Light Multiple Launch Rocket Systems
From Concept to Combat: Defense Ideas in Action 2025
Our latest cruise missile system is designed for high-impact, long-range precision strikes, launched from land or sea. Utilizing a rocket booster for initial launch, the missile transitions into a cruise phase, ensuring extended reach and enhanced survivability.
L-MLRS 122
Light Multiple Launch Rocket System 122 mm (L-MLRS 122)
New 122mm G-DK 50km
MULTIPLE LAUNCH ROCKET SYSTEM 122mm (MLRS122) is acontainer type multi– barrel rocket launcher mounted on a military vehicle 4×4, with good tactical mobility.
MLRS 122 is used for sudden and concentrated fire on large– scale targets, such as concentrations of manpower, fire and technical assets, convoys, communication centers,
airfields, traffic nodes, docks, landings and other costcost– effective targets located in the depth of the enemy
Two types of launch modules (containers) can be installed on the launch pad:
Launch containers 122 mm
The launch module can consist of:
2×20 or 2×24 launcher steel tubes 122 mm (reusable reusable)
S-MLRS 122 can be launched:
- All missiles Standard Grad BM21 9M22U 122 mm missiles with HE warhead 18,4 kg with a maximum range of 20km
- Rocket G 2000 122mm maximum range 40 km,
- New G-DK 122 mm rocket with a maximum range of up to 50 km
Action time
- Time from transport to firing position up to 60 s (+ time for weapon orientation orientation),
- Time from firing to transport position 30 s,
- Rate of fire 0,4 s to 2 s between two rocket launches,
- Field of action in azimuth +/ -110 degrees,
- Time to change the container: 7 min (on the field with a vehicle equipped with a crane or in the workshop workshop).
MLRS122 is equipped forfor:
- Automatic, semi-automatic or manual movement of the launch platform in azimuth and elevation,
- Automatic and manual switching off of the elastic system (lowering and raising the foot ),
- Atomatic placing of the launcher in the position or transport and charging,
- Launching the rockets via the control panel from the driver's cabin or from the shelter via a 25 mcable,
- Automatic limitation of fire in defined zones of the field of action in the traverse and in elevation,
- Atomatic braking of the mechanisms after placing the fire elements.
Main components of MLRS 122:
- Activation panel for all Sub-Systems,
- Fire Control Unit (FCU),
- Fire Unit (FU),
- Control Unit,
- External HMI,
- Remote Fire trigger
- Sensor's positioning system (encoders for azimuth and elevation),
- GPS Compass (true azimuth)
- Rocket Type Loading Programing Device
- Meteo Probe, (optional),
- Weather trials (bulletin),
- Fire Control System (FCS) Computer (optional),
- Monitor, Touch panel & Bessel
- Inertial Navigation System (INS) (optional),
- Battle Management System (BMS)
L-MLRS 107
Light Multiple Launch Rocket System 107 mm (L-MLRS 107)
- LIGHT MULTIPLE LAUNCH ROCKET SYSTEM (L-MLRS 107) is a rocket systems land artillery based. L-MLRS 107 is designed for sudden, quick and powerful strikes at main directions of attack against enemy personnel and armored objects.
- This maneuverable automatic rocket system is characterized by high precision and consistency of fire.
- The L-MLRS 107 can fire 36 rockets in less than 20 seconds in a range of up to 11.5+ km, thus exploiting the surprise factor.
- L-MLRS is high mobility fire support system capable of being used in all types of terrain and operations, particularly special operations.
Launcher Fire Control System (FCS )
FCS is intended for determining the weapon standpoint and orientation by using the GPS antenna (INS Optional), as well as receiving data about target from the battery command post and communicating with higher command levels by using the radio – antenna, both located on the cabin roof.
Main subcomponents :
- Activation panel for all subsystems
- Sensor’s system
- GPS Compass (true azimuth)
- Meteo probe (bilten)
- FCS Computer
- Ballistics calculator
- BMS (Battle Management System)
- 12.2” Monitor
- Touch panel & Bessel
- Fire Control Unit
- Fire Unit
Technical features of 107 mm rocket with HE warhead
L-MLRS 107 is mounted on vehicle, 4×4 drive, and consists of:
- Azimuth and elevation platform mounted on the vehicle chassis.
- Four feet for supporting the launcher with electric drive and backup mode with manual drive,
- Launch container with 2 x 18 launch tubes (optional 2 x 24),
- Electric drives for moving the launch platform in the azimuth and elevation, with manual backup mechanism,
- Positioning sensors (encoders) for azimuth and elevation,
- Activation panel and control block,
- Electric trigger,
- Aiming devices,
- Integrated FCS with GPS and automatic sight,
- Electro movable camouflage roof with a special fabric that prevents radar detection of the launch platform.
- In a standard mode of operation (automatic mode), battery commander sends to the vehicle commander command to go to the firing position.
- Location of the target area is marked on the vehicle commander FCS digital map.
- The commander with the help of a GPS device comes with the L-MLRS 107 on the firing position.
- After reaching firing position FCS automatically calculate firing data, north direction from GPS north finder, terrain inclination from launcher sensors. With press of the button, L-MLRS 107 commander send command to FCS to automatically align launching platforms in elevation and azimuth according to calculated ballistic data.
- After alignment of the launcher platforms (time for deployment and alignment is less than 1 minute) launcher is ready for firing.
