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ZALA 421-12

From Wikipedia, the free encyclopedia
Unmanned plane ZALA 421-12

ZALA 421-12 is a micro miniature UAV developed and produced by the Izhevsk-based company ZALA Aero. It is a small, portable and reliable UAV platform. ZALA 421-12 is designed for front-line reconnaissance, overground and overseas surveillance. It takes 3 minutes to prepare the UAV for launching. The UAV is operated in the autonomous or semi-autonomous mode.

Specifications

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Physical:

  • Takeoff weight, kg - 3.9;
  • Navigation - GNSS;
  • Flight duration, h - 2;
  • Engine - electric;
  • Minimum speed, km/h - 65;
  • Maximum speed, km/h - 120[1] (limited by program);
  • Maximum flight altitude, m above the sea level - 3600;
  • Wingspan, m - 1.6;
  • Length, m - 0.62;
  • Wind speed during takeoff, no more than m/s - 10;
  • Payload weight, kg max - 1;
  • Launch - by means of catapult;
  • Landing - parachute.

Payload:

  • Color Video camera (550 TVL)
  • Infrared camera (320*240 px)
  • Photo camera (10 megapixels)
  • Hazard Gas Analysis Module (Optional)

References

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  1. Dalamagkidis, Konstantinos; Valavanis, Kimon P.; Piegl, Les A. (5 October 2011). On Integrating Unmanned Aircraft Systems into the National Airspace System: Issues, Challenges, Operational Restrictions, Certification, and Recommendations. Springer Science & Business Media. ISBN 978-94-007-2479-2. Retrieved 30 March 2026.

"ZALA 421-12 Russian Unmanned Aerial Vehicle (UAV)".

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