Aircraft |
| Weight | 42.5 kg (without battery)
65 kg (with two DB2000 batteries) |
| Max Takeoff Weight | 95 kg (with cargo at sea level) |
| Max Diagonal Wheelbase | 2200 mm |
| Dimensions (L x W x H) | Arms unfolded, propellers folded: 1590 x 1900 x 947 mm
Arms & propellers unfolded: 2800 x 3085 x 947 mm
Arms & propellers folded: 1115 x 760 x 1027 mm |
| Folding Method | Towards body |
| Loadable Battery Quantity | 2 |
| Hovering Endurance (empty weight, with max battery capacity) | 29 mins (dual battery mode)
15 mins (single battery mode)
*The data was collected in controlled conditions: Zero altitude and a windless environment. For reference only. |
| Hovering Endurance (max weight, with max battery capacity) | 18 mins (30 kg weight load, dual battery mode)
8 mins (40 kg weight load, single battery mode)
*The data was collected in controlled conditions: Zero altitude and a windless environment. For reference only. |
| Max Flight Distance (empty weight, with max battery capacity) | 28 km (dual battery mode)
12 km (single battery mode)
*The data was collected in controlled conditions: Zero altitude and windless environment, at a constant speed of 15m/s. For reference only. |
| Max Flight Distance (max weight, with max battery capacity) | 16 km (30 kg weight load, dual battery mode)
8 km (40 kg weight load, single battery mode)
*The data was collected in controlled conditions: Zero altitude and windless environment, at a constant speed of 15 m/s. For reference only. |
| Max Flight Time (max weight, with max battery capacity) | 18 mins (30 kg weight load, dual battery mode)
9 mins (40 kg weight load, single battery mode)
*The data was collected in controlled conditions: Zero altitude and a windless environment, at a constant speed of 15 m/s. For reference only. |
| Operating Temperature | -20¡ãC to 45¡ãC |
| Ingress Protection Rating | IP55 |
| Hovering Accuracy (with strong GNSS signal) | RTK positioning enabled: ¡À10 cm horizontal, ¡À10 cm vertical
RTK positioning disabled: ¡À60 cm horizontal and ¡À30 cm vertical (radar enabled: ¡À10 cm) |
| RTK/GNSS Operating Frequency | RTK: GPS L1/L2, Galileo F1/F2, BeiDou B1I/B2I/B3I, Galieo E1/E5b, QZSS L1/L2
GNSS: GPS L1, BeiDou B1I, Galileo F1, Galieo E1, QZSS L1 |
| Max Pitch Angle | 30¡ã |
| Max Ascent Speed | 5 m/s
*The data was collected in controlled conditions: zero altitude and a windless environment, with a 30 kg payload. For reference only. |
| Max Descent Speed | 3 m/s (vertical)
5 m/s (tilted)
*The data was collected in controlled conditions: Zero altitude and a windless environment, with a 30 kg payload. For reference only. |
| Max Horizontal Speed | 20 m/s
*The data was collected in controlled conditions: Zero altitude and a windless environment, with a 30 kg payload, for reference only. |
| Max Flight Altitude | 6000 m (without payload) |
| Max Wind Speed Resistance | 12 m/s
*The data was collected in controlled conditions: zero altitude and a windless environment, with a 30 kg payload. For reference only. |
Propulsion System |
| Stator Size | 100 x 33 mm |
| Motor KV Value | 48 rpm/V |
| Max Motor Power | 4000 W/rotor |
| Propellers Material | Carbon fiber composite |
| Propellers Diameter | 54 inch |
| Propellers Type | Foldable double-blade propellers |
| Main-rotor Diameter | 1375 mm |
| Rotor Quantity | 8 |
| LED Light |
| Effective Illumination Distance | 10m |
| Illumination Mode | 60 Hz, automatically switch on according to ambient light |
DJI O3 Image Transmission |
| Model | Pigeon (with DDR)-2T4R |
| Signal Effective Distance | 20 km (FCC) 8 km (CE/SRRC/MIC)
*Measured with FCC compliance in unobstructed environments with typical interference. Data is for reference only. The actual transmission distance may vary depending on the environment's obstruction and interference conditions. Please pay attention to reminders in the app. |
| O3 Operating Frequency | 2.4000 to 2.4835 GHz
5.725 to 5.850 GHz
*Some countries or regions do not support the 5.8 GHz frequency band. Please refer to local flight laws and regulations for details. |
| EIRP | 2.400 GHz - 2.4835 GHz:
<33 dBm (FCC)
<20 dBm (CE/SRRC/MIC)
5.725 GHz - 5.850 GHz:
<33 dBm (FCC)
<30 dBm (SRRC)
<14 dBm (CE) |
| Data Security | AES-256 |
| ADS-B | Supported |
Forward and Backward Active Phased Array Radar |
| Model Number | RD241608RF (forward)
RD241608RB (backward) |
| Altitude Detection | Fixed altitude range: 1.5-200 m |
| Rear Obstacle Avoidance | Sensible distance (rear): 1.5-50m.
FOV Forward: 360¡ã horizontal, ¡À45¡ã vertical£¬¡À45¡ãupward; Backward: ¡À45¡ã horizontal, 360¡ã vertical.
Operating conditions: Available during takeoff, landing, and ascending when an obstacle is more than 1.5 m away from the aircraft.
Safe distance: 3.5 m (distance between the propeller tip and obstacle when the aircraft is hovering after braking).
Sensing direction: Multi-direction. |
Binocular Vision System |
| FOV | Horizontal: 90; Vertical: 106¡ã |
| Work Environment Requirements | Normal lighting with clearly textured surfaces |
