> For the complete documentation index, see [llms.txt](https://docs.deltaquad.com/gov/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/gov/vehicle-specifications.md).

# Vehicle Specifications

This section discusses the technical specifications of the DeltaQuad Evo GOV and the DeltaQuad Evo Performance Calculator.

<figure><img src="https://content.gitbook.com/content/KBsYYYTTfla4fXzYBpU6/blobs/3d79DgdfD2d0iR6snz2R/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 %}

{% embed url="<https://youtu.be/0MWr88wU5Qk>" %}

| **Dimensions:**                               | ​                                                                                           |
| --------------------------------------------- | ------------------------------------------------------------------------------------------- |
| Wingspan                                      | 269 cm                                                                                      |
| Length                                        | 75 cm                                                                                       |
| Height                                        | 33 cm (landing gear extended)                                                               |
| Wing area                                     | 84 sq. dm.                                                                                  |
| Airframe material                             | Fiberglass, carbon, Kevlar, and composite                                                   |
| 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 bay                                   | 1x 20 x 20 x 11 cm or 2x 10 x 20 x 11 cm                                                    |
| Payload capacity                              | 3 kg (single battery) 1 kg (dual battery)                                                   |
|                                               |                                                                                             |
| **Flight Characteristics with Dual battery:** | ​(Measured at 0 m AMSL takeoff location, at 100 m flight altitude, and 20 degrees Celsius.) |
| Flight speed                                  | 16.54 m/s (60 km)                                                                           |
| Payload capacity                              | 1 kg                                                                                        |
| Maximum flight time                           | 255 minutes / 4 hours 15 minutes                                                            |
| Range through air                             | 254 km (158 mi)                                                                             |
| ​                                             | ​                                                                                           |
| **Power**                                     | ​                                                                                           |
| Battery type                                  | Semi Solid State Lithium-ion                                                                |
| Battery cells                                 | 6                                                                                           |
| Battery capacity                              | 22 Ah per battery                                                                           |
| Charging time for 2 batteries (parallel)      | Under 1 hour                                                                                |
| ​                                             | ​                                                                                           |
| **Tolerances \***                             | ​                                                                                           |
| Maximum takeoff/landing wind                  | 12.5 m/s (45 km/h)                                                                          |
| Maximum wind cruise flight                    | 14 m/s (50 km/h)                                                                            |
| Maximum precipitation                         | 7 mm/h (Drizzle)                                                                            |
| Operating temperature                         | Between -20 and +45 Celsius                                                                 |
| Maximum takeoff altitude AMSL                 | 4000 m (13123 ft)                                                                           |
| Maximum flight altitude AMSL                  | 5500 m (18044 ft)                                                                           |

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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