Product overview
The T-MOTOR AT4130 is a propulsion kit intended for integration into a fixed-wing UAV. Its procurement role is aircraft propulsion, with a stated application range of 12–15 kg maximum takeoff weight. That range describes the intended aircraft weight class rather than a payload capacity.
The kit is designated as a 20 cc gas-engine equivalent, providing an engine-size comparison for propulsion selection. Its product identity is a propulsion kit for an aircraft installation; the 12–15 kg MTOW designation applies to the intended fixed-wing UAV application.
Specifications
| Specification | Value & conditions |
|---|---|
| Manufacturer and model | T-MOTOR AT4130 |
| Product configuration | Fixed-wing UAV propulsion kit |
| Intended aircraft maximum takeoff weight | 12–15 kg MTOW |
| Gas-engine equivalence | 20 cc gas-engine equivalent |
| Model | T-MOTOR AT4130 fixed-wing UAV propulsion kit |
| Aircraft MTOW | 12–15kg |
| Gas engine equivalent | 20CC |
| Recommended takeoff weight | 12–15kgFor fixed-wing UAVs |
| Included motor | AT4130 KV230Kit selection shown on product page |
| Included electronic speed controller | AT115A 14SKit selection shown on product page |
| Propeller | Optional AUZ 17×12Selectable with or without propeller |
Request a quote for T-MOTOR AT4130 fixed-wing UAV propulsion kit
Send your application, destination country and expected quantity to the ChinaDrone team. We can discuss product selection, configuration and sourcing from China.
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