EDePro, Engine Development & Production

SAGR

Designed for superiority

EDePro | SAGR
The Benchmark for the Industry in Performance and Accuracy

The SAGR (Small Advanced Guided Rocket) is a result of EDePro’s groundbreaking in-house research and development programme for delivering a full range of top-notch solutions to keep pace with the rapid evolution of modern defensive operations. By pushing the boundaries of modern industrial technology, EDePro developed a 128mm, multirole, precision strike missile that effectively destroys moving and stationary targets alike, including medium armoured vehicles, small patrol boats, command posts and artillery positions.

Guided autonomously via reflected laser energy, SAGR can be both - ground-launched and air-launched, even from fixed and rotary-wing aircraft. It features LoAL (Lock-on-After-Launch), LoBL (Lock-on-Before-Launch) and laser coding capabilities, an enhanced built-in test, a seeker detection range of up to 10 km, as well as delayed and offset target lasing. 

 

Thanks to its navigation system, based on inertial navigation (INS) and GPS including the GCS’s preset trajectory points and impact point prediction (IPP) this missile is highly accurate and responsive to moving and stationary targets. Meanwhile, the communication with the launcher allows laser coding, along with sending and receiving commands and target position data.

With a minimum shelf life of 15 years, SAGR’s modular design makes its launch platform and warhead integration scalable and extremely reliable. It also makes the missile a new benchmark for the industry, in terms of performance, accuracy and modularity.

   

KEY FEATURES

  • Maximum effective range: 12.7 km (ground-launched); 29 km (air-launched)
  • Enabled communication with the Ground Control Station (GCS) during the mission setup
  • Inclinometer-based initial alignment during the mission setup
  • Aided INS (AINS) based on the INS or GPS (depending on availability)
  • Midterm guidance based on preset trajectory points from the GCS and IPP guidance
  • A seeker that catches the reflected laser beam on the expected range (> 4 km)
  • Terminal guidance based on the seeker’s signal
  • Mission abort: automatic, based on predefined criteria
  • A blast fragmentation warhead
EDePro | CTA
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