ACCUAV MUQ777E-CF

Design Criterion	Design Parameter
Configuration	Quadcopter (4 arms)
Span	777mm
Propulsion System	LiPo Battery powering 4 electric motor
Material	Carbon Fibre
Weight with Payload	4kg
Flight endurance (with payload)	Approx. 20min
Fly options	Manual, GPS aided, Autonomous
Flying height	Upto 1km
Telemetry Range	20km

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