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)