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