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107 mm SELF-PROPELLED MULTIPLE LAUNCH ROCKET SYSTEM

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