INDELA – 9
Robotic airborne reconnaissance complex
Description
«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;
Information from UAV board is transmitted through a radio channel to the ground control station and is additionally recorded to the black box.
«INDELA-9» with airframe hull made of composition materials is intended for multiple use. Autonomous and radio-adjusted methods of performing of a flight task can be used.
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 | |
«INDELA-9» uses a gyro-stabilized optoelectronic system with an infrared camera and integrated laser range finder. Biaxial gyro-stabilized and completely integrated direct-drive suspension system.
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