Description

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.

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