Detail Information |
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Wingspan: | 1600mm | Folded Size: | 670mm*670mm*250mm |
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Speed: | 22m/s | Max. flight Altitude: | 5000m |
Control Mode: | Manual/Automatic | Max. Takeoff Weigh: | 19.5 Kgs |
Working Temperature: | -10℃-60℃ | Battery Life: | ≥30 Min. With Full Load |
High Light: |
CCC Multi-Rotor Detection Drone, Light-Duty Detection Drone, NFPA Multi-Rotor Detection Drone |
Product Description
1. Product Introduction of Light-Duty Multi-Rotor Detection Drone
- The “S1600” unmanned aerial vehicle is composed of rotor frame, flight control, motor, ESC, battery pack, etc. The fuselage structure of the unmanned aerial vehicle is made of carbon fiber materials. The frame, support arm, landing gear, motor frame, etc. are all designed with light and strong structure, and the arm is composed of ESC, motor and propeller.
- “S1600” aerial photography and publicity system is an unmanned aerial vehicle solution for professional aerial photography and publicity lighting. It perfectly matches the brushless motor PTZ. The frame has a unique design. The arm has a special quick-release device to quickly disassemble the arm. The propeller also has a foldable module. The two foldable modules can be used together to reduce the space occupied by the aircraft by more than half, making transportation and carrying more Convenience. The center frame circuit, arm, and ESC all adopt highly integrated design, making the installation and debugging process of the whole set of equipment simple and quick. The electronic governor and the connection lines are embedded in the center plate and the arm. The highly integrated design makes the circuit clear and clear, and the overall appearance of the body is simple and generous. The main material of the fuselage is carbon fiber, which has the characteristics of long life, light weight and strong rigidity. It has high autonomous flight ability and is suitable for high speed and long endurance operations. It can be equipped with different industry platforms such as visible light pod and infrared heat. Imagers, etc., can be equipped with real-time image transmission and ground station to process information in real time and return records.
2. Technical Parameters
Model | S1600 | |
Main Parameter |
Diagonal wheelbase | 1600mm |
Folded size | 670mm*670mm*250mm | |
Max. horizontal flight speed | 22m/s | |
Max. flight altitude | 5000m | |
Satellite positioning module | GPS,BEIDOU | |
GPS hovering accuracy | vertical ±1m, horizontal ±2m | |
Control mod | manual/automatic | |
Security Mechanism |
Support low battery return and control signal loss return |
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Battery Life |
≥60min(Empty) ≥30min(Full load with 5KG) |
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Wind resistance | 6 Level | |
Takeoff weight | 14.5KG | |
Max. Takeoff weight | 19.5kg | |
Number of flight batteries | 2pcs | |
Working temperature | -10℃-60℃ | |
Working environment | Sunny day and Rainy | |
Compatible mount |
Megaphone | |
Flashlight | ||
30x zoom HD PTZ | ||
Gas detector |