Technical Characteristics:
DJI Matrice 400

WARNING: This document was generated automatically and may contain errors and/or ommissions. You MUST review the data and satisfy yourself that it is complete and accurate. There is a link to the original source of the data below to help you do that.

Mass

Empty Mass

Takeoff Weight:
Without Batteries: 5020±20 g
With Batteries: 9740±40 g

The actual product weight may vary due to differences in batch materials and external factors.

Maximum Take-Off Mass (MTOM)

Max Takeoff Weight:
15.8 kg

Dimensions for Rotorcraft / Multirotor

Length of aircraft body

Dimensions:
Unfolded: 980 x 760 x 480 mm (L x W x H) (with landing gear)
Folded: 490 x 490 x 480 mm (L x W x H) (with landing gear and gimbal)

Maximum dimensions excluding propellers.

Aircraft carrying case dimensions: 779 x 363 x 528 mm (L x W x H)

Diagonal Wheelbase:
1070 mm

Width of aircraft body

N/A

Height of aircraft body

N/A

Propeller Dimensions

N/A

Propeller Configuration

N/A

Centre of Gravity (CG)

N/A

 

Flight Duration / Endurance

Max Flight Time:
59 minutes

Measured with the aircraft flying forward at a constant speed of 10 m/s in a windless environment at sea level, carrying only the H30T (total weight 10,670 g), and from 100% battery level until 0%. Data is for reference only. Actual experience may vary depending on the environment, usage, and firmware version.

Maximum Range

Max Flight Distance:
49 km

Measured by the aircraft flying forward at a constant speed of 17 m/s in a windless environment at sea level, without external payloads, and from 100% battery level until 0%. Actual experience may vary depending on the environment, usage, and firmware version.

Maximum Operating Height (Service Ceiling)

Max Takeoff Altitude:
7000 m

Maximum Airspeed

Max Horizontal Speed (at sea level, no wind):
25 m/s

Environmental / Weather Limitations

Max Wind Speed Resistance:
12 m/s

Max wind speed resistance during takeoff and landing.

Operating Temperature:
-20 Deg. to 50 Deg. C (-4 Deg. to 122 Deg. F) (without solar radiation)

Any other relevant information

Ingress Protection Rating[3]:
IP55

The rating is not permanently effective and may decrease due to product wear and tear.
 

Fuel Type

N/A

Status Indicators / Alert Messages

N/A

Hazardous Substances

N/A

Any other relevant information

N/A
 

Batteries

Quantity

N/A

Type

Model:
TB100

Arrangement

N/A

Electrical Loads

Energy:
977 Wh

Standard Voltage:
48.23 V

Any other relevant information

Capacity:
20254 mAh
 

Engines

Type

N/A

Quantity

N/A

Propeller Type

Propeller Model:
2510F

Any other relevant information

N/A
 

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

Type

Sensing Type:
Omnidirectional binocular vision system (surround view provided by full-color fisheye vision sensors)

Horizontal rotating LiDAR, upper LiDAR and downward 3D infrared range sensor

Six-direction mmWave radar

Forward:
Measurement Range: 0.4-21 m
Detection Range: 0.4-200 m
Field of View (FOV): 90 Deg. (horizontal), 90 Deg. (vertical)

Backward:
Measurement Range: 0.4-21 m
Detection Range: 0.4-200 m
Field of View (FOV): 90 Deg. (horizontal), 90 Deg. (vertical)

Lateral:
Measurement Range: 0.6-21 m
Detection Range: 0.5-200 m
Field of View (FOV): 90 Deg. (horizontal), 90 Deg. (vertical)

Downward:
Measurement Range: 0.5-19 m
The FOV to the front and rear is 160 Deg. and 105 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

N/A

Backup Means of Navigation and Guidance

N/A

Automatic Flight Control Functions

N/A

Geo-awareness Functions

Global Navigation Satellite System:
GPS + Galileo + BeiDou + GLONASS*

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

Equipped with standard airborne ADS-B In receiver and dual antennas, supporting reception up to 20 km.

Any other relevant information

Beacon:
Built into the aircraft
 

C2 Link

Range

N/A

Transceivers / Modems

Power Levels

N/A

Operating Frequencies Used

N/A

Third Party Link Service Provider

N/A

Data rates

N/A

Latencies

N/A

Any other relevant information

N/A
 

Data source

https://enterprise.dji.com/matrice-400/specs

Generated using dronespec.info
Source data aquired 2023-01-23 19:03:43