GUIDANCE KIT


Length 2.1 m (TEBER-81) 2.6 m (TEBER-82)

Weight ~155 kg (TEBER-81) ~270 kg (TEBER-82)

Range 2 - 28 km

Guidance Modes INS* only INS + GPS* INS + GPS + SAL* INS + SAL*

Warhead Types MK-81 MK-82

Seeker SAL

Proximity Sensor 2-15 m

Accuracy (CEP) <3 m

Maneuverability ± 3 g

Moving Target <50 km/sec Engagement

*INS: Inertial Navigation System *GPS: Global Positioning System *SAL: Semi-Active Laser

34

SOMSTAND-OFF MISSILE


35

Stand-Off Missile SOM is an air-to-surface cruise missile fired from beyond the reach of the hostile air defence systems, against heavily defended land or moving naval targets, deep in the battlefield.

SOM (SOM-A / SOM-B1 / SOM-B2)

STAND-OFF MISSILE

*INS: Inertial Navigation System

*GPS: Global Positioning System

*TRN: Terrain Relative Navigation

*IBN: Image-Based Navigation

*ATA: Automatic Target Acquisition


SOM STAND-OFF MISSILE

System Specifications• Low Radar Signature

• Survivable

• Turbojet Engine

• Resistance to Countermeasures/Clutter

• Target of Opportunity Capability

• Selectable Impact Parameters

Length

Weight

Guidance

Range

Warhead Types

Warhead Weight

Seeker

Platforms

~4 m

~600 kg

INS/GPS/TRN*

250+ km

High Explosive Blast/Fragmentation

~230 kg

-

F-4

F-16

~4 m

~600 kg

INS/GPS/TRN/IBN/ATA*

250+ km

High Explosive Blast/Fragmentation

~230 kg

IIR*

F-4

F-16

~4 m

~650 kg

INS/GPS/TRN/IBN/ATA*

250+ km

Tandem Penetrator

~230 kg

IIR*

F-4

F-16

SOM-A SOM-B1 SOM-B2


36

SOM-J JSF-COMPATIBLE STAND-OFF MISSILE


37

SOM-J is an air-to-surface missile designed to use against heavily defended, high-value maritime and land targets. The missile’s modular design supports necessary operational flexibility.

SOM-J provides enhanced capabilities by building on existing SOM air-to-surface cruise missile technologies already in service with the Turkish Air Force.

SOM-J complements other long range weapon systems and provides an affordable solution to maximize stealth and stand-off across the battlespace.


System Specifications• Low Radar Cross Section

• Survivable

• High Precision Terminal Guidance with IIR Seeker and Data Link

• Resistance to Countermeasures/Clutter

• Network Enabled Weapon (NEW) Capability

• Target of Opportunity Capability

• Selectable Impact Parameters

• In-Flight Retargeting

• Universal Armament Interface (UAI) Compatibility



*TRN: Terrain Relative Navigation

*IBN: Image Based Navigation

*ATA: Automatic Target Acquisition




Length ~3,9 m

Weight ~540 kg

Range 150+ nm

Guidance INS/GPS/TRN/ IBN/ATA*

Warhead Type Fragmentation Armor Piercing

Warhead Weight ~140 kg

Seeker IIR*

Platforms F-35 (JSF) F-16

Speed High Subsonic

38

ATMACAANTI-SHIP MISSILE


39

ATMACA is a high precision, long range, surface-to-surface, precision strike anti-ship missile which can be integrated to patrol boats, frigates and corvettes.

ATMACA ANTI-SHIP MISSILE

System Specifications• Autonomous

• Low Radar Signature

• High Precision

• All Weather Operational Capability

• Resistant to Countermeasures

• Target Update, Re-Attack, Re-Target and Mission Abort Capability via Data Link

• 3D Mission Planning

• Super Sea Skimming

• Anti-Surface Warfare (ASuW)



ATMACA ANTI-SHIP MISSILE


Length 4,800 - 5,200 mm

Weight < 800 kg

Range >200 km

Guidance INS + GPS* + Barometric Altimeter + Radar Altimeter

Warhead Type High Explosive with Penetration

Warhead Weight 250 kg

Seeker Active RF

40

HİSARAIR DEFENCE

MISSILES


The HİSAR Air Defense Missiles are operationally used for the protection of military bases, ports, facilities and troops against rotary and fixed wing aircrafts, cruise missiles, air-to-ground missiles and unmanned aerial vehicles (UAV). HİSAR-A and HİSAR-O have a modular structure as part of their family concept, and are designed to be compatible with different platforms, fire control and command control infrastructures.

HİSAR AIR DEFENCE MISSILES

Intercept Range 15 km 25 km

Warhead Types

Seeker

Engine

Types of Targets

High Explosive Fragmentation

Dual Pulse Solid Propellant

Midcourse Guidance with INS* and Data LinkTerminal Guidance with IIR*

Fixed-Wing AircraftsRotary-Wing Aircrafts

Cruise MissilesUAV

Air-to-Ground Missiles

HİSAR-A (Low Altitude)

HİSAR-O(Medium Altitude)

41


HİSAR AIR DEFENCE MISSILES



System Specifications• Vertical Launch Capability with 360°

Effectiveness

• Dual-Stage Rocket Motor

• Multiplatform Integration Interface

• Thrust Vector Control System

• Impact and Proximity Fuze

• Common Canister and Umbilical Connection Interface for HİSAR-A and HİSAR-O

42

ARTILLERYROCKETS


43

ROKETSAN Artillery Rockets provide mass firepower to maneuvering forces with minimum dispersion and maximum warhead effectiveness on targets between 3 - 40 km ranges.

ARTILLERY ROCKETS

ARTILLERY ROCKETS

*HE: High Explosive *PD: Point Detonating

Diameter

Weight

Minimum Range

Maximum Range

Propellant Type Warhead Types

Warhead Weight

Warhead Effective Radius

Fuze Type

107 mm20 kg3 km (at Sea Level) 11+ km (at Sea Level)

Reduced Smoke Composite Solid

HE* + Fragmentation

8.4 kg ≥ 14 m PD*

122 mm66 kg16 km (at Sea Level)21 km (at 600 m above Sea Level)10 km (with Drag Ring)36 km (at Sea Level) 40 km (at 600 m above Sea Level)Composite Solid HE* + Fragmentation

18.4 kg ≥ 20 m PD*

122 mm66 kg16 km (at Sea Level)21 km (at 600 m above Sea Level)10 km (with Drag Ring)36 km (at Sea Level) 40 km (at 600 m above Sea Level)Composite Solid HE* + Steel Ball

18 kg ≥ 40 m PD* and Proximity

TR-107 TR-122 TRB-122


Sealed Pod

107 mm and 122 mm Rocket Pod is designed for long term storage. Sealed Pod contains 20 x ready to fire rockets/guided rocket.

It provides advantages such as:• Protection Against Adverse Weather and

Environmental Conditions• Extended Shelf Life• Easy Transportation, Fast and Easy Loading

and Unloading• Quick Reaction Time• Maintenance Free• Built-In Test Capability

44

TRG-122GUIDED ROCKET


45

TRG-122 Guided Rocket provides accurate and effective fire power on high priority targets within the ranges 16 - 35 km.

Potential Targets• Targets Located with High Accuracy

• Artillery and Air Defence Systems

• Radar Sites

• Assembly Areas

• Logistic Facilities

• C3 Facilities

• Other High Priority Targets

System Specifications• 7/24 All Weather/Terrain Usage Capability

• Ready to Fire

• Highly Accurate

• Low Collateral Damage

• Precision Strike Capability

• Anti-Jamming/Anti-Spoofing Solutions

TRG-122 GUIDED ROCKET


*GLONASS: Global Navigation Satellite System

*HE: High Explosive

*PD: Point Detonating

TRG-122 GUIDED ROCKET


Diameter 122 mm

Weight 76 kg

Range 16 - 35 km

Guidance GPS* + GLONASS*

Control Aerodynamic Control with Electromechanical Actuation System

Propellant Type Composite Solid

Warhead Types HE* + Steel Ball


Warhead Effective Radius ≥ 40 m (Steel Ball)

Fuze Type PD* and Proximity

Accuracy (CEP) ≤ 15 m

46

TRG-230MISSILE


47

TRG-230 Missile provides accurate and effective fire power on high priority targets within the ranges 20 - 70 km.

TRG-230 Missile can be launched from ROKETSAN TIGER Multi Barrel Rocket Launcher (MBRL) Weapon System, MCL (Multi-Caliber Launcher) Artillery Weapon System and other platforms with compatible interfaces.


• Ready to Fire

• Highly Accurate


• Precision Strike Capability

• Anti-Jamming/Anti-Spoofing Solutions

TRG-230 MISSILEPotential Targets• Targets Located with High Accuracy


• Radar Sites

• Assembly Areas


• C3 Facilities





*HE: High PD and Proximity


TRG-230 MISSILE


Diameter 230 mm

Weight 210 kg

Range 20 - 70 km

Guidance GPS* + GLONASS* Aided INS*





Warhead Effective Radius ≥ 55 m



48

TRGK-300GUIDANCE KIT


49

With the installation of the TRGK-300 Guidance Kit on unguided 300 mm rockets, targets within a range of 40 - 90 km can be surpassed with high accuracy.

The guidance kit integration provides a cost-effective solution by using the existing rocket components.

TRGK-300GUIDANCE KIT



*HE: High Explosive


Technical Specifications of Rocket

Diameter 300 mm

Weight 600 kg

Range 40 - 90 km

Guidance GPS* + GLONASS*





Warhead Effective Radius ≥ 70 m



TRGK-300 GUIDANCE KIT


• Ready to Fire

• Highly Accurate

• Increased Effectiveness Against Critical Targets

50

TRG-300TIGER MISSILE


System Specifications• Combat Proven

• 7/24 All Weather/Terrain Usage Capability

• Ready to Fire


• Long Range Highly Accurate Precision Strike Capability

• Anti Jamming/Anti Spoofing Solutions

TRG-300 TIGER Missile provides accurate and effective fire power on high priority targets within the ranges 20 - 120 km.

TIGER Missile can be launched from ROKETSAN TIGER Multi Barrel Rocket Launcher (MBRL) Weapon System, MCL (Multi-Caliber Launcher) Weapon System and other platforms with compatible interfaces.



• Radar Sites

• Assembly Areas


• C3 Facilities


TRG-300TIGER MISSILE

51

*BLOCK-II: Enhanced Warhead Dynamic Effectiveness




*HE: High Explosive

TRG-300 TIGER MISSILE

Technical Specifications BLOCK-I BLOCK-II*

Diameter 300 mm

Weight 585 kg 670 kg

Range 30 - 120 km 20 - 90 km

Guidance GPS* + GLONASS* Aided INS*

ControlAerodynamic Control

with Electromechanical Actuation System



Warhead Weight 105 kg 190 kg

Warhead Effective Radius ≥ 70 m ≥ 80 m

Fuze Type Point Detonating and Proximity


52

T-107/122MULTI-PURPOSE and

MULTI BARREL ROCKET LAUNCHER (MBRL) SYSTEM


53

The T-107/122, 107 and 122 mm Multi-Purpose and Multi Barrel Rocket Launcher (MBRL) is a weapon system that provides concentrated and effective fire support against high priority targets in all weather and terrain conditions during day and night.

Highly maneuverable T-107/122 MBRL can fire TR-107, TR-122, TRB-122 Rockets and TRG-122 Missiles.

The T-107/122 MBRL Battery consists of Command & Control Vehicle, Ammo Supply Vehicle, Meteorology Vehicle, Maintenance & Repair Vehicle and other auxiliary vehicles.

T-107/122MULTI-PURPOSE and MULTI BARREL ROCKET LAUNCHER (MBRL) SYSTEM


Diameter 107 mm and 122 mm

Range 3 - 40 km

Number of Tubes 3x20 TR-107 1x20 TR-122, TRB-122, TRG-122

Salvo Interval 0.5 ~ 2 sec

Vehicle 4x4 or 6x6 Tactical Wheeled Vehicle

Aiming Automatic Manual (Back-Up)

Stabilization 4 Hydraulic Legs

Vehicle Navigation INS*/GPS* System



T-107/122 MULTI-PURPOSE and MULTI BARREL ROCKET LAUNCHER (MBRL) SYSTEM

System Specifications• Onboard Crane for Ammunition Supply

• Automatic Aiming

• Communication System (Wired/Wireless – Voice/Data)

• Hydraulic Stabilization System

• Integrated Ground Meteorology System

• Cabin Pressurization System (Optional)

• Power Supply and Distribution System

• Inside Cabin or Remote Firing Capability

• Ready to Fire in Maximum 5 Minutes

• Ballistic Protection (Optional)

• Capability of Firing at Negative Elevation

5454

T-107/122 MBRL Battery Structure

The T-107/122 MBRL Battery is capable of performing independent missions with its mission support vehicles.

T-107/122 Battery is composed of 1 x C-107/122 Command & Control Vehicle, 6 x T-107/122 Launchers, 6 x L-107/122 Ammo Supply Vehicles, 1 x M-107/122 Meteorology Vehicle and 1 x R-107/122 Repair Vehicle. The number and type of vehicles can be customized according to the customer's requirements.

T-107/122 MBRL Battery Organization

The Command & Control System and Weapon Management System of the battery can be integrated with modern fire support automation (tactical fire direction system) and battlefield command-control and management systems. Target acquisition radars or Unmanned Aerial Vehicles supply target information to the Battery.

Integration with Tactical Fire Direction System,

Battlefield C2 and Management System and Target Acquisition Systems

R-107/122 Repair Vehicle

6 x L-107/122Ammo Supply

Vehicles

6 x T-107/122Launchers

M-107/122 Meteorology Vehicle

C-107/122 Command & Control Vehicle

Fire Support Command Control System

Target Acquisition

RadarQuick Fire

Channel

Technical Fire Direction

System Technical Fire Direction

System

Quick Fire Channel

Tactical Fire Direction System

LauncherFire Control System

Battery C2 Vehicle Command Control System

Forward Observer

NATO & C4I Systems

UAV

5555

Shoot and Scoot Capability

The T-107/122 Launcher perfectly performs “shoot and scoot tactics” with its inertial and global navigation and automatic aiming systems.

• Capability to fire within 5 minutes after deploying

• Capability to displace in 5 minutes after firing

• Capability to carry out multiple firing missions in a short period of time.

Negative Elevation

The T-107/122 is able to fire the 107 mm rockets at negative elevations in mountainous areas to targets below the launcher's altitude.

Direct Fire Capability (Optional)• TR-107 Rockets can be fired directly by

using direct fire control unit inside the cabin.

• Launcher’s hydraulic support legs, help the dispersion to be kept at a minimum level.

• With its massive fire capability, the T-107/122 Launcher can be used not only to suppress target areas, but it can also be used against point targets effectively.

High Mobility Capability

The T-107/122 Launcher Platform is a 4x4 or 6x6 tactical wheeled vehicle, which provides superior on-road and off-road capability. Its compact and robust structure provides a reliable launching platform.

Minimum Crew

Due to the fully automatic navigation and aiming systems, the T-107/122 can be operated with two crew, launcher commander and driver.

55

T-107/122 MULTI-PURPOSE and MULTI BARREL ROCKET LAUNCHER (MBRL) SYSTEM

56

T-122 MBRL MULTI BARREL

ROCKET LAUNCHER (MBRL) SYSTEM


The T-122, 122 mm Multi Barrel Rocket Launcher (MBRL) is a weapon system that provides concentrated and effective fire support against high priority targets in all weather and terrain conditions during day and night.

The T-122 MBRL System can provide indirect firepower within a range of 16 - 40 km.

T-122 MBRL MULTI BARREL ROCKET LAUNCHER (MBRL) SYSTEM

57

System Specifications• Steel or Composite Pods• Onboard Crane for Ammunition Supply• Automatic Aiming• Communication System

(Wired/Wireless – Voice/Data)• Hydraulic Stabilization System• Integrated Ground Meteorology System• Cabin Pressurization System (Optional)• Power Supply and Distribution System• Firing Inside Cabin or Remote Firing Capability• Ready to Fire within 5 Minutes• Ballistic Protection (Optional)• Combat Proven• 7/24 All Weather/Terrain Usage Capability• Increased Responsiveness • Increased Effectiveness Against Critical

Targets• Air, Rail and Sea Transportable• Three Man-Crew

T-122 MBRL MULTI BARREL ROCKET LAUNCHER (MBRL) SYSTEM

*INS: Inertial Navigation System *GPS: Global Positioning System


Diameter 122 mm

Range 16 - 40 km

Number of Tubes 2x20 TR-122, TRB-122, TRG-122

Salvo Interval 0.5 sec

Vehicle 6x6 Tactical Wheeled Vehicle

Elevation 0 - 55°

Deflection ±110°




Fire Control System

The Fire Control System of T-122 MBRL System provides mission critical advantages.

• Computer Aided-Deployment

• Fire Planning

• Technical Fire Direction

• Situational Awareness

• Digital Integration to other Fire Support Systems

• Digital Mapping

• Digital Communication

• User friendly interface

58

MCL (MULTI-CALIBER LAUNCHER) WEAPON

SYSTEM


59

MCL (Multi-Caliber Launcher) Weapon System is capable of providing precise fire on critical targets between 16 - 280 km range.

MCL Weapon System is a highly maneuverable fire support system that can fire TR-122, TRB-122, TRG-122, TRG-230, TRG-300, TRGK-300 and KHAN Rockets and Missiles. The battery is composed of Command & Control Vehicle, Launchers, Ammo Supply Vehicles, Meteorology Vehicle and Maintenance & Repair Vehicle, as well as other mission vehicles needed.

MCL (MULTI-CALIBER LAUNCHER) WEAPON SYSTEM

MCL (MULTI-CALIBER LAUNCHER)WEAPON SYSTEM



System Specifications• Steel or Composite Pods

• Onboard Crane for Ammunition Supply (Optional)

• Automatic Aiming

• Communication System (Wired/Wireless – Voice/Data)

• Hydraulic Stabilization System

• Integrated Ground Meteorology System

• Cabin Pressurization System (Optional)

• Power Supply and Distribution System

• Firing from the Cabin or Remote Firing Capability

• Ready to Fire within 5 Minutes

• Ballistic Protection (Optional)


Diameter 122 mm, 230 mm, 300 mm and 610 mm

Range 10 - 280 km

Number of Tubes 2x20 TR-122, TRB-122, TRG-122 2x6 TRG-230 2x4 TRG-300, TRGK-300 1x KHAN

Salvo Interval 0.5 - 15 sec

Vehicle 6x6 or 8x8 Tactical Wheeled Vehicle




122 mm (TR/TRB/TRG-122)2 Pods (2 x 20=40 Rockets/ Guided Rockets)

230 mm (TRG-230) 2 Pods (2 x 6=12 Missiles)

610 mm (KHAN)1 Pod (1 Missile)

300 mm (TIGER) 2 Pods (2 x 2=4 Missiles)

6060

Battery Structure

The MCL Weapon System Battery is capable of performing independent missions with its mission support vehicles. A typical MCL Weapon System battery is composed of 1 x Command & Control Vehicle, 6 x Launcher Vehicles, 6 x Ammo Supply Vehicles, 1 x Meteorology Vehicle and 1 x Maintenance & Repair Vehicle. The number and type of vehicles can be customized.

Battery Organization

The Command & Control System and Weapon Management System of the battery can be integrated with modern fire support automation (tactical fire direction system) and battlefield command-control and management systems. Target acquisition radars or Unmanned Aerial Vehicles supply target information to the Battery.

Integration with Tactical Fire Direction System,

Battlefield C2 and Management System and Target Acquisition Systems

Meteorology Vehicle

Command & Control Vehicle

Repair Vehicle6 x Ammo Supply Vehicles

6 x Launchers

Ease of Use

Transportability

Flexibility

DeterrentForce

LogisticSupportability

Survivability

Mobility

Interoperability

Shoot and Scoot

• Ergonomy• User Friendly GUI• Automated System &

Minimum Crew

• Long Range & Mass Fire Capability

• Wide Range and Area Coverage

• Precision Fire

• Situational Awareness• Safe and Secure

Communication• Anti Jamming/Anti

Spoofing Solutions

• Fast Deployment & Redeployment

• Short Preparation Time to Fire

• Integration to NATO & C4I Systems

• All Terrain Conditions

• Multiple Caliber • Autonomous• Day & Night Operational

Capability• All Weather

• Compact Structure• Land, Rail, Sea and Air

Transportation

• High Reliability & Operational Readiness

• Long Shelf Life & Life Extention

• Training and Training Aids • Long Term Logistic Support • Tailored Solutions

6161

Deterrent Force

The system is a deterrent force due to its long range and mass fire capabilities. It can therefore perform vital tasks in a wide range of missions from peace keeping, defence and to attack operations for the support of a maneuvering force.

High Survivability

The system provides high survivability on the battlefield with its quick aiming and displacement capability, shoot and scoot ability, high mobility and secure digital & voice communication system.

Transportability

The system can be transported by land, air, sea and railways.

It is transportable by almost all types of cargo planes.

High Mobility

The Launcher Vehicle is a 6x6 or 8x8 tactical wheeled vehicle, which provides superior on-road and off-road travel capability. Its compact and robust structure provides a reliable launching platform.

Shoot and Scoot Capability

The Launcher perfectly performs “shoot and scoot” with its inertial and global navigation and automatic aiming systems.

• Capability to fire within 5 minutes after deploying

• Capability to displace in 5 minutes after firing

• Capability to carry out multiple firing missions in a short period of time

MCL (MULTI-CALIBER LAUNCHER)WEAPON SYSTEM

62

KHAN MISSILE


63

KHAN Missile provides accurate and effective fire power on strategic targets within the battlefield.

The missile can be launched from 8x8 Tactical Wheeled Vehicle, ROKETSAN MCL (Multi-Caliber Launcher) Artillery Weapon System and other platforms with compatible interfaces.



• Radar Sites

• Assembly Areas


• C3 Facilities

• High Priority Targets

KHAN MISSILE


Diameter 610 mm

Weight 2,500 kg

Range 80 - 280 km

Guidance GPS* + GLONASS* Aided INS* INS* Only

Control Aerodynamic Control with Hydraulic Actuation System


Warhead Type HE* Blast Fragmentation



Accuracy (CEP) ≤ 10 m GPS + GLONASS Aided INS* ≤ 100 m INS* Only

KHAN MISSILE




*HE: High Explosive


Sealed Pod

Features• Combat Proven

• 7/24 All Weather/Terrain Usage Capability

• Ready to Fire


• Long Range Highly Accurate Precision Strike Capability

• Anti Jamming/Anti Spoofing Solutions

64

ALKADIRECTED ENERGY

WEAPON SYSTEM


ALKA DIRECTED ENERGY WEAPON SYSTEM

65

ALKA Directed Energy Weapon System (DEWS) neutralizes or totally destructs targets such as Improvised Explosive Devices (IED), mini/micro unmanned aerial vehicles (UAV), drones, mini/micro unmanned aerial vehicles (UAV) carrying a variety of payloads (camera, explosives, etc.) as well as swarm attacks.

ALKA DIRECTED ENERGYWEAPON SYSTEM

Drone

Swarm Destruction Destruction Interception

IED*Precise

TrackingSwarm

Interception

* EJS: Electromagnetic Jamming System

* EDS: Electromagnetic Destruction System

* IED: Improvised Explosive Device

System Specifications• Automatic Aiming to Target Detected by

Radar

• Automatic Target Detection and Tracking Through Artificial Intelligence Assisted Image Processing (Minimum False Alarm Rate)

• Standalone Use without Radar

• EJS* 4,000 m

• Effective Laser Destruction Range 500 m

• Effective Destruction Range of 1,000 m with EDS*

• Independent of Number of Targets, Interception Capability Against Swarm Attacks

• Selection of Precise Destruction Point on the Target

• Tracking and Destruction of High Speed Targets (150 km/hr)

• High Precision Target Tracking (8 mm Precision at 1,000 m)

• Multiple Target Tracking

• Day/Night Operations

• Surveillance Only Mode

• Reduction of Operator Cognitive Workload through Neuro-Ergonomics Approach

• Low Cost per Shot

• Successive Firing Capability

66

Areas of Use

• Urban Operations (against IEDs)

• Protection of Military Units

• Protection of Government Buildings

• Protection of Airports

• Protection of Residential Areas

• Protection of High-Tech Production Facilities

• Protection of Power Plants

• Protection of VIP

• Protection of Other Critical Facilities

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Mobile Use

• Ability to Perform on 4X4 Vehicle

• Operation within the Cabin

• Internal Power Unit

• Modular Configuration

• Deployment on Desired Location

• Easy Operation with 2 Personnel

Stationary Use

• Tower or Shelter Configuration

• Remote Operation from the Command Center

• Use of External Power Sources

• Easy Operation with Single Personnel

ALKA DIRECTED ENERGY WEAPON SYSTEM

68

ASWANTI-SUBMARINE

WARFARE ROCKET AND LAUNCHER SYSTEM


Anti-Submarine Warfare (ASW) Rocket and Launcher System can be deployed on patrol boats and engage undersea targets at 500 - 2,000 m ranges and in 15 - 300 m depth. Stabilized Launcher has automatic laying (manual as back-up) system which works in couple with vessel’s combat management system and sonar.

The system can fire insensitive munition class rockets in single or in salvo, and its time setting fuze enables the rockets to detonate at the desired depth.

The fire control system utilizes the navigation and target data provided by the vessel and calculates the necessary firing data.

ASWANTI-SUBMARINEWARFARE ROCKET AND LAUNCHER SYSTEM

69

Diameter 196 mm

Weight (Rocket) 35.5 kg

Explosive Weight 12 kg

System Weight 1,200 kg (with Rockets)

Length (Rocket) 1.3 m

Range 500 - 2,000 m

Depth of Detonation 15 - 300 m

Warhead Type HE*

Fuze Type Time Setting (Depth Setting by Fire Control Computer)

Salvo Interval 0.8 sec

Propellant Type Reduced Smoke Composite Propellant

Launcher System Stabilized, Automatic Launcher Laying Using Vessel Sonar Data

Number of Rockets 6 in the Launcher

Launcher Laying Automatic Manual (Back-up)


ASW ANTI-SUBMARINE WARFARE ROCKET AND LAUNCHER SYSTEM

*HE: High Explosive

70

BALLISTICPROTECTION SYSTEMS


71

BALLISTICPROTECTION SYSTEMSROKETSAN Ballistic Protection Center (BPC) has been established to fulfill the ballistic protection requirements of military and civilian platforms. BPC is capable of designing, developing, producing and testing composite and explosive reactive armors (ERA) for lightly and heavy armored vehicles. It also provides force protection and Elastic Layered Armor System solutions to increase protection level of armored vehicles against RPG threats.

BALLISTIC PROTECTION SYSTEMS


• Heavy Armor Ceramic Block Production

• Oxide and Non-Oxide Ceramic Armor Production Infrastructure

• Infrastructure for Production of Passive Armor Materials

• Advanced Ceramics: AI203, Sic, Hp-B4c, etc.

• Support Materials: Aramide, Ultmwpe, S2 Glass, etc.

• High Hardness Ceramic Grinding, Cutting Confinement and Armor Welding Infrastructure

• Insensitive Reactive Armor Explosive Material Production

• Armor Integration Facility

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ERA

ERA system is a hybrid armor system developed to increase survivability of armored combat vehicles and their modernization.

Different energetic material technologies, from those developed for main battle tanks, to self-limiting reactive armor, to light armored vehicles are employed in ERA.

System Specifications

• Maximum Protection Against Anti-Tank Missiles (ATGM) and RPG Type Threats

• Protection Against Tandem Warheads

• Insensitive Explosive

• Minimum Collateral Damage

• Modular System – Easy Mounting and Dismounting

• Applicable on Different Type Vehicles

• No Maintenance Required

Reactive Armor on Wheeled Armored Vehicle

Reactive Armor on Tracked Armored Vehicle

Reactive Armor on Main Battle Tank

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Armor Kits Against Mine and Improvised Explosive Devices

Due to Mines and Improvised Explosive Devices (IED) being among the primary threats against military units, ROKETSAN has developed various ballistic protection systems, including armor and protection systems of the ALTAY Main Battle Tank. These systems have been designed in compliance with armored vehicles in the inventory of Turkish Armed Forces and tested in accordance with STANAG 4569 AEP 55 Volume 2 and Volume 3. The mine kits provide protection against mines in accordance with STANAG Levels II-IV.

Composite Armor System

Composite Armor System is a modern and light protection solution for kinetic and shaped charge ammunition and can be installed on land, naval and air platforms. At BPC ROKETSAN produces both passive composite armor plates from ceramic powder, and reactive armor plates from energetic materials with integrated armor modules.


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Base Protection

Base Protection Systems provide modular, portable and easily mountable ballistic protection against various threats for military camps. They also protect the critical facilities and areas against kinetic energy ammunition, mortar and RPG threats.

Force Protection System (RZB-20/20B)

The patented RZB-20/20B Composite Armor Block developed by ROKETSAN BPC for increasing the protection of bases is especially designed to protect against effects of light weapons, shrapnel and high explosives. Due to its modular structure, it can be easly installed and replaced.

75

Force Protection Systems (RZP-10)

RZP-10, developed for the protection of containers against blast effect and shrapnel of mortar rounds, is a protection panel integrated to reinforced containers with elevated roof. The patented RZP-10 can be easily installed due to its modular structure.

Force Protection Systems (RZK-7)

RZK-7, used with Composite Armor Blocks, has a caged structure and is part of the Force Protection Systems. RZK-7 can easily be positioned and relocated due to its modular structure.


76

BASEBLEED UNIT


77

BASEBLEED UNITBase Bleed Unit is used to increase the 155 mm Artillery Shell’s range.

Base Bleed Unit increases the range of the 155 mm MOD274 shell by approximately 30%.

Diameter 155 mm

Range of MOD274 39+ km with Base Bleed Unit

Propellant Type Composite Solid Propellant


Approx. 30% More Range

BASE BLEED UNIT

without Base Bleed Unit

with Base Bleed Unit


ALBATROS MODULAR INTEGRATED

INERTIAL NAVIGATION SYSTEM

ROKETSAN

79

ALBATROS MODULAR INTEGRATEDINERTIAL NAVIGATION SYSTEM

ALBATROSMODULAR INTEGRATEDINERTIAL NAVIGATIONSYSTEMITAR free ALBATROS is a modular integrated Inertial Navigation System (INS), which can utilize different Inertial Measurement Units (IMU) and Global Navigation Satellite System (GNSS) receivers. Modular architecture provides the capability to integrate the existing compatible IMUs and GNSS receivers. In addition, TurNa TM/TQ/N IMUs and ALDEBARAN/ANTARES GNSS receivers can be used in ALBATROS to obtain the INS that meets the system requirements.

ALBATROS can be integrated into different platforms (missiles, guided munitions, unmanned aerial vehicles, air and land platforms, naval vessels, etc.) due to its modular architecture.

Horizontal & Vertical Positioning Accuracy Horizontal Position (CEP) Vertical Position (PE) Inertial + GNSS* ≤ 10 m ≤ 10 mFree Inertial (Land Application) ≤ 0.5 nm/hr ≤ 0.5 nm/hrFree Inertial ≤ 10 nm/hr ≤ 10 nm/hr

Environmental Specifications Compatible with MIL-PRF-71185A (AR), MIL-STD-810G and MIL-STD-461E standards.

Mechanical Specifications DimensionsMass

210 mm x 210 mm x 165 mm< 4.7 kg


*GNSS : Global Navigation Satellite System (GPS, GLONASS, GALILEO, BEIDOU etc. globally positioned satellite based navigation systems)

ROKETSAN

ROKETSAN


ALDEBARANGPS and GLONASS

RECEIVER

ROKETSAN

81

ALDEBARAN GPS and GLONASSRECEIVER

ALDEBARAN GPS and GLONASS RECEIVER

ITAR free ALDEBARAN is a Global Navigation Satellite System (GNSS) receiver which can work with passive or active antennas, designed to perform under high dynamics (velocity, acceleration and altitude). The receiver which utilizes Global Positioning System (GPS) and GLONASS satellite systems, has a software-based structure, thus can be adapted to different platform (missile, guided munitions, unmanned aerial vehicle, land vehicle, etc.) requirements.

Performance Specifications

Channel Configuration GPS L1 C/A, GLONASS L1 C/A, SBAS L1 C/A

Horizontal Position ≤ 10 m (RMS) Accuracy

Vertical Position ≤ 15 m (RMS) Accuracy

Dynamic Range

Velocity ≥ 1,400 m/sec

Altitude ≥ 40,000 m

Mechanical Specifications

Dimensions Ø 149 mm x 49 mm

Mass 826 g

Environmental Specifications

Compatible with MIL-STD-810G and MIL-STD-461E standards.


ROKETSAN

ROKETSAN


ANTARESGPS and GLONASS

RECEIVER

ROKETSAN

83

ANTARES GPS and GLONASSRECEIVERANTARES is a Global Navigation Satellite System (GNSS) receiver designed to perform under high dynamics (velocity, acceleration and altitude). The receiver which utilizes Global Positioning System (GPS) and GLONASS satellite systems, has a software-based structure, thus can be adapted to different platform (missile, guided munitions, unmanned aerial vehicle, land vehicle etc.) requirements. With its innovative architecture, ANTARES can be integrated with new capabilities such as different satellite constellations and internal anti-jamming.

Performance Specifications

Channel Configuration GPS L1 C/A, GLONASS L1 C/A

Position ≤ 10 m (RMS) Accuracy (3D)

Dynamic Range

Velocity ≥ 1,400 m/sec

Altitude ≥ 40,000 m

Mechanical Specifications

Dimensions Ø 108 mm x 38 mm

Mass 340 g

Environmental Specifications

Compatible with MIL-STD-810G and MIL-STD-461E standards.


ANTARES GPS and GLONASS RECEIVER

ROKETSAN

ROKETSAN


RAL2000 NAVIGATION GRADE RLG

BASED INERTIALMEASUREMENT UNIT

85

RAL2000 NAVIGATION GRADE RLG BASED INERTIAL MEASUREMENT UNIT

RAL2000 NAVIGATION GRADE RLG BASED INERTIAL MEASUREMENT UNITThe RAL2000 is a navigation grade Inertial Measurement Unit (IMU) developed for long range missiles in addition to land, sea and air platforms, including unmanned aerial vehicles. The RAL2000 could satisfy high navigation performance and adverse environmental requirements through its optimized system design, Ring Laser Gyroscopes and Quartz Pendulum Accelerometers. It is the upgraded version of RNU-100M in terms of mass and volume.

Technical Specifications1

Sensor Quartz Pendulum Accelerometer Ring Laser Gyroscope3

Performance SpecificationsMeasurement Range ± 22 g ± 400 °/secResidual Bias Error (1σ) < 25 μg < 0.04 °/hr

Mechanical Specifications2 DimensionsMass

IMU: Inertial Measurement Unit

1 IEEE-528-2001

2 IEEE-1293-1998

3 IEEE-647-2006

265 mm x 255 mm x 230 mm< 16 kg

Environmental SpecificationsCompatible with MIL-STD-810G and MIL-STD-461E standards.


RNL2000-KRLG BASED INERTIAL LAND

NAVIGATION SYSTEM

87

RNL2000-K RLG BASED INERTIAL LAND NAVIGATION SYSTEM

RNL2000-KRLG BASED INERTIAL LANDNAVIGATION SYSTEM

RNL2000-K is a navigation grade Inertial Measurement Unit (IMU) capable of satisfying the high navigation performance and adverse environmental requirements through optimized system design and Ring Laser Gyroscopes.

The ITAR free RNL2000-K can be integrated into air, underwater and surface platforms with auxiliary aiding systems.

Optionally, RNL2000-K can be provided with Navigation Control and Visualization Unit (NCVU).

*GNSS : Global Navigation Satellite System (GPS, GLONASS, GALILEO, BEIDOU etc. globally positioned satellite based navigation systems)

*ZUPT: Zero Velocity Update

*DT: Distance Traveled

Horizontal & Vertical Positioning Accuracy Horizontal Position (CEP) Vertical Position (PE)Inertial + GNSS* ≤ 10 m ≤ 10 mFree Inertial ≤ 18 m ≤ 10 m(ZUPT* period: 4 min.) (DT* ≤ 27 km) (DT ≤ 35 km)



265 mm x 255 mm x 230 mm< 15.5 kg

88

RNU-100MNAVIGATION GRADE

RLG BASED INERTIAL MEASUREMENT UNIT


89

RNU-100MNAVIGATION GRADE RLG BASED INERTIAL MEASUREMENT UNIT

RNU-100M NAVIGATION GRADE RLG BASED INERTIAL MEASUREMENT UNIT

RNU-100M is a navigation grade Inertial Measurement Unit (IMU) developed for land, aerial and naval platforms. RNU-100M could satisfy high navigation performance and adverse environmental requirements through optimized system design, Ring Laser Gyroscopes and Quartz Pendulum Accelerometers.

Sensor Quartz Pendulum Accelerometer2 Ring Laser Gyroscope3

Performance SpecificationsMeasurement Range ± 22 g ± 400 °/secResidual Bias Error (1σ) < 25 μg < 0.04 °/hr


Mechanical SpecificationsDimensionsMass

315 mm x 420 mm x 240 mm22 kg

1 IEEE-528-2001

2 IEEE-1293-1998

3 IEEE-647-200


TurNa-NNAVIGATION GRADE

FOG BASED INERTIAL MEASUREMENT UNIT

ROKETSAN

91

TurNa-N NAVIGATION GRADE FOG BASED INERTIAL MEASUREMENT UNITTurNa-N is a navigation grade Inertial Measurement Unit (IMU) consisting of 3 Fiber Optic Gyroscopes (FOG) and 3 Quartz Pendulum Accelerometers. TurNa-N is designed for high performance under harsh environmental conditions, thus can be used on different platforms such as land vehicles, fire control systems, unmanned aerial vehicles and naval vessels.

With its high performance, TurNa-N can satisfy both Global Navigation Satellite System (GNSS) aided and pure inertial navigation (0.8 nm/hr) requirements.


TurNa-N NAVIGATION GRADE FOG BASEDINERTIAL MEASUREMENT UNIT

Sensor Quartz Pendulum Accelerometer2 Fiber Optic Gyroscope3

Performance SpecificationsMeasurement Range ± 30 g ± 250 °/secResidual Bias Error (1σ) < 50 µg < 0.04 °/hr

Mechanical SpecificationsDimensionsMass

286 mm x 160 mm x 160 mm< 9.4 kg

Environmental SpecificationsCompatible with MIL-STD-810G and MIL-STD-461E standards.

1 IEEE-528-2001

2 IEEE-1293-1998

3 IEEE-952-1997

ROKETSAN

ROKETSAN


TurNa-TQTACTICAL GRADE


ROKETSAN

93

TurNa-TQ TACTICAL GRADE FOG BASED INERTIAL MEASUREMENT UNIT TurNa-TQ, containing 3 Fiber Optic Gyroscopes (FOG) and 3 Quartz Pendulum Accelerometers, is a tactical grade Inertial Measurement Unit (IMU) which can be used in different guidance, control and navigation applications. TurNa-TQ has high performance under harsh environmental conditions and can be used in different platforms. TurNa-TQ can be used in missiles, guided munitions, stabilized platforms, unmanned aerial vehicles and on their flight computer systems.

TurNa-TQ TACTICAL GRADE FOG BASED INERTIAL MEASUREMENT UNIT


Sensor Quartz Pendulum Accelerometer2 Fiber Optic Gyroscope3

Performance SpecificationsMeasurement Range ± 60 g ± 490 °/secResidual Bias Error (1σ) < 1 mg < 1 °/hr


Ø 127 mm x 79 mm1.3 kg

Environmental SpecificationsCompatible with MIL-STD-810G and MIL-STD-461F standards.

1 IEEE-528-2001

2 IEEE-1293-1998

3 IEEE-952-1997

ROKETSAN

ROKETSAN


TurNa-TMTACTICAL GRADE


ROKETSAN

95

TurNa-TM TACTICAL GRADE FOG BASED INERTIAL MEASUREMENT UNIT

TurNa-TM TACTICAL GRADE FOG BASED INERTIAL MEASUREMENT UNIT TurNa-TM, containing 3 Fiber Optic Gyroscopes (FOG) and 3 Micro Electro Mechanical Systems (MEMS) accelerometers, is a tactical grade Inertial Measurement Unit (IMU) which can be used in different guidance, control and navigation applications. TurNa-TM has high performance under harsh environmental conditions and can be used on different platforms. TurNa-TM can be used in missiles, guided munitions, stabilized platforms, unmanned aerial vehicles and on their flight computer systems.

Sensor MEMS* Accelerometer2 Fiber Optic Gyroscope3

Performance SpecificationsMeasurement Range ± 10 g a ± 30 g b

Residual Bias Error (1σ) < 0.33 mg a < 0.66 mg b

± 490°/sec

< 1 °/hr



Ø 127 mm x 79 mm1.2 kg

Environmental SpecificationsCompatible with MIL-STD-810G and MIL-STD-461F standards.

1 IEEE-528-2001

2 IEEE-1431-2004

3 IEEE-952-1997

(a,b): In different axes TurNa-TM performance specifications

* MEMS: Micro Electro Mechanical Systems

ROKETSAN

ROKETSAN

97

Rocket Motor Igniters & Safe and Arm Devices (SAD)

Rocket Motor Igniters

• Designed for Solid Propellant Rocket Motors (with or without SAD)

• Designed for Turbojet Motors

• Complies with MIL-STD-1901A, MIL-STD-1576, STANAG 4368

• Safe to Electrostatic Discharge (AECTP-500)

• Complies with Electromagnetic Compatibility Standards (MIL-STD-464A/461F)

• 1W/1A/5 Minutes No Fire, High Reliability

Safe and Arm Devices (SAD)

• Arm - Safe Signal

• Arm - Safe Indicator

• Manual / Remote Control

• Arming Time for EM-SADs <250 ms

• -40 to +70°C Operation Temperature

• Adjustable Interfaces (Mechanical or Electrical)

PYROTECHNIC SYSTEMS

EM-EKM100 EM-EKM200 EM-EKM300 E-EKM400 EM-EKM500 EM-EKM600

PYROTECHNIC SYSTEMS

98

Initiators & Power CartridgesHighly reliable, low cost and light weight low voltage hot-bridgewire initiators are used for initiations of rocket motor igniters, gas generators, and pyrotechnic devices.

Squibs RSKM-100 RSKU-100 RSKT-200 RSKKOM-100 RSKKOM-110

Bridgewire Resistance 1.1 ± 0.1 Ω 0.6 ± 0.1 Ω 2.15 ± 0.15 Ω 1.15 ± 0.1 Ω 1.15 ± 0.1 Ω

Max. No-Fire (5 min.) 1 A/1 W 1 A/1 W 0.35 A 1 A/1 W 1 A/1 W

All Firing Current 3.5 A (50 ms) 3.5 A (50 ms) 1.2 A (10 ms) 3.5 A (50 ms) 3.5 A (50 ms)

Function Time < 5 ms < 25 ms < 10 ms < 5 ms < 5 ms

Output (16,4 cc chamber) 1.5 MPa 1.5 MPa 1.5 MPa 0.7 MPa 0.7 MPa

Electrical Interface Pin Type Pin Type Pin Type Pin Type Pin Type

Operational Temperature -60 / +70ºC -60 / +70ºC -35 / +60ºC -60 / +70ºC -60 / +70ºC

Environmental Tests MIL-DTL-23659 MIL-DTL-23659 MIL-DTL-23659 MIL-DTL-23659 MIL-DTL-23659

Power Cartridges RS-GK100 RS-GK200 RS-GK400

Bridgewire Resistance 1.15 ± 0.2 Ω (Dual BW) 1.15 ± 0.2 Ω (Dual BW) 1.15 ± 0.2 Ω (Dual BW)

Max. No-Fire (5 min.) 1 A/1 W (Each BW) 1 A/1 W (Each BW) 1 A/1 W (Each BW)

All Firing Current 3.5 A - 50 ms (Each BW) 3.5 A - 50 ms (Each BW) 3.5 A - 50 ms (Each BW)

Function Time < 10 ms < 10 ms < 10 ms

Output (16,4 cc chamber) 2.0 MPa 1.0 MPa 1.0 MPa

Electrical Interface MS3111P8-4P Connector per MIL-DTL-26482 Pin Type Shielded Twisted Pair

Cable

Operational Temperature -60 / +70ºC -60 / +70ºC -60 / +70ºC

Environmental Tests MIL-DTL-23659 MIL-DTL-23659 MIL-DTL-23659


99

Detonation Systems

Detonation Systems, Exploding Foil Initiators (EFI) and Low Energy Exploding Foil Initiators (LEEFI), are used to activate warhead or rocket motors. The systems are resistant to electromagnetic interference and are activated with high voltage.

System Properties

• Function time < 5µsec

• Hermetically Sealed

• Complies with MIL-DTL-23659, MIL-STD-1316 and MIL-STD-1901A

PYROTECHNIC SYSTEMS

100


RS-PC100 Explosive Bolt



RS-PIC100 Ejection Device

RS-PV100 Pyro Valve

PropertiesType: Non-

Fragmenting Tensile Load ≥ 2,000 N

Type: Non-Fragmenting

Tensile Load ≥ 10,000 N

Type: Non-Fragmenting Tensile

Load ≥ 91,000 N Double Bridgewire

Tensile Load ≥ 20,000 NMin. Force: 10,000 N

Double BridgewireDouble Bridgewire

Weight < 100 g < 100 g < 300 g < 300 g < 350 g

Function Time < 10 ms < 10 ms < 10 ms < 10 ms < 10 ms

Bridgewire @21°C 1.1 ± 0.1 Ω 1.1 ± 0.1 Ω 1.1 ± 0.1 Ω per each 1.1 ± 0.1 Ω per each 1.1 ± 0.1 Ω per each

Maximum No-Fire @21°C

1A/1W 5 Minutes 1A/1W 5 Minutes 1A/1W 5 Minutes 1A/1W 5 Minutes 1A/1W 5 Minutes

All Fire Current 3.5 A (50 ms) 3.5 A (50 ms) 3.5 A (50 ms) per Each Bridgewire

3.5 A (50 ms) per Each Bridgewire

3.5 A (50 ms) per Each Bridgewire

Operational Temperature Range -54 °C / +71 °C -54 °C / +71 °C -54 °C / +71 °C -54 °C / +71 °C -54 °C / +71 °C

Shelf Life 15 Years 15 Years 15 Years 15 Years 15 Years

Pyrotechnic Compositions

• Magnesium/Teflon/Viton (MTV)

• Boron/Potassium Nitrate (BKNO3)

• Zirconium/Potassium Perchlorate (ZPP)

• MIL-P-46994B Compliant Formulation, II-B, II-D and II-T Size Pellets

• Doughnut Shaped Pellets

• Nanothermite Compositions

• Special Primer Compositions

101

RS-PI100Pin Pusher

RS-PI172Pin Pusher

RS-PI300 Pin Pusher

RS-KK100 Cable Cutter

RS-PCK100 Pin Puller

RS-AS100 Separation

Nut

PropertiesStroke: 3mm

Min. Force: 500N

Cuts 0.05" (1.27 mm) diameter 6061-T6

Aluminum Pin

Stroke: 3mm Min. Force:

3,500N

3 mm diameter AISI 302/304 SS Steel Wire Cutter

Stroke: 13 mm (backwards)

Lateral Load on Pin ≤ 1,000 N

Tip: Non-Fragmenting

Tensile Load ≥ 75,000 N

Weight < 20 g < 0.4 g < 50 g < 100 g < 100 g < 600 g

Function Time < 5 ms < 1 ms < 15 ms < 10 ms < 10 ms < 10 ms

Bridgewire @21°C 1.1 ± 0.1 Ω 4 ± 9.5 Ω 1.1 ± 0.1 Ω 1.1 ± 0.1 Ω 1.1 ± 0.1 Ω 1.1 ± 0.1 Ω

Maximum No Fire @21°C

1A/1W5 Minutes

0.010 Ampere 10 s

1A/1W 5 Minutes

1A/1W5 Minutes

1A/1W5 Minutes

1A/1W5 Minutes

All Fire Current 3.5 A (50 ms)3.0 V DC

(100 μF capacitor) 150 mA (10 ms)

3.5 A (50 ms) 3.5 A (50 ms) 3.5 A (50 ms) 3.5 A (50 ms)

Operational Temperature Range -54 °C / +71 °C -54 °C / +71 °C -54 °C / +71 °C -54 °C / +71 °C -54 °C / +71 °C -54 °C / +71 °C

Shelf Life 15 Years 10 Years 15 Years 15 Years 15 Years 15 Years

PYROTECHNIC SYSTEMS

102

FUZE SYSTEMS


103

FUZE SYSTEMS

Action Impact, Impact, Impact Precision/Delayed Precision/DelayedArming Spin Acceleration Acceleration and SpinArm 14,000 rpm 25 g 120,000 g, 830 rpsOperational Temperature -40 to +60 °C -40 to +60 °C -40 to +60 °CWeight 637 gr 740 gr 22 grFuze Length 123 mm 196 mm 31.6 mmIntrusion Length 46 mm 55 mm 9.6 mmDiameter Ø40 mm Ø64 mm Ø17 mm

107 mm Rocket Fuze

122 mm Rocket Fuze

20 mm M56 Ammo Fuze (M505 A3)


Action Impact, Time (0-200 s), Impact, Time (0-200 s), Proximity (1-15 m) Proximity (1-15 m)Arming Acceleration Acceleration Arm 25g 25 gOperational Temperature -40 to +60 °C -40 to +60 °CWeight 740 gr 2,400 grFuze Length 233 mm 224 mmIntrusion Length 54 mm 57 mmDiameter Ø64 mm Ø80 mm

122 mm Proximity Rocket/Missile Fuze

300 mm Proximity Rocket/Missile Fuze

FUZE SYSTEMS

Programmable, delayed and precision mechanical fuzes for 107 mm and 122 mm rockets; electromechanical proximity fuzes/missiles (122 mm and 300 mm); fuzes for Anti-Submarine Warfare (ASW) Rockets; tactical

missiles; anti-tank missiles and unmanned aerial vehicles’ munitions are produced in accordance with MIL-STD-331 and MIL-STD-1316.


PRODUCTCATALOG

ROKE

TSAN

PRO

DUCT

CAT

ALOG

ENG

2019 ENG-v2

Kemalpaşa Mahallesi Şehit Yüzbaşı Adem Kutlu Sokak No:21 06780 Elmadağ, ANKARA / TURKEYPhone : + 90 (312) 860 55 00Fax : + 90 (312) 863 42 08e-mail : [email protected] : www.roketsan.com.tr


roketsan product catalogthe laser seeker may be equipped with a proximity sensor. the teber tail...

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