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GAUTEN UAV SKYV293 VTOL drone Engine
VTOL / GAUTEN UAV

GAUTEN UAV SKYV293 Fixed-Wing VTOL Drone - Engine Version

Listed wingspan
2930 mm
Listed material
Carbon Fiber
Listed payload capacity
3 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 notice
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Share the package, quantity and destination. Confirm included parts and delivery terms in your quote.

SKU: SKYV293-CFK

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 SKYV293 UAV Fixed Wing VTOL Drones Engine — product details

The SKYV293 engine listing describes a 2930 mm carbon-fiber VTOL airframe. The source tables also use SV293 component names; confirm the exact model, propulsion package and included parts in your quote.

What to review

  • 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.
  • VTOL planning: Define a clear takeoff and landing area, surface conditions and operating limits. Confirm transition performance and the complete propulsion setup before use.
  • Flight performance: Use the source-listed values in the table as a starting point. Confirm propulsion, payload, power or fuel load, weather and test conditions for your final system.
  • 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.
  • Performance evidence: Ask which configuration and test conditions produced the listed values. Do not treat maximum figures as guaranteed results for every payload.

Listed technical specifications

SPECIFICATION PARAMETERS
Specifications Materials Carbon Fiber
Wingspan 2930 mm
Length 2030 mm
Payload Bay Dimensions (L*W*H) 560 mm * 210 mm * 185 mm
Wing Area 100 dm²
Empty Weight 10 kg
Payload Capacity 3 kg
Maximum Takeoff Weight (MTOW) 23 kg
Fuel Tank Capacity 5.5 L
Performance Characteristics Cruising Speed 23 to 25 m/s
Maximum Speed 30 m/s
Stall Speed 18 m/s
Max Flight Time (Electric) 1.5 Hours
Max Flight Time (Gasoline) 3 Hours
Recommended Battery 44.4V (12S LiPo)

Package options & included parts

Category Specification Item KIT Package PNP (Electric) Package
Flying Platform SV293 Outer Wing 2 pcs 2 pcs
SV293 Mid-Wing 1 pc 1 pc
SV293 Mainframe 1 pc 1 pc
SV293 Support Mast (incl. Vertical Stabilizer) 2 pcs 2 pcs
SV293 Landing Gear 2 pcs 2 pcs
SV293 Horizontal Stabilizer 1 pc 1 pc
SV293 Fuel Tank 1 pc 1 pc
SV293 Engine Cowling 1 pc 1 pc
Power System & Electronics Tailthrust Engine / Motor — 1 pc
Tailthrust Propeller — 1 pc
VTOL Motor — 4 pcs
VTOL ESC — 4 pcs
VTOL Propeller — 2 pairs (4 pcs)
Servos — 7 pcs
Pitot Tube (Airspeed Sensor) — 1 pc
Hardware & Cable Package — 1 pc

Product questions

Q: What is the difference between the KIT and PNP(E) versions?
Compare the component tables for the exact option you select. Confirm the airframe, propulsion, servos, wiring and customer-supplied items in your quote. PNP is not a complete ready-to-fly system.
Q: What payload sensors can the SV293 carry?
Check the listed payload limit and bay dimensions against your equipment. Share its mass, dimensions, mounting, power and data needs. Space and weight limits alone do not confirm sensor compatibility.
Q: What power system and battery do you recommend for electric setup?
Confirm the propulsion option, wiring and required battery or fuel setup for this model. Ask for matching voltage and cell-count information before choosing electrical parts; listed endurance is configuration-dependent.
Q: Is the SV293 suitable for operations in remote or tight spaces?
For mapping, surveying or aerial inspection, define the required output and sensor first. Review payload fit, avionics, operating conditions and test evidence; these are planning uses, not confirmed customer deployments.
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