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ALAS XX

Precision at its best

EDePro | Alas XX
Fifth-Generation Cruise Missile for Land Attacks

ALAS XX is a multi-purpose surface-to-surface missile system developed under the Yugoimport SDPR programme for the Serbian Armed Forces. Officially introduced into service in September 2025, ALAS XX provides precision-strike capabilities to modern artillery formations when integrated with the modular, self-propelled MLRS M-18 OGANJ - the first Serbian artillery platform capable of launching guided missiles. Each launcher vehicle can accommodate four to eight missile containers, depending on mission configuration.

The system is designed for NLoS (Non-Line-of-Sight) engagement: its embedded inertial measurement unit (IMU/INS) and imaging homing head permit automatic guidance to designated coordinates supplied by third-party sensors (UAVs, forward observers or other target-acquisition assets). The architecture supports a “man-in-the-loop” concept, allowing real-time target selection and in-flight course corrections.

ALAS XX’s sensor suite comprises electro-optical (EO) and imaging infrared (IIR) seekers with day/night thermal imaging, enabling accurate target detection and tracking. The communication is provided via dual-channel links - primary fibre-optic cable with an alternative radio datalink - ensuring robust, low-latency control and resistance to electronic interference.

As for its matrix of sensors and effectors, it is designed for LoS (Line-of-Sight) targets and facilitates communication with other combat units. On top of that, they ensure its precision while removing the need for additional manoeuvres. ALAS XX has a maximum range of 25 km, while the missile can reach a cruising speed of 120–130 m/s and the maximum altitude of 500 m, supporting low-profile flight profiles that reduce radar exposure and enhance survivability against conventional air-defence detection.

KEY FEATURES

  • Integrated tandem warhead that can penetrate over 1000 mm of RHA
  • Initial alignment
  • AINS (Aided INS) based on the INS, GPS and altimeter (based on availability)
  • Midterm guidance based on the GCS’s preset trajectory points
  • Terminal guidance based on the homing head’s signal with an absolute accuracy of 1 m
  • Target detection range of up to 12 km
  • Target recognition range of up to 10 km
  • Tracking and lock-on range of up to 7 km
  • Target tracking can be aborted at any time during the flight
  • Target retracking, as well as setting a new target
  • Communication with the GCS (Ground Control Station) during the mission setup and flight
  • Continuous in-flight monitoring of all missile and communication and control subsystems (booster separation control, missile velocity control, warhead arming and disarming)
  • Mission abort (manual, via GCS, or automatic, based on predefined criteria)
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