Description

«INDELA-6M» 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;

- video information about use of main traffic arteries;

- carrying out of prospecting works;

- aerial mapping;

Characteristics

Engine Two-cycle, two-cylinder, opposite, of internal combustion

Statistical traction N 161

Volumetric capacity cm3 56

Engine power KW 4,0

Hourly fuel consumption at V econom. l/h 0,68

Parachute rescue system is designed for emergency landing

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 2693

Span of wings mm 6012

Wing load g/dm² 235

Weight data

Takeoff mass kg 35

Standard fuel margin l 7

Basic flight characteristics

Range of horizontal flight speed km/h 65-140

Cruise speed km/h 80

Takeoff speed km/h 67

Landing speed at glide path with extended flaps km/h 55

Planner’s quality 13,63

Contact velocity km/h 60

Flight attitude range m 50-3000

Practical flight length km 440

Flight duration h 5

Control

Flight control Automatic/dual

Communication range (within line of sight) up to 50 km (video channel)

Communication range (within line of sight) up to 100 km (telemetry)

Control system Autonomous navigation, automatic performance of the flight task, automatic performance of procedures in case of loss of contact/accident, automatic waiting for commands, continuous/on request telemetry