GSA-300 VTOL Drone
GSA-300 VTOL Drone
Dronepoulis GSA-300 is a 2.7 m wingspan aerodynamically optimized UAV. It uses electric powered motors for take-off and landing and does not require a runway or catapult. It is a composite airframe with 2 kg payload capacity, powered by a petrol engine for forward flight. The low fuel consumption enables a safe endurance of 5 hours. The GSA-300 can take-off from any surface and land on a 3×3 m surface with high accuracy.
The UAV has a 17 kg MTOW (including payload). It can be operated by just two people. Flight missions are carried out fully autonomous!
The GSA-300 uses separate communication systems for datalink and video-link. The systems operate at different frequencies to increase redundancy. It is also possible to add Satellite communication. The video-link can use 256 bit AES encryption in order to secure the data transferred.
Technical Specifications
- Fully autonomous
- Capable of outdoor flights in harsh environment
- Capable to taking-off and landing vertically while flying horizontally
- 5 hours endurance
- Flight time (endurance) of up to 5 hours
- 2 kg payload
- 3000 m AMSL. max. altitude
- Optionally EFI engine
- 60 km/hr cruise speed
- 90 km/hr maximum speed
- 17 kg Maximum Take-off Weight
- 80-100W onboard power generation
- Fixed wing VTOL drone
- Capable of outdoor flights in harsh environment (wind up to 40 km/hr)
- Great endurance and great stability in high, turbulent winds
- Specifically designed for long-endurance stable flight
- Extensively used for surveillance and reconnaissance
- Can also be used for live video surveillance and monitoring of infrastructure
- Various payloads can be seamlessly integrated and used with this drone
- 61 MP Sony high resolution visual camera
- Multispectral cameras
- EO/IR and thermal cameras (EO 1080p 30x zoom, TiR 640x512)
- Lidar
- Laser Range Finder (LRF)
- Laser Designator
Specifications
- Endurance – up to 5 hours
- Speed – 60 km/h
- Radio link range – 100 km
- Video transmission range – up to 50 km
- Max flight range – 300 km
- Max payload weight – up to 2 kg
- Altitude – 3000 m AGL
Take-off and Landing Requirements
- Autonomous vertical take-off using vertical lift motor-propellers
- Autonomous landing using vertical lift motor-propellers on fixed undercarriage
Operational conditions
- Wind gusts: up to 40 km/hr
- Operational temperature: from -5°С to +65°С
Payload options
- 42/61 MP Sony full frame photogrammetry camera
- Electro optical and thermal infrared camera
- Multispectral camera
- Lidar
- Laser Range Finder (LRF)
- Laser Designator
- Other types of payloads can also be integrated
