Aircraft Parameters |
|
|
38 kg (without battery) |
|
50 kg (with battery) |
Max Takeoff Weight[1] |
Max takeoff weight for spraying: 90 kg (at sea level) |
|
Maximum takeoff weight for spreading: 101 kg (at sea level) |
Max Diagonal Wheelbase |
2184 mm |
Dimensions |
2800 mm × 3150 mm × 780 mm (arms & propellers unfolded) |
|
1590 mm × 1930 mm × 780 mm (arms unfolded, propellers folded) |
|
1125 mm × 750 mm × 850 mm (arms folded) |
Hovering Accuracy Range (with strong GNSS signal) |
RTK positioning enabled: ±10 cm horizontal, ±10 cm vertical |
|
RTK positioning disabled: ±60 cm horizontal and ±30 cm vertical (radar enabled: ±10 cm) |
RTK/GNSS Operating Frequency |
RTK: GPS L1/L2, GLONASS F1/F2, BeiDou B1/B2, Galileo E1/E5 |
|
GNSS: GPS L1, GLONASS F1, Galileo E1, BeiDou B1 |
Hovering Time[2] |
Hovering without payload: 18 min (@30000 mAh & takeoff weight 50 kg) |
|
Hovering and spraying with full payload: 7 min (@30000 mAh & takeoff weight 90 kg) |
|
Hovering and speading with full payload: 6 min (@30000 mAh & takeoff weight 101 kg) |
Max flight radius can be set |
2000 m |
Max Wind Resistance |
6 m/s |
Propulsion System - Motor |
|
100×33 mm |
Motor KV Value |
48 RPM/V |
Motor Power |
4000 W/rotor |
Propulsion System - Propeller |
|
54 inch |
Rotor Quantity |
8 |
Dual Atomized Spraying System - Operation Box |
|
Full load 40 L |
Operating Payload |
Full load 40 kg |
Dual Atomized Spraying System - Sprinkler |
|
LX8060SZ |
Sprinkler Quantity |
2 |
Droplet Size |
50-300 μm |
Max Effective Spray Width[3] |
11 m (relative operating altitude 2.5 m, flight speed 7 m/s) |
Dual Atomized Spraying System - Water Pump |
|
Magnetic Drive Impeller Pump |
Max Flow Rate |
6 L/min*2 |
T40 Spreading System |
|
Solid dry particles with a diameter of 0.5 to 5 mm |
Spread Tank Volume |
70 L |
Spread Tank Internal Load |
50 kg[1] |
Spread Width of Spreading System[4] |
7 m |
Recommended Operating Temperature |
0°C to 40°C (32°F to 104°F) |
Active Phased Array Omnidirectional Radar |
|
RD2484R |
Terrain Follow |
Max incline: 30° |
Obstacle Avoidance[5] |
Sensible distance (horizontal): 1.5-50 m |
|
FOV: 360° horizontal, ±45° vertical |
|
Operating conditions: Flying higher than 1.5 m over the obstacle at a speed not exceeding 7 m/s |
|
Safe distance: 2.5 m (distance between the propeller tip and obstacle when the aircraft is hovering after braking) |
|
Sensing direction: horizontal omnidirectional avoidance |
|
Sensible distance (above): 1.5-30 m |
|
FOV: 45° |
|
Operating conditions: Available during takeoff, landing, and ascending when an obstacle is more than 1.5 m above the aircraft |
|
Safe distance: 2.5 m (distance between the top of the aircraft and the obstacle when the aircraft is hovering after braking) |
|
Sensing direction: Upward |
Active Phased Array Backward and Downward Radar |
|
RD2484B |
Altitude Detection[5] |
Within the altitude detection range: 1-45 m |
|
Fixed altitude range: 1.5-30 m |
Rear Obstacle Avoidance[5] |
Sensible distance (rear): 1.5-30 m |
|
FOV: ±60° horizontal, ±25° vertical |
|
Operating conditions: Available during takeoff, landing, and ascending when an obstacle is more than 1.5 m behind the aircraft and the flight speed does not exceed 7 m/s |
|
Safe distance: 2.5 m (distance between the propeller tip and obstacle when the aircraft is hovering after braking) |
|
Sensing direction: backward |
Binocular Vision System |
|
0.4-25 m |
Effective Sensing Speed |
≤7 m/s |
FOV |
Horizontal: 90; Vertical: 106° |
Work Environment Requirements |
Normal lighting with clearly textured surfaces |
Intelligent Remote Controller |
O3 Pro Operating Frequency[6]
|
2.4000 to 2.4835 GHz |
|
5.725 to 5.850 GHz |
O3 Pro Signal Effective Distance |
SRRC: 5 km |
|
MIC/KCC/CE: 4 km |
|
FCC: 7 km |
|
(aircraft altitude at 2.5 m in an unobstructed environment with no interference) |
Wi-Fi Protocol |
WIFI 6 |
Wi-Fi Operating Frequency[6] |
2.4000 to 2.4835 GHz |
|
5.150 to 5.250 GHz |
|
5.725 to 5.850 GHz |
Bluetooth Protocol |
Bluetooth 5.1 |
Bluetooth Operating Frequency |
2.4000-2.4835 GHz |
Location |
GPS + Galileo + BeiDou |
Display Screens |
7.02-inch touch LCD with 1920*1200 resolution and 1200cd/m brightness2 |
Supported Aircraft |
AGRAS T40, AGRAS T20P |
Operating temperature |
-20°C to 50°C (-4°F to 122°F) |
Storage Temperature Range |
-30°C to 45°C (within one month) |
|
-30°C to 35°C (between one month and three months) |
|
-30°C to 30°C (between three months and one year) |
Charging Temperature |
5° to 40°C (41° to 104°F) |
Internal Battery Life |
3.3 hours |
External Battery Life |
2.7 hours |
Charging Type |
Use a USB-C charger with a maximum rated power and voltage of 65 W and 20 V. The DJI Portable Charger is recommended. |
Charging Time |
Two hours for both internal and internal plus external batteries (to use the official charging method when the aircraft is off) |
T40 Intelligent Flight Battery |
|
BAX601-30000mAh-52.22V |
Weight |
Approx. 12 kg |
Capacity |
30000 mAh |
Voltage |
52.22 V |
D12000iE Multifunctional Inverter Generator |
|
DC charging output 42-59.92V/9000W |
|
Power supply for air-cooled heat sink 12 V/6 A |
|
AC output 230V/1500W or 120V/750W[7] |
Battery Charging Time |
To fully charge one battery (T40 battery) takes 9-12 mins |
Fuel Tank Capacity |
30 L |
Starting Method |
Starting the Generator via the One-Button Start Switch |
Max Power of Engine |
12000 W |
Fuel Type |
Unleaded gasoline with RON ≥91 (AKI ≥87) and alcohol content less than 10% |
|
(*Brazil: unleaded gasoline with RON ≥ 91 and alcohol content of 27%) |
Reference Fuel Consumption[8] |
500 ml/kWh |
Engine Oil Model |
SJ 10W-40 |