Price:Negotiable
Delivery Date:Within 3 days after your order is confirmed

Offer

«INDELA-9» is designed for performance of a wide range of practical tasks:

- monitoring of territories and objects;

- monitoring of power lines;

- control of situation with regard to fire prevention;

- monitoring of ecologic situation;

- video information about use of main traffic arteries;

- carrying out of prospecting works;

- aerial mapping;

Characteristics

Engine Electric engine without the collector

Statistical traction N 226

Engine power KW 12,5

Operating voltage V 45,8

Optionally (internal combustion engine) «INDELA-9»

Engine Two-cylinder, two-cycle, opposite engine

Volumetric capacity cm3 97

Statistical traction N 280

Engine power KW 7,6

Hourly fuel consumption l/h 2,5

Optionally (parachute rescue system is designed for emergency landing, available only with internal combustion engine)

Min. height for activation of the parachute above the level of landing field m 100

Barometric height of location of the area above sea level m up to 2000

Key geometric characteristics

Length mm 3336

Span of wings mm 9100

Weight data

Takeoff mass kg 55

Basic flight characteristics

Range of horizontal flight speed km/h 55-140

Cruise speed km/h 90

Takeoff speed km/h 51

Landing speed at glide path with extended flaps km/h 60

Planner’s quality 18

Flight attitude range m 50-3000

Practical flight length (with electric engine) km 90

Optionally (with internal combustion engine) km 360

Fight duration (with electric engine) h 1,5

Optionally (with internal combustion engine) h 6

Control

Flight control Automatic/dual

Communication range (within line of sight)INDELA-9 with electric engine up to 25 km (video signal)

Communication range (within line of sight)INDELA-9 with electric engine up to 64 km (telemetry)

Communication range (within line of sight)INDELA-9M with internal combustion engine up to 60 km (video channel)

Communication range (within line of sight)INDELA-9M with internal combustion engine up to 100 km (telemetry)

Control system autonomous navigation, automatic performance of the flight task