KOL-15N supports development and project-related work connected with MLRS systems, with focus on 262 mm launcher-related components, launch module integration, control elements, platform interface support and customer-specific configuration.
The 262 mm MLRS configuration is intended for long-range rocket artillery applications and uses disposable launch containers with six 262 mm rockets per container. The system is designed for autonomous operation through navigation and fire control systems, supporting pre-planned combat missions, rapid preparation for firing and quick departure from the firing position.
KOL-15N does not provide 400 mm rocket production. The scope is focused on MLRS-related engineering, launcher components, integration support and customization for applicable 262 mm system configurations.
Final launcher configuration, component scope, platform interface and technical specification can be adapted according to project requirements. Contact us to discuss customization options for your MLRS-related application.
Launch Container Modules
Precision Tube Assemblies
Modular Platform Interface
Heavy-Duty Field Structure
| Specification | 262 mm MLRS Configuration |
|---|---|
| Product Reference | 262/400 mm Self-Propelled MLRS |
| KOL-15N Scope | 262 mm MLRS-related development, launcher components, integration support and customization |
| Range | 70 km with 262 mm Jerina 2 rocket |
| Caliber | 262 mm |
| Launch Device | Disposable containers |
| Number of Launch Modules | 2 |
| Rockets per Container | 6 rockets in one 262 mm container |
| Combat Set on Weapon | Total of 12 rockets in 262 mm configuration |
| Field of Action | Elevation: 0° to 60° Traverse: ±110° |
| Launcher Laying | Automatic Semi-automatic |
| Drive | Electric motors |
| Angular Velocity of Laying | Elevation: 1°/s max Traverse: 2°/s max |
| Orientation and Navigation | Autonomous, using INS and GPS |
| Combat Mission | Autonomous fire control system Pre-planned combat mission |
| Engagement / Launching | Burst-fire Single-shot launching Launching from vehicle cabin or shelter at 25 m |
| Loading | By lifting device on the utility vehicle |
| Weapon Stability During Firing | Achieved by four trails for system stability |
| Preparation / Leaving Time | Preparation for firing: 120 s Leaving firing position: 120 s |
| Operating Temperature | From -30°C to +50°C |
| System Weight | Vehicle dependent |
| Customization | Final launcher configuration, component scope and platform interface can be adapted according to project requirements |
Towed multiple launch rocket system for land and naval targets, available in 107 mm and 128 mm configurations with steel launch pods and automatic or semi-automatic elevation and traverse control.
Self-propelled modular MLRS designed for vehicle-mounted integration, supporting 122 mm and 262 mm rocket configurations with automatic line-of-sight control.
