# Features & Specifications

The PRS-M3DTEX has been designed to easily integrate with the DJI M3D/T. The PRS mounting holes screws, and strap secure the PRS-M3DTEX without interfering with onboard sensors or DJI Dock 2 usage. The system includes an integrated EM to power the PRS. The FTS is initiated when either the pilot instigates a deployment through the MTD or when the ATS, using the onboard sensors located in the EM, determines that the DJI M3D/T has breached the safe flying parameters. Once the FTS is initiated and stops the motors from spinning, the Parachute Pod™ is deployed and will result in the DJI M3D/T descending under an inflated parachute.

## Features

| Mounting Bracket                  | The custom base of the PRS-M3DTEX has an integrated mounting bracket that allows the PRS to be easily installed with minimal effort.                |
| --------------------------------- | --------------------------------------------------------------------------------------------------------------------------------------------------- |
| Mounting Straps                   | The mounting straps are secured to the PRS-M3DTEX and loop around the forward arms of the DJI M3D/T to provide an additional attachment method.     |
| Independent Power Source          | The PRS-M3DTEX is equipped with an independent power source that allows the system to deploy if the DJI M3D/T loses power.                          |
| Automatic Triggering System (ATS) | The ATS automatically detects failures and triggers the parachute release.                                                                          |
| Manual Triggering Device (MTD)    | The MTD can initiate deployment of the parachute recovery system at the discretion of the remote pilot in command.                                  |
| Flight Termination System (FTS)   | The plug-and-play FTS stops power to the motors in the event of a failure and reduces the likelihood of entanglement in the DJI M3D/T’s propellers. |
| Flight Data Logging               | Flight data logging to a dedicated internal storage device that is integrated in the PRS-M3DTEX.                                                    |

## Specifications

| Maximum Takeoff Weight                         | 1.61 kg (3.55 lbs)                  |
| ---------------------------------------------- | ----------------------------------- |
| Average Descent Rate\* (1.61 kg)               | 4.39 m/s (14.4 ft/s)                |
| Minimum Deployable Altitude Rating\* (1.61 kg) | 34.8 m (114.17 ft)                  |
| Deployment Technology                          | Energetic Charge                    |
| Deployment Trigger                             | Manual, Geofence, and/or Autonomous |
| Average Kinetic Energy (1.61 kg)               | 15.5 J (11.5 ft-lbs)                |

### Parachute Recovery System

| Main System Weight             | 195.0 g (6.88 oz) \[+/- 5 g]     |
| ------------------------------ | -------------------------------- |
| Deployment Release Time        | <100ms                           |
| Operating Temperature          | -20˚C to +45˚C (-4°F to 113°F)\* |
| Ingress Protection (IP) Rating | IP54                             |

### Flight Termination System (FTS)

| FTS Method          | Power Cut          |
| ------------------- | ------------------ |
| Integration Process | Slide Over Battery |

### Manual Triggering Device (MTD)

| Range         | < 8 km (<4.97 mi)                    |
| ------------- | ------------------------------------ |
| Arming Height | ≥ 5 m (≥ 16.4 ft)                    |
| Type          | DJI M3D/T Transmitter PSDK Interface |

{% hint style="danger" %}
IF USING THE GEOFENCE FEATURE, THE MTD RANGE WILL CORRESPOND TO THE LIMITS OF THE GEOFENCE, NOT THE 8 KM MAXIMUM. FOR ADDITIONAL INFORMATION, SEE THE "[GEOFENCING](/prs-m3dtex-for-dji-dock2/prs-m3dtex-for-dji-m3d-and-m3td/geofencing.md)" SECTION.
{% endhint %}

\*Per ASTM F3322-22 (Actual values may vary)


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