AT-MIN210 — electric VTOL fixed-wing UAV
- Maximum payload / recommended working payload: 5 kg / 1.2 kg recommended
- Maximum endurance (unloaded): 210 min
- Max takeoff weight: Less than 13.5 kg
Product overview
The AT-MIN210 is an electric VTOL fixed-wing aircraft for civil inspection. Its maximum payload is 5 kg, and 1.2 kg is the recommended working payload. Maximum endurance is 210 minutes unloaded; confirm endurance for the selected payload and configuration. Transport usually takes about two weeks, subject to destination, transport arrangements and customs clearance; confirm the final schedule in your quotation.
Published selection facts
- Maximum payload / recommended working payload: 5 kg / 1.2 kg recommended.
- Maximum endurance (unloaded): 210 min.
How to assess this model
For a civil or commercial project, send payload mass, sensor or cargo dimensions, desired endurance, operating environment, quantity and destination. We will check configuration fit and provide an email quotation or WhatsApp consultation;
Application and integration
For a civil or commercial survey, inspection, mapping, logistics or emergency-response project, confirm the payload, sensor or cargo interface, operating area and launch or recovery conditions before ordering. Application cards below link to the relevant planning pages.
Product questions
What payload is published for this VTOL model?
5 kg / 1.2 kg recommended.
What endurance is published for this VTOL model?
210 min.
What is the estimated transport time?
Transport usually takes about two weeks, subject to destination, transport arrangements and customs clearance. Confirm the final schedule in your quotation.
What should I send for a configuration quotation?
Send the model, payload mass, sensor or cargo dimensions, desired endurance, operating environment, quantity and destination. We will confirm configuration fit and quotation scope.
Configuration and application fit
AT-MIN210 — electric VTOL fixed-wing UAV AT-MIN210 is an electric VTOL fixed-wing UAV for civil inspection in the Aerosys industrial UAV line. Maximum payload: 5kg; recommended working payload: 1.2kg. Maximum endurance: 210min unloaded. Max takeoff weight: less than 13.5kg; wingspan: 2500mm; airframe length: 1260mm. Published specification: landing gear height: 195mm; mission bay dimensions: 260mm*172mm*90mm; battery bay dimensions: 260mm*150mm*85mm; packing box dimensions: 1500mm*490mm*370mm; powerplant type: electric brushless motor; electronic speed control system; airframe material: carbon fiber, fiberglass, Kevlar, PVC, etc.; mission bay position: directly below the aircraft center of gravity.
Published selection points
- Published specification: Airframe length: 1260mm
- Published specification: Wingspan: 2500mm
- Published specification: Landing gear height: 195mm
- Published specification: Mission bay dimensions: 260mm*172mm*90mm
- Published specification: Battery bay dimensions: 260mm*150mm*85mm
- Published specification: Packing box dimensions: 1500mm*490mm*370mm
For a configuration quote, send the model, quantity, destination and intended civil or commercial use. Add the required interface, payload, cargo or sensor details where relevant so the supply scope can be checked clearly.
Technical Specifications
| Parameter | Value |
|---|---|
| Airframe length | 1260mm |
| Wingspan | 2500mm |
| Landing gear height | 195mm |
| Mission bay dimensions | 260mm*172mm*90mm |
| Battery bay dimensions | 260mm*150mm*85mm |
| Packing box dimensions | 1500mm*490mm*370mm |
| Powerplant type | Electric brushless motor; electronic speed control system. |
| Airframe material | Carbon fiber, fiberglass, Kevlar, PVC, etc. |
| Mission bay position | Directly below the aircraft center of gravity |
| Structural weight | Approx. 3200g (including all structural and mounting parts) |
| Max takeoff weight | Less than 13.5kg |
| Maximum payload / recommended working payload | 5kg / 1.2kg recommended |
| Maximum endurance (unloaded) | 210min |
| Max control distance | Ground station / 5km-80km |
| Standard cruise speed over flat terrain | 68km/h (approx. 19m/s at 12.5kg) (recommended cruise speed for mountain work 21m/s at 12.5kg) |
| Max cruise speed | 108km/h (30m/s) |
| Standard battery configuration | 22.8v/25Ah*2 (45.6V) |
| Never-exceed speed | 120 km/h (approx. 33.3 m/s) |
| Max flight radius | 200km |
| Max level-flight ceiling | Altitude 5000m |
| Wind resistance in fixed-wing mode | Wind up to level 6 |
| Max wind resistance in rotor takeoff/landing mode | Wind up to level 4 |
| Operating environment | -20℃~45℃; can fly in light rain |
| Takeoff and landing method | Vertical takeoff and landing |
| VTOL propulsion propeller size | 16/17 inch (recommended) |
| Fixed-wing tail pusher propeller | 15~17 inch (recommended) |
| Max thrust-to-weight ratio in fixed-wing mode | 0.65 (standard configuration) |
| High-altitude performance | Passed high-altitude plateau testing |
| Standard empty takeoff weight | 11.2kg |
Application Scenarios
- Long-range linear infrastructure patrol
- Mapping and survey of large areas
- Emergency response and disaster assessment
- Maritime and border monitoring
- Heavy-payload logistics and delivery
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