| Aircraft | |
| Weight for spraying standard with two nozzles | 75 kg |
| Weight for spraying optional with four nozzles | 77 kg |
| Weight for spreading equipped with spreading system | 75 kg |
| Weight for lifting equipped with lifting system | 65 kg |
| Weight for lifting equipped with dual battery lifting system | 90 kg |
| Max takeoff weight for spraying standard with two nozzles | 175 kg |
| Max takeoff weight for spraying optional with four nozzles | 177 kg |
| Max takeoff weight for spreading equipped with spreading system | 175 kg |
| Max takeoff weight for lifting equipped with lifting system | 165 kg |
| Max takeoff weight for lifting equipped with dual battery lifting system | 170 kg |
| Max diagonal wheelbase | 2330 mm (diagonal) |
| Dimensions arms and propellers unfolded | 3220 mm × 3224 mm × 975 mm |
| Dimensions arms unfolded propellers folded | 1820 mm × 1840 mm × 975 mm |
| Dimensions arms and propellers folded | 1105 mm × 1265 mm × 975 mm |
| Hovering accuracy range with strong GNSS signal RTK enabled | ±10 cm horizontal, ±10 cm vertical |
| Hovering accuracy range with strong GNSS signal RTK not enabled | Horizontal ±0.6 m, vertical ±0.3 m |
| Max configurable flight radius | 2 km |
| Operating temperature | 0 °C to 40 °C |
| Max wind resistance | Less than 6 m per second |
| Propulsion System | |
| Motor stator size | 155 × 16 mm |
| Motor KV | 60 rpm per volt |
| Propeller material | Carbon fiber composite |
| Propeller dimensions | 62 inches |
| Propeller quantity | Eight pairs |
| Spraying System | |
| Model | LS100 |
| Dimensions spray rod folded | 880 mm × 870 mm × 810 mm |
| Dimensions spray rod unfolded | 1020 mm × 1930 mm × 810 mm |
| Spray tank material | HDPE |
| Spray tank volume | 100 L |
| Operating payload | 100 kg |
| Sprinkler model standard nozzle and optional mist nozzle | LX07550SX standard / LX09550SX optional |
| Sprinkler quantity standard optional | Two standard, four optional |
| Nozzle distance two nozzles four nozzles outermost | 1834 mm |
| Droplet size | 50 to 500 micrometers |
| Effective spray width | 5 to 13 meters |
| Delivery pump type | Impeller pump with magnetic drive |
| Delivery pump quantity | Two |
| Max flow rate | 30 L per minute standard two nozzles, 40 L per minute optional four nozzles |
| Spreading System | |
| Spreading system dimensions | 900 mm × 820 mm × 920 mm |
| Compatible material diameter extra large auger standard | 0.5 mm to 10 mm |
| Compatible material diameter medium auger standard | 4 mm to 6 mm |
| Compatible material diameter large auger optional | 4 mm to 10 mm |
| Compatible material diameter small auger optional | 0.5 mm to 4 mm |
| Spreading tank volume | 150 L |
| Spreader structure type | Centrifugal disc |
| Discharge structure type | Screw feeder feeding |
| Max discharge rate compound fertilizer | 400 kg per minute |
| Max load inside the spreading operation box | 100 kg |
| Effective spreading width | 3 to 10 meters |
| Lifting System | |
| Load capacity | 100 kg |
| Lifting cable length standard configuration | 10 meters |
| Recommended cable length | 10 to 15 meters |
| Operating temperature | 0 °C to 40 °C |
| Dual battery lifting system load capacity | 80 kg |
| Dual battery lifting system dimensions | 805 mm × 960 mm × 669 mm |
| Emergency escape mode | Cable fuse disconnection and escape |
| Safety System 3.0 | |
| Millimeter wave radar EIRP | Less than 20 dBm |
| Safety system operating temperature | 0 °C to 40 °C |
| Operating environment requirement | Adequate light and discernible surroundings |
| Field of view laser radar | Vertical 272 degrees, Horizontal 60 degrees |
| Field of view front radar | Horizontal 360 degrees, Vertical plus or minus 45 degrees |
| Field of view downward radar | Left and right plus or minus 12.5 degrees, front and back plus or minus 22.5 degrees |
| Field of view rear radar | Left and right plus or minus 45 degrees, front and back plus or minus 45 degrees |
| Quad vision system field of view | Horizontal 360 degrees, Vertical 180 degrees |
| FPV camera field of view | Horizontal plus or minus 86 degrees, Vertical 108 degrees |
| Measurement range | Up to 60 meters |
| Effective safe obstacle avoidance speed | Up to 13.8 meters per second |
| Effective obstacle avoidance height | 1.5 meters or greater |
| Remote Controller | |
| Model | TKPL 2 |
| Screen | 7 inch LCD touchscreen, 1920 × 1200 resolution, 1400 cd per m squared brightness |
| Storage temperature less than one month | Minus 30 to 45 degrees Celsius |
| Storage temperature one to three months | Minus 30 to 35 degrees Celsius |
| Storage temperature three months to one year | Minus 30 to 30 degrees Celsius |
| Charging temperature | 5 to 40 degrees Celsius |
| Internal battery runtime | 3.8 hours |
| External battery runtime | 3.2 hours |
| Batteries and Chargers | |
| DB2160 intelligent flight battery weight | 14.7 ± 0.3 kg |
| DB2160 capacity | 41,000 mAh |
| DB2160 nominal voltage | 52 V |
| DB2160 recharge time 30 to 95 percent | 8 to 9 minutes |
| C12000 smart charger model | CSX901-12000 |
| C12000 dimensions | 456 mm × 291 mm × 107 mm |
| C12000 weight | 13.13 kg |
| C12000 input voltage | Three phase AC 175 to 520 V, single phase AC 200 to 264 V |
| C12000 output voltage | 62 V |
| C12000 rated power | 12,000 W three phase input, 3,000 W single phase input |
| C12000 recharge time 30 to 95 percent | 8 to 9 minutes |
| Generator | |
| D14000iE multifunctional inverter generator output channels | DC recharge output 42 to 61.6 V at 11,500 W, air cooled radiator charge 12 V at 6 A, AC output 220 V at 1500 W |
| Generator recharge time DB2160 30 to 95 percent | 8 to 9 minutes |
| Generator fuel tank capacity | 30 L |
| Generator starting method | One button start switch |
| Generator compatible battery | DB1580 and DB2160 intelligent flight batteries |
| Relay | |
| Relay dimensions without antenna | 112 mm × 112 mm × 51 mm |
| Relay dimensions with antenna | 120 mm × 112 mm × 101 mm |
| Relay weight | 630 g |
| Relay effective signal range | 5 km SRRC, 4 km MIC KCC CE, 8 km FCC in interference free unobstructed environment at 2.5 m flight altitude |
| D RTK 3 AG | |
| Supported satellite systems | GPS L1 L2 L5, BeiDou B1I B2I B3I B1C B2A B2B, Galileo E1 E5a E5b E6, GLONASS G1 G2, QZSS L1CA L2C L5, L BAND |
| D RTK dimensions | 345 mm × 244 mm × 300 mm |
| D RTK weight | 3.77 kg including packaging |
| D RTK effective signal range FCC | 15 km |
| D RTK effective signal range SRRC | 12 km |
| D RTK effective signal range CE JP | 8 km |
| Positioning Accuracy | |
| PPP satellite based service convergence time | 20 minutes |
| PPP horizontal accuracy | 30 cm RMS |
| PPP elevation accuracy | 40 cm RMS |
| Network RTK calibration horizontal | 0.8 cm plus 1 ppm RMS |
| Network RTK calibration vertical | 1.5 cm plus 1 ppm RMS |
| Footnotes | |
| [1] Measured at sea level. The DJI Agriculture App will recommend loading weight based on aircraft status environment conditions and tasks. Do not exceed recommended maximum loading weight. In Australia follow local regulations and keep maximum takeoff weight at 149.9 kg. [2] The effective spray width depends on the actual working scene. [3] Working height is 3 m disc rotation speed 1100 rpm uniformity requirement CV less than 30 percent measured broadcast width is 10 m. Faster disc rotation higher flight altitude increase broadcast width. [4] Includes weight of ropes and hooks. Measured at sea level the DJI Agriculture App will recommend loading weight based on aircraft state environment conditions and tasks. Do not exceed recommended values. [5] Effective working range of sensing distance obstacle avoidance and bypassing may vary due to lighting rain fog and object material location and shape. Downward sensing assists terrain following altitude flight. Sensing in other directions is for obstacle avoidance. For linear obstacles mark them as obstacles otherwise bypass failure is user's responsibility. [6] Sea level height environmental temperature between 15 and 40 degrees Celsius time to charge battery from 30 percent to 95 percent. Fast charging supported when cell temperature is within 15 to 75 degrees Celsius. Charging time varies with input power altitude initial charge level and other factors. [7] Positioning accuracy and reliability are affected by equipment tilt signal obstruction multipath number of satellites geometry and atmosphere. Set up equipment in open scenes away from electromagnetic interference and multipath environments. |
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