Compare specifications
Figures from the 2026 brochures. Endurance is measured under the conditions in the notes below the table. Compare payloads →
| eVTOL fixed-wing | Multirotor | |||||
|---|---|---|---|---|---|---|
| Item |  Avix GN220 |  Vertix VL260 |  Vilverin VL340 |  Xtrix VL390 |  Voxel MX |  Voxel GS |
| Airframe and weight | ||||||
| Max. takeoff weight (MTOW) kg | 7.5 | 15.5 | 21.5 | 35 | 12.5 | 14.5 |
| Maximum payload kg | 0.5 | 2 | 3.5 | 5 | 3.5 | 5 |
| Wingspan mm | 2,180 | 2,670 | 3,610 | 3,914 | – | – |
| Diagonal wheelbase mm | – | – | – | – | 1,200 | 1,320 |
| Flight performance | ||||||
| Endurance, no payload min | 1001 | 1201 | 1501 | 1801 | 752 | 902 |
| Mapping endurance (RGB camera) min | 713 | 863 | 1053 | 1163 | 533 | – |
| Cruise speed m/s | 18–22 | 22–28 | 21–24 | 23–26 | 8–10 | 9–114 |
| Maximum speed m/s | 24 | 28 | 30 | 30 | 15 | 16 |
| Distance flown per flight km | 70+ | 110+ | 130+ | 150+ | 20+ | 30+ |
| ISR operating range km | 7–10 | 15–25 | 25–35 | 35–50 | 5–7 | 10–15 |
| Wind and altitude | ||||||
| Wind resistance, VTOL m/s | 7 | 8.3 | 8.3 | 8.3 | 13.8 | 13.8 |
| Wind resistance, cruise m/s | 12 | 13.8 | 13.8 | 13.8 | – | – |
| Maximum wind resistance m/s | – | – | – | – | 13.8 | 13.8 |
| Service ceiling m AMSL | 3,500 | 4,500 | 4,500 | 4,500 | 4,000 | 4,000 |
| Systems and operation | ||||||
| Assembly time min | < 3 | < 3 | < 5 | < 10 | < 3 | 2 |
- 1 Flight test in a windless environment at 100 m AMSL until battery reaches 5%. Actual flight time varies with flight method and scenario.
- 2 Flight speed ~8 m/s, windless, at mean sea level, until battery reaches 0%.
- 3 Normal operation: mapping with RGB camera, landing with 25% battery reserve (the practical working range).
- 4 Economical cruise speed; depends on payload weight and shape.
- Flight times are averages measured in Thailand in normal wind. When comparing with foreign datasheet figures measured in no wind, add about 15-20% to the flight time of ICS UAVs.