SP MLRS 107mm BASIC SUBSYSTEMS

•  Vehicle
• Launcher system
• Launcher control system
• Two multi tube rocket pods (2 x 24)
• Fire Control System
• Automatic awning cover

SP MLRS 107mm -  BASIC CHARACTERISTICS

• Caliber 107mm
• Range 8.2km  and 11.5km with extended range rocket
• Number of tubes 2x24
• Operating temperature range -30 to 60 deg          
• Programmed firing by firing control unit and remote firing, rate of fire - single- ripple 2 round/s
• Automatic and  semiautomatic aiming
• Automatic, semiautomatic and manual control of legs
• Stabilization of the system by four legs
• Direction range ±110˚
• Elevation range -1˚ to 60˚
• Special construction and disposition of the launcher system enables even distribution of loads on axle shafts in transport and firing over the cabin possibility
• Automatic fire control system- Automatic navigation, orientation and aiming by GPS and INS- Performing the task based on in advanced planned mission- Automatic and accurate calculation of firing elements
• Camouflage by semiautomatic tarpaulin cover and smoke screen

SP MLRS 107mm -  VEHICLE

Weight and Load Capacities: 

• Vehicle curb weight,kg                      8350
• Engine:           
• Model                                                740.13-260
• Type    diesel, turbocharged
• Rated horsepower, kwt (H.P)             191 (260)
• at crankshaft rotation, rpm                2200
• Maximum torque, NM (kgcm)               931 (95)
• at crankshaft rotation, rpm                       1300-1500
• Arrangement and number of cilinders           V-shape, 8
• Max speed, km/h                                           85
• Max slope angle at gross vehicle weight       25

LAUNCHER SYSTEM

 DIRECTIONAL MECHANISM-

• The worm type self locking gearing transmission serves to point the launching platform into demanded directional position in range of ± 110˚ with accuracy better then 1mil.
• Automatic locking device for fixing launching platform in desired position
• Automatic and semiautomatic control mode

ELEVATION MECHANISM -

• Two ball-bearing lead screws and self locking warm gearing transmission for positioning of launching platform in range from 0˚ to 60˚  with accuracy better than 1mil
• Automatic and semiautomatic control mode

LAUNCHING PLATFORM -

• Accept end carry two rocket pods in transport as well as firing condition.
• Equipped  with container locking devices the function of which is to precisely position and firmly grip container in four points at the same time

ROCKET PODS EQUILIBRATOR -

• Moment equilibration on rocket pods by mechanical equilibrator enabling low power consumption of the servo systems

-SUPPORT HAISTING JACK - LEGS -

• ‘Disconnects’ inherent elastic system of the vehicle and puts launching system into necessary stability during firing.
• Automatic and semiautomatic control mode

 SP MLRS 107mm - ROCKET PODS – CONTAINERS

•  Two containers - pods with 24 packed rockets each serve for storing/transporting and aiming  and firing rockets
• Possibility of single and multi rate usage

 LAUNCHER CONTROL SYSTEM CONSISTS OF:

•  Launcher control computer (LCC)
• Microcontrollers to control drives, position limits, protected fields of operation and fire
• Electromechanical drives – servo systems for- directional positioning of launching platform

               -elevation positioning of launching platform

               -support legs deployment/retracting

               -cover opening and closing

                -meteo sensor opening and closing

• Vehicle level determination system
• Fire Control Unit
• Manual Control Unit

 FIRE CONTROL UNIT

• Rocket selection buttons
• Fire rate selection
• Checking of firing circuit
• Default firing program option
• Remote firing unit
• Automatic rocket identification
• Single/ ripple mode operation
• Firing of smoke unit
• Automatic and semiautomatic support legs deployment/retraction
• Automatic and semiautomatic aiming of launching platform
• Moment equilibration on launching platform by mechanical equilibrator enabling low power consumption of the servo systems
• Maximal elevation platform speed 3 deg/s

MANUAL LAUNCHER CONTROL UNIT

• Enables manual control of
• Launching platform position
• Supporting legs position

VEHICLE LEVEL DETERMINATION SYSTEM

• Consists of two axis inclinometer, software and interface.
• Feature:
• Pitch (longitudinal) and roll (transversal) vehicle angles measurement; accuracy 0.5mils
• Automatic correction of elevation and azimuth of the launching platform due to vehicle inclination.

 AUTOMATIC AWNING COVER -

• Automatic, semiautomatic, and manual opening/covering
• Short time for opening/covering les then 10s
• Good protection and masking characteristics