Technical Characteristics:
DJI Matrice 4T

Mass

Empty Mass

Takeoff Weight:
1229 g*

* The standard weight of the aircraft (including the battery, propellers, and a microSD card). The actual product weight may vary due to differences in batch materials and external factors.

Maximum Take-Off Mass (MTOM)

Max Takeoff Weight:
Standard Propellers: 1420 g
Low-Noise Propellers: 1430 g

Dimensions for Rotorcraft / Multirotor

Length of aircraft body

Dimensions:
Folded: 260.6 x 113.7 x 138.4 mm (L x W x H)
Unfolded: 307.0 x 387.5 x 149.5 mm (L x W x H)

Maximum dimensions excluding propellers.

Diagonal Wheelbase:
438.8 mm

Width of aircraft body

Height of aircraft body

Propeller Dimensions

Propeller Configuration

Centre of Gravity (CG)

N/A

Flight Duration / Endurance

Max Flight Time:
49 min (standard propellers)
46 min (low-noise propellers)

Measured with the aircraft flying at approximately 8 m/s without payloads in a windless environment until the battery level reached 0%. Data is for reference only. Actual usage time may vary depending on the flight mode, accessories, and environment. Please pay attention to reminders in the app.

Maximum Range

Max Flight Distance:
35 km (standard propellers)
32 km (low-noise propellers)

Measured by the aircraft hovering in a windless environment at sea level, from 100% battery level until 0%.

Maximum Operating Height (Service Ceiling)

Maximum Airspeed

Max Horizontal Speed (at sea level, no wind):
21 m/s
21 m/s flying forward, 18 m/s flying backward, 19 m/s flying sideways*

* No faster than 19 m/s with Sport mode in EU regions.

Environmental / Weather Limitations

Max Wind Speed Resistance:
12 m/s*

* Max wind speed resistance during takeoff and landing.

Operating Temperature:
-10 Deg.C to 40 Deg.C (14 Deg.F to 104 Deg.F)

Any other relevant information

Fuel Type

Status Indicators / Alert Messages

Hazardous Substances

Any other relevant information

Batteries

Quantity

Type

Arrangement

Electrical Loads

Energy:
99.5 Wh

Any other relevant information

Capacity[1]:
6741 mAh

Engines

Type

Quantity

Propeller Type

Propeller Model:
1157F (standard propellers)
1154F (low noise propeller)

Any other relevant information

Sensors (These are sensors that assist in the safe flight of the UA, and not the payload)

Type

Sensing Type:
Omnidirectional binocular vision system, supplemented with a 3D infrared sensor at the bottom of the aircraft.

Forward:
Binocular Measurement Range: 0.4-22.5 m
Measurement Range: 0.4-200 m
Obstacle Avoidance Speed: Flight Speed <=21 m/s
FOV: 90 Deg. (horizontal), 135 Deg. (vertical)

Backward:
Measurement Range: 0.4-22.5 m
Measurement Range: 0.4-200 m
Obstacle Avoidance Speed: Flight Speed <=21 m/sField of View (FOV)-90 Deg. (horizontal), 135 Deg. (vertical)

Lateral:
Measurement Range: 0.5-32 m
Measurement Range: 0.5-200 m
Obstacle Avoidance Speed: Flight Speed <=21 m/s
FOV: 90 Deg. (horizontal), 90 Deg. (vertical)

Downward:
Measurement Range: 0.3-18.8 m
Obstacle Avoidance Speed: Flight Speed <=10 m/s
The FOV to the front and rear is 160 Deg. and 160 Deg. to the right and left.

Operating Environment:
Forward, Backward, Left, Right, and Upward:
Delicate texture on the surface, adequate light.

Downward:
The ground has rich textures and sufficient lighting conditions*, with a diffuse reflection surface and a reflectivity greater than 20% (such as walls, trees, people, etc.).

* Sufficient lighting conditions refer to an illuminance not lower than that of a nighttime city light scene.

Quantity

Backup Means of Navigation and Guidance

Automatic Flight Control Functions

Geo-awareness Functions

GNSS:
GPS + Galileo + BeiDou + GLONASS*

* GLONASS is supported only when the RTK module is enabled.

Any other relevant information

Beacon:
Built into the aircraft

C2 Link

Range

Transceivers / Modems

Power Levels

Operating Frequencies Used

Third Party Link Service Provider

Data rates

Latencies

Any other relevant information

Data source