GAUTEN UAV SV360 Fixed-Wing VTOL Drone - Engine Version
- Listed wingspan
- 3600 mm
- Listed material
- Full Carbon Fiber
- Listed payload capacity
- 6 kg
Listed values depend on the configuration. Confirm the final specifications with sales.
Export and dispatch: confirm each stage
Our current airframe order process includes Chinese dual-use export licence applications, including for bare airframes. This is our handling process, not a blanket legal classification of every product. Document preparation, export review, production and freight must be confirmed separately; approval and a total delivery date are not guaranteed.
Read the export and dispatch noticeShare the package, quantity and destination. Confirm included parts and delivery terms in your quote.
Contact sales to confirm availability.
Tell us your model, payload, application and package choice. Specifications below come from the original listing; confirm them for your final configuration.
GAUTEN UAV SV360 Fixed-Wing VTOL Drone - Engine Version — product details
The SV360 engine listing describes a 3600 mm carbon-fiber VTOL airframe. Review the KIT and PNP(E) tables to identify the structure, VTOL propulsion and other included parts.
Airframe construction: Review the listed material, dimensions and structural parts. Ask for model-specific drawings and inspection information; material alone does not prove weather resistance or service life.
Listed performance & conditions
Battery and power: Ask for a wiring diagram and the specified voltage, cell count, capacity and connectors for this package. Confirm these together before choosing a battery.
Payload space & installation
Payload installation: Check the listed bay dimensions and payload limit. Sensor fit also depends on mounts, balance, power and data interfaces; compatibility must be confirmed.
Launch & landing requirements
VTOL planning: Define a clear takeoff and landing area, surface conditions and operating limits. Confirm transition performance and the complete propulsion setup before use.
Launch & landing requirements
Payload space & installation
Mapping and aerial inspection: Define the data or inspection output first. Select the sensor, positioning, processing workflow and flight plan together; no completed integration is implied.
Listed technical specifications
| PARAMETER & SPECIFICATIONS | VALUE | |
|---|---|---|
| Physical Specifications | Airframe Material | Full Carbon Fiber |
| Wingspan | 3600 mm | |
| Aircraft Length | 2420 mm | |
| Wing Area | 132 dm² | |
| Payload Bay Dimensions (L*W*H) | 560 mm × 260 mm × 270 mm | |
| Empty Airframe Weight | 16 kg | |
| Max. Payload Capacity | 6 kg | |
| Maximum Takeoff Weight (MTOW) | 40 kg | |
| Performance & Power | Fuel Tank Capacity | 11 Liters |
| Cruising Speed | 30 m/s | |
| Maximum Flight Speed | 35 m/s | |
| Stall Speed | 24 m/s | |
| Maximum Flight Endurance | Up to 6 Hours | |
Package options & included parts
| Category | Component Description | KIT Package | PNP(E) Package |
|---|---|---|---|
| Flying Platform | SV360 Outer Wing | 2 | 2 |
| SV360 Mid-Wing | 1 | 1 | |
| SV360 Mainframe Airframe | 1 | 1 | |
| Support Strut (incl. Vertical Stabilizer) | 2 | 2 | |
| Landing Gear (Updated Latest Style) | 2 | 2 | |
| Horizontal Stabilizer | 1 | 1 | |
| Fuel Tank (11L) | 1 | 1 | |
| Engine Cowling | 1 | 1 | |
| Power System | Tail Thruster Engine | - | 1 |
| Tail Thruster Blades | - | 1 | |
| VTOL Motors | - | 4 | |
| VTOL ESCs | - | 4 | |
| VTOL Propellers | - | 2 Pairs | |
| Servos | - | 7 | |
| Pitot Tube | - | 1 | |
| Parts Packaging & Accessories | - | 1 Package |
Battery and power: Ask for a wiring diagram and the specified voltage, cell count, capacity and connectors for this package. Confirm these together before choosing a battery.
