MAD 5010 EEE is designed to carry payloads of 800–2900g per rotor, with 14-22"carbon propeller. Support 6S-12S. Max thrust of single rotor is up to 4400g, unit motor only weighs 158g. EEE reduction version design, minimized weight, optimized efficiency and flight time extended.
* Open body design for better passive heat dissipation.
* Propeller installation compatibility.
* Reduced motor weight.
* Motor mounting holes standarization.
* Reduced motor weight.
* Motor mounting holes standarization.
Motor Test Benchmarks
Products Packaging
