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ZALA 421-21 Russian Micro Unmanned Aerial Vehicle (UAV)

ZALA

Tactical Unmanned Aerial Vehicle (UAV)
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Basic Information
Name
ZALA 421-21 Russian Micro Unmanned Aerial Vehicle (UAV)
Designation
ZALA
Alternate Designation
Equipment Type
Tactical Unmanned Aerial Vehicle (UAV)
Manufacturer
ZALA AERO
Date of Introduction
2010
Description

On Tuesday 8st June 2010 ZALA AERO officially launched its new ZALA 421-21 with its unique six-rotor design. The unmanned complex based on the helicopter UAV ZALA 421-21 is designed for remote landing and monitoring at altitude 10-1000m at a distance of 5km from the ground control station with a maximum endurance of 25 minutes. The unique design permits the UAV to be extremely quiet in any environment. UAV transmits real-time video and photographs. The UAV is fully autonomous which requires minimal operator input for any mission and semi-autonomous without GPS mode is available for use inside buildings. The UAV can land on structures to preserve power while still monitoring and listening in on the target. Easy application and transportations are key elements that this platform offers. The payload capacity of 0.5 kilograms offers the VTOL ability to integrate payloads of small UAVs but at a much closer range and zero movements. Infrared payloads are currently being implemented for nighttime reconnaissance. Future developments are being focused on increasing endurance to around 40 minutes and increasing the range to around 15km. Payload modifications include combining day video cameras and infrared cameras for multi-purpose missions. The new model is due to be released before the end of the year.

Air & Air Defense Specifications
Max Speed 40.0 km/h
Range 15.0 km
System
Alternative designations ZALA 421-21
Type Micro Unmanned Aerial Vehicle (UAV)
Ground Crew Two, backpack
Engine Electric, battery powered
Propulsion 6-two blade propeller, Vertical Take-Off and Landing (VTOL)
Max Payload Takeoff weight 0.5 kg
Ceiling, Operational 10-1,000 m
Endurance 130 min
Range 15 km
Launch Method Hand Launched
Wind speed at launch INA
Recovery Method Two fixed, skid landing gear
Launcher (1x) (optional)
Speed
Maximum (level) 40 km/h
Dimensions (cm)
Wing Span INA, See picture for est. scale
Length (fuselage) INA
Height INA
Payload Types
Description All imagery is real-time transfer to ground control
Photo camera Single frame photo (color)
Color Video Camera INA
Infrared Camera (Optional) INA
System Components
Number of UAVs (2 X) UAVs
Number of transport cases (2x) transport cases
Ground Control Station (GCS) (1x) hand-held, ruggedized
GCS Power Supply Independent 6 hour battery
Setup Time 5-10 min.
Control Capability UAV and payload controlled independently by GCS
Roll-stabilized cameras (2x) Video and photo camera
Infrared Camera (optional) (1X) IR Camera
Notes
Description PAYLOADS FIT IN THE STANDARD MOUNTING BLOCK THAT IS INTERCHANGEABLE WITH OTHER PAYLOADS. MULTI-SINGLE PHOTO/VIDEO/IR CAMERA SENSOR PAYLOAD IN DEVELOPMENT. 12/220 VOLT EXTERNAL CONNECTION FOR OPTIONAL POWER SOURCE FOR THE GCS.
Details
Country of Origin Russia
Category UAVs
Air > UAVs
Filter Label
Z
Classification
Domain
Air & Air Defense
Equipment Status
Active
Operators (1)
Russia
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