MAD M6C12 IPE V3 Drone Motor Summary

The MAD M6C12 IPE V3.0 motor is a high-performance motor designed for UAV applications, featuring a stator from Taiwan with anticorrosive properties and a varnished wire degree of 180°C. It has a compact size (D:72 × 35.4 mm) and provides IP45 protection. The motor is equipped with EZO 696ZZ bearings and supports centrifugal heat dissipation. It comes with multiple propeller mounting hole options and additional accessories for easy integration. The motor specifications include various KV options (150KV, 170KV, 280KV, 400KV), each offering different performance characteristics in terms of current, thrust, and power, making it suitable for different UAV configurations ranging from quadcopters to octocopters with varying take-off weights.

MAD ANTIMATTER brand motors are defined as “not ordinary” in the field of multi-rotor motors. We are proud to launch the ANTIMATTER series motors (M6C06, M6C08, M6C10, M6C12) at the end of 2019. We spent a year designing and proving which drone motors are the most efficient with 21-24in props. This is the magic! MAD Components in Poland.
The M6C12 IPE is designed for a payload of 2.5-4kg and supports 6S-12S voltage.

MAD M6C12 IPE V3 Drone Motor Specifications

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Specifications

Antimatter M6C12 IPE is designed to carry payload of 2.5-4kg, supports 6S-12S voltage. Comparing with equivalent same class motors in the market, our M6C12 IPE has higher efficiency, and about 30 gram lighter. It’s your best to go motor in this load for endurance flight.

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MAD M6C12 Drone Motor – Industry Professional Edition. This motor features 150KV, 170KV, 280KV, or 400KV brushless design for RC long-range UAV applications, including video, mapping, and aerial photography.Key specifications include:* Energy-efficient with a maximum thrust of 2.5-3.0 kgf (7.5 kgf recommended)* Thrust dependent on battery level, propeller type, hover thrust, air pressure, and other conditions* Efficiency: 80%* Maximum current: 80A (5-14S or 6S Li-C)* Analytical graph of motor operation: + Current (A) + Input Power (W) + Electrical Efficiency (%) + Thrust (N) + Rotational Speed (RPM)The data above was measured at an input voltage of 24V, temperature of 25°C, and sea level. The rotational speed was adjusted by the throttle (P = W ÷ rotor) ni%).

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