Zala Aero Group manages a growing stable of Russian-engineered Unmanned Aircraft Systems (UASs). The ZALA 421-20 series is one such offering intended for tactical service use. The product is marketed as a long-loiter Intelligence, Surveillance, Reconnaissance (ISR) platform and geared towards various industries including military, law enforcement, border protection, the oil sector, fire service and the like.
The 421-20 features a 50 kilogram payload capability, mounting various optics and sensor sets as needed. The platform can be used to laser-designate precision-guided munitions for accompanying attack aircraft, offer InfraRed (IR) high definition camera functionality and provide real-time over-battlefield data collection / transference to ground forces / commanders for further interpretation.
Available optics fits include a High Definition camcorder, thermal zoom and photo / video camera, all gyro-stabilized for maximum picture / video clarity.
Operational ranges reach out to 400 kilometers with a mission endurance window between six and eight hours. Maximum operating altitude is 5,000 meters with power provided from an internal combustion engine driving a bladed propeller unit in pusher configuration, giving the vehicle a speed up to 220 kilometers per hour. Onboard navigation is handled by an INS-corrected GPS / GLONASS system with electronic telemeter.
The overall design arrangement of the aircraft is of twin-boom allowing the central fuselage nacelle to house all pertinent mission equipment and the powerplant itself. The wing mainplanes are straight and shoulder-mounted to the fuselage. From the trailing edges the booms take shape and lead to vertical tail fins supporting a single horizontal plane. The fixed tricycle wheeled undercarriage arrangement allows for rough-field operations in both launching and retrieving the air vehicle.
[ 50 Units ] : ZALA Aero Group - Russia
- Reconnaissance (RECCE)
(Showcased structural dimension values pertain to the ZALA 421-20 production model)
265 lb (120 kg)
441 lb (200 kg)
(Showcased weight values pertain to the ZALA 421-20 production model)
1 x Internal combustion engine of unknown make, model and output; driving multi-bladed propeller unit arranged in pusher configuration.
(Showcased powerplant information pertains to the ZALA 421-20 production model)
137 mph (220 kph; 119 kts)
16,404 feet (5,000 m; 3.11 miles)
75 miles (120 km; 65 nm)
(Showcased performance values pertain to the ZALA 421-20 production model; Compare this aircraft entry against any other in our database)
None. Mission payload consisting of various optics and sensor fits to meet mission requirements.
(Showcased armament details pertain to the ZALA 421-20 production model)
Model 421-20 - Base Series Designation
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