The unmanned aerial vehicles INDELA-I.N.SKY of a medium operating radius is designed to fulfill a wide range of practical tasks:
- twenty-four-hour monitoring of specified territories, water surfaces, industrial projects, vehicles, boats, yachts, ships, groups of people, individuals etc.;
- real-time video and infra-red information transmission to the ground control station at a distance of up to 50 km within line of sight from a ground control station during 5 hours;
The construction of INDELA-I.N.SKY UAV, at the customer's option, allows installing additional equipment into the payload compartment, which expands range of application of the complex for other tasks. The UAV construction allows building up flight and navigation equipment and installation of different variations of payload. Ground control station (GCS) includes all the necessary components for flight programmed control and real time equipment diagnostics. The helicopter is based on a classic single-rotor scheme with a tail rotor.
General specifications
Engine rotory-piston engine
Takeoff power kW 26
Fuel consumption kg/h 5-8
Key geometric characteristics
Length Nose to Tail mm 3052
Main rotor diameter mm 3168
Height mm 1346
Wheelbase mm 1180
Weight data
Maximum takeoff weight kg 140
Weight kg 90
Fuel-carrying capacity kg 25
Payload weight, kg kg 25
Basic flight characteristics
Cruising speed at ground level km/h 70
Static ceiling m 1500
Maximal vertical speed m/s 5
Flight duration (100-500 m high) h up to 5
Wind (takeoff and landing) m/s 10
Operating temperature С -35 … +55
