4112 PRO IPE eVTOL Motor
The MAD 4112 PRO IPE V1.0 is listed for 1,400–1,900 g payload per rotor, 15–16 inch carbon-fiber propellers and 3,788 g maximum thrust per motor. Its feathering function is described as reducing drag after engine failure.
Technical Specifications
| Motor size | D46.6 × 34.7 mm |
|---|---|
| Weight | 146 g |
| Protection | IP35 |
| Propeller | 15–16 inch carbon fiber |
| Maximum thrust | 3,788 g per motor |
| Propeller mounting | D12 M3×4 |
| KV option | 450KV |
| Packaging options | 1pc; 2pcs |
Application and Compatibility
The published payload and feathering-propeller data make this model relevant to eVTOL propulsion studies. Confirm the complete propeller, battery, ESC and transition-control configuration before ordering.
Preguntas frecuentes
What is the feathering function? The product data states that it automatically reduces drag after engine failure. Confirm the aircraft mechanism and control integration separately.
Request a Quote
Provide payload, propeller, battery, ESC and quantity requirements for a compatibility review.
