Light Offensive Rocket and Non Line of sight system

RALAS missile system is graded as a tactical system for backup of infantry action whose primary device is modern guided projectile with its own propulsion. RALAS system is designed for battlefield isolation and anti-armor combat at distances up to 9km.

Missile of RALAS system is consisted of following functional units – sub-systems:

• Homing system with gyro stabilized TV camera,
• Control subsystem,
• Payload (HEAT warhead capable to penetrate up to 1000 mm armored steel plate),
• Propulsion group consist of solid propellant rocket engines, sustainer and booster,
• Communication subsystem based on real time fiber optic communication (Communication subsystem contains coil holder – spool with 9 km of winded optic cable, electronic set of video emitter of laser signal with digital signal transceiver).

 Missile data

• Body diameter 175 mm
• Wing span 1500 mm
• Operational altitude 50~5000 m
• Equivalent flight speed >600 km/h
• Flight altitude 500 m
• Endurance 40 sec
• Limit of overload 4 g
• Max. weight in flight 57 kg
• Propulsion type
  -          Solid propellant booster (Total impulse 12375 Ns max. thrust)
  -          Solid sustainer (Total impulse 12789 Ns)