Product overview
The DJI T200 is an agricultural lifting aircraft with a maximum single-aircraft payload of 200 kg in either its two-battery or four-battery operating mode. Two aircraft can work cooperatively under one person's control, with a maximum cooperative payload of 360 kg. These configurations provide distinct lifting arrangements: the cooperative rating applies to two aircraft together, while the 200 kg rating applies to one aircraft. Its battery specification is 46 Ah, accompanied by a stated fast-charging time of 7–8 minutes.
The physical architecture combines upper and lower motors on a common axis, with maximum thrust of 183 kg per axis. A 120 V electrical platform powers flat-wire motors with a stated 41% increase in slot fill factor. The 68-inch carbon-fiber propellers have straight-locking structures fitted as standard to both upper and lower blades to reduce vibration. Integrated equipment also includes an intelligent safety system with 11 sensors and O4 video transmission using eight antennas, supporting the aircraft's agricultural lifting role.
Specifications
| Specification | Value & conditions |
|---|---|
| Manufacturer and model | DJI T200 agricultural UAV |
| Maximum payload | 200 kgSingle-aircraft operation; supported in both two-battery and four-battery modes. |
| Maximum cooperative payload | 360 kgTwo-aircraft cooperative operation. |
| Operator requirement | One person can control cooperative operation.Two-aircraft cooperative operation. |
| Battery configurations | Two-battery and four-battery modes |
| Battery capacity | 46 Ah |
| Charging time | 7–8 minutesFast charging. |
| Sensor count | 11 sensorsNew-generation intelligent safety system. |
| Video transmission | O4 video transmission with 8 antennas |
| Electrical platform | 120 V high-voltage platform |
| Motor construction | Flat-wire motors |
| Slot fill factor increase | 41%Flat-wire motor design. |
| Propeller size and material | 68-inch carbon-fiber propellers |
| Propeller locking equipment | Straight-locking structures on both upper and lower propellersUpper and lower propellers; standard equipment. |
| Propulsion architecture | Coaxial upper and lower dual-motor arrangement |
| Maximum thrust | 183 kgPer propulsion axis. |
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