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Description
«H.U.SKY-II» unmanned airborne vehicle of vertical takeoff and landing belongs to the class of light helicopters, which can be used as a carrier included in UAV complex for fulfillment of a wide range of practical tasks:
- monitoring of territories and objects;
- carrying out of prospecting works;
- aerial mapping;
- target designation; protection of transport columns;
Characteristics
Engine two four-cycle, two-cylinder, water-cooled
Takeoff power kW 52
Volume cub.sm 588
Fuel consumption kg/h 5-8
Key geometric characteristics
Length with main rotor mm 5850
Length Nose to Tail mm 4358
Main rotor diameter mm 4800
Height mm 1534
Wheelbase mm 1350
Weight data
Maximum takeoff weight kg 255
Useful load kg 55
Fuel-carrying capacity l 83
Reserve fuel-carrying capacity l 17
Basic flight characteristics
Cruise speed level flight km/h 100
Static ceiling m 2100
Maximal vertical speed m/s 5
Practical flight range km 240
Flight duration (Height 100-500 м) h 5
Wind (takeoff and landing) m/s up to 10