«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
