Maximum Spraying Takeoff Weight: 92 kg (standard configuration with 2 nozzles + 40 L tank, at sea level) Maximum Spraying Takeoff Weight: 103 kg (with optional orchard kit, 2 additional nozzles + 50 L tank, at sea level) Maximum Spreading Takeoff Weight: 103 kg (at sea level)
With RTK Positioning Enabled: Horizontal+10 cm,Vertical+10 cm Without RTK Positioning Enabled: Horizontal: +60 cm, Vertical: +30 cm (with radar function enabled, 10 cm)
1.DC Charging Output:42-59.92V/9000W 2.Air-Cooled Radiator Power Supply:12V/6A 3.AC Output:220V/1500W
Battery Full Charging Time[6]
9-12 minutes per battery(DB1560智能飞行电池)
Fuel Tank Capacity
30 L
Starting Method
One-button start
Engine Maximum Power
12 KW
Fuel Type
92#Gasoline
Reference Fuel Consumption
500 ml/kwh
Engine Oil Specification
SJ10W-40
Power System - Motor
Stator Dimensions
100×33 mm
Motor KV Value
48 rpm/V
Motor Power
4000 W/rotor
Power System - Propeller
Material
Nylon-carbon fiber composite
Blade Size
54 inches
Main Rotor Diameter
8
Number of Rotors
ABS
Active Phased Array Radar System
Model
RD241608RF(Front Phased Array Digital Radar) RD241608RB(Rear Phased Array Digital Radar)
Terrain Following
Maximum Mountain Slope50° Altitude Measurement Range:1-50 m Altitude Hold Range:1.5-30 m
Obstacle Avoidance[4]
Detection Range (Omnidirectional):1-50m Field of View(FOV): Front Phased Array Radar: Horizontal 360°, Vertical +45°, Upward +45° (conical) Rear Phased Array Radar: Vertical 360°, Horizontal +45° Operating Conditions: Aircraft relative altitude >1.5 m Horizontal speed ≤10 m/s Vertical speed ≤3 m/s Safety Distance:2.5m(distance between aircraft and obstacle after braking and stable hovering) Detection Direction:Omnidirectional obstacle sensing