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Minimum quantity for "AVINA SOFTWING UAS SYSTEM" is 1.

Avina was designed with high value payloads in mind. This aircraft is intended to provide an open and customizable UAV platform for ISR missions, systems testing and large payload. This gives the Avina both efficiency and reliability at high altitudes. The Avina is also equipped with an on-board electrical generator that allows customers to provide power to their equipment without the need to add batteries. The Avina utilizes a high Efficiency soft-wing to achieve both long duration flights and high aerodynamic efficiency. the Avina can be programmed for auto take-off, auto-pilot flight patterns, and auto landing at the end of the mission.

Carbon Fiber Frame
3120 mm
Empty weight: 400 lbs
Powerplant: 1 x Rotary Engine
Fuel Cap: 12 gal
Maximum speed: 75 mph
Range: 820 mi
Endurance: 6 hours
Service Ceiling: 11,000 ft
Payload: 800 lbs


• Applications: Mapping, Photography and Aerial Surveillance EO/IR.
• Wingspan: 2121 mm
• Length: 3120 mm
• Height: 1744 mm
• Empty weight: 400 Lbs
• Max Takeoff Weight: 1200 Lbs
• Powerplant:
1 x Rotary Engine ( Diesel JP-4) 278 hp (207 kW)
• Fuel Cap: 12 Gal
• Maximum speed: 75 mph
• Range: 820 mi
• Endurance: 6 Hours
• Service Ceiling: 11,000 ft (3352.8 m)
• Rate of Climb: 1000 ft/min at Gross
• Payload: 800 Lbs


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