| Aircraft Parameters | |
|---|---|
| Total weight | 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 x 3150 mm x 780 mm (arms & propellers unfolded) 1590 mm x 1930 mm x 780 mm (arms unfolded, propellers folded) 1125 mm x 750 mm x 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 | |
| Stator Size | 100 x 33 mm |
| Motor KV Value | 48 RPM/V |
| Motor Power | 4000 W/rotor |
| Propulsion System - Propeller | |
| Diameter | 54 inch |
| Rotor Quantity | 8 |
| Dual Atomized Spraying System - Operation Box | |
| Operation Box Capacity | Full load 40 L |
| Operating Payload | Full load 40 kg[1] |
| Dual Atomized Spraying System - Sprinkler | |
| Sprinkler Model | 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 | |
| Pump Model | Magnetic Drive Impeller Pump |
| Max Flow Rate | 6 L/min*2 |
| T40 Spreading System | |
| Applicable Materials | 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 Deg.C to 40 Deg.C (32 Deg.F to 104 Deg.F) |
| Active Phased Array Omnidirectional Radar | |
| Model Number | RD2484R |
| Terrain Follow | Max incline: 30 Deg. |
| Obstacle Avoidance[5] | Sensible distance (horizontal): 1.5-50 m FOV: 360 Deg. horizontal, ±45 Deg. 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 Deg. 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 | |
| Model Number | 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 Deg. horizontal, ±25 Deg. 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 | |
| Measurable Range | 0.4-25 m |
| Effective Sensing Speed | <=7 m/s |
| FOV | Horizontal: 90; Vertical: 106 Deg. |
| 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 Deg.C to 50 Deg.C (-4 Deg.F to 122 Deg.F) |
| Storage Temperature Range | -30 Deg.C to 45 Deg.C (within one month) -30 Deg.C to 35 Deg.C (between one month and three months) -30 Deg.C to 30 Deg.C (between three months and one year) |
| Charging Temperature | 5 Deg. to 40 Deg.C (41 Deg. to 104 Deg.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 | |
| Model | BAX601-30000mAh-52.22V |
| Weight | Approx. 12 kg |
| Capacity | 30000 mAh |
| Voltage | 52.22 V |
| D12000iE Multifunctional Inverter Generator | |
| Output Channel | 1. DC charging output 42-59.92V/9000W 2.Power supply for air-cooled heat sink 12 V/6 A 3.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 |
| Definition | |
| The terms HDMI, HDMI High-Definition Multimedia Interface, HDMI Trade dress and the HDMI Logos are trademarks or registered trademarks of HDMI Licensing Administrator, Inc. | |
|
Data source |
https://www.dji.com/t40/specs |
Generated using dronespec.info
Source data acquired 2023-01-23 19:03:44