> For the complete documentation index, see [llms.txt](https://docs.deltaquad.com/sth/llms.txt). Markdown versions of documentation pages are available by appending `.md` to page URLs; this page is available as [Markdown](https://docs.deltaquad.com/sth/vehicle-specifications.md).

# Vehicle specifications

<figure><img src="https://content.gitbook.com/content/13glpP4Qg8c29eos11BK/blobs/YNgxRYTHbtYFrkvB61jS/cropped-Evo-Drawing-1536x685.jpg" alt=""><figcaption></figcaption></figure>

{% hint style="info" %}
To calculate the expected performance of the DeltaQuad Evo based on specific payloads and conditions, please refer to the [DeltaQuad Evo Performance Calculator](https://evo.deltaquad.com/calc/).
{% endhint %}

| **Dimensions:**                               | ​                             |
| --------------------------------------------- | ----------------------------- |
| Wingspan                                      | 269 cm                        |
| Length                                        | 75 cm                         |
| Height                                        | 33 cm (landing gear extended) |
| Wing area                                     | 84 sq. dm.                    |
| Payload bay                                   | 20 x 20 x 11 cm               |
| Flightcase dimensions                         | 112 x 82 x 46 cm              |
| Flightcase weight                             | \~ 30.4 kg                    |
| ​                                             | ​                             |
| **Weight and Payload:**                       | ​                             |
| Empty weight                                  | 4.8 kg                        |
| Empty weight including 1 battery              | 6.8 kg                        |
| Maximum takeoff weight                        | 10 kg                         |
| Payload capacity                              | 3 kg                          |
| ​                                             | ​                             |
| **Flight Characteristics with Dual battery:** | ​                             |
| Flight speed                                  | 16.8 m/s (60 km/h)            |
| Payload capacity                              | 1 kg                          |
| Maximum flight time                           | 16.8 m/s (60 km/h)            |
| Range through air                             | 244 km (151 mi)               |
| ​                                             | ​                             |
| **Power**                                     | ​                             |
| Battery type                                  | Semi Solid State Lithium-ion  |
| Battery cells                                 | 6                             |
| Battery capacity                              | 22Ah per battery              |
| ​                                             | ​                             |
| **Tolerances \***                             | ​                             |
| Maximum takeoff/landing wind                  | 12.5 m/s (45 Km/h)            |
| Maximum wind cruise flight                    | 14 m/s (50 Km/h)              |
| Maximum precipitation                         | 7mm/h (Drizzle)               |
| Operating temperature                         | Between -20 and +45 Celsius   |
| Maximum flight altitude AMSL                  | 13.000ft (4000m)              |

All flight characteristics are based on optimized settings at sea level

These values assume 90% battery usage, and low wind conditions and include a low-altitude vertical takeoff and landing at sea level.&#x20;

\* The tolerances are provisional and subject to change


---

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