Development
Applications

ACCUAV MUQ777E-CF

Design CriterionDesign Parameter
ConfigurationQuadcopter (4 arms)
Span777mm
Propulsion SystemLiPo Battery powering 4 electric motor
MaterialCarbon Fibre 
Weight with Payload4kg
Flight endurance (with payload)Approx. 20min
Fly optionsManual, GPS aided, Autonomous
Flying heightUpto 1km
Telemetry Range20km

ACCUAV MUH1150E-CF

Design Criterion Design Parameter
Configuration Hexacopter (6 arms)
Span 1150mm
Propulsion System LiPo Battery powering to 6 electric motor
Material Carbon Fibre
Frame weight 5kg
Max Payload 3kg
Flight endurance (with max payload) Approx. 45min
Fly options Manual, GPS aided, Autonomous
Flying height Upto 1km
Telemetry Range 20km

ACCUAV FW2000E-EP

Design Criterion Design Parameter
Configuration Flying Wing
Span 2000mm
Propulsion System LiPo Battery with one electric motor
Material EPP foam
Frame Weight 4kg
Payload capacity Upto 1kg
Flight endurance (with payload) Approx. 1 hour
Fly options Manual, GPS aided, Autonomous
Flying height Upto 1km
Telemetry Range 20km

Kakillakale Tea Plantation

Matara Paddy Field

Firing Range 300m