Guide to Motors on Drones
By Association for Drones
Drone motors are one of the most important parts of the propulsion system because they convert electrical energy into mechanical rotation. That rotation turns the propellers, which generate the thrust required for take-off, hovering, climbing, manoeuvring and forward flight. On a multirotor, the motors are controlled individually by the flight controller through Electronic Speed Controllers, or ESCs. By increasing or decreasing the speed of different motors, the drone can roll, pitch, yaw, climb or descend. On fixed-wing and hybrid VTOL drones, motors may be used for forward propulsion, vertical lift or both. The correct motor depends on the aircraft’s weight, propeller size, battery voltage, required thrust, flight endurance and operating environment. A small inspection drone has very different motor requirements from a heavy-lift cargo platform, agricultural sprayer or long-range VTOL aircraft. For drone manufacturers, motor selection is therefore not simply about choosing the most powerful option available. The motor, propeller, ESC, battery and airframe all need to be designed as one complete propulsion system. ## **What Is a Drone Motor?** A drone motor converts electrical power from the battery into rotational movement. The motor spins a propeller, which accelerates air and creates thrust. Most modern electric drones use brushless motors because they are efficient, lightweight and reliable. These motors are electronically controlled rather than using mechanical brushes to switch current inside the motor. The motor itself does not decide how fast to rotate. The flight controller sends commands to the ESC, and the ESC regulates the electrical power supplied to the motor. ## **Brushless Motors** Brushless DC motors, often called BLDC motors, are the standard propulsion choice for most professional drones. They use permanent magnets and electromagnetic coils to create rotational force. Because there are no physical brushes rubbing against a commutator, there is less mechanical wear than with traditional brushed motors. This improves efficiency, reliability and service life. Brushless motors are particularly well suited to drones because they can respond rapidly to changes in throttle and provide a high power-to-weight ratio. ## **Brushed Motors** Brushed motors are simpler and less expensive than brushless motors, but they are less efficient and generally wear out faster. They are more common in very small toy drones and lightweight indoor aircraft. For professional commercial systems, brushless motors are normally preferred because of their greater efficiency, reliability and power. Heavy-duty drone applications almost always rely on brushless propulsion. ## **Stator and Rotor** The two main parts of a brushless motor are the stator and rotor. The stator contains the copper windings that create electromagnetic fields when current flows through them. The rotor contains permanent magnets and rotates around or inside the stator depending on motor design. The ESC energises the stator windings in sequence. This creates a rotating magnetic field that pulls the rotor around. ## **Outrunner Motors** Outrunner motors are very common on multirotor drones. In this design, the outer motor casing rotates around the stationary stator. Outrunners can generate relatively high torque at lower rotational speeds, making them well suited to driving larger propellers directly. Many commercial multirotors use outrunner motors because they provide good efficiency without requiring a gearbox. ## **Inrunner Motors** Inrunner motors have a rotating internal shaft while the outside of the motor remains stationary. They generally operate efficiently at higher rotational speeds. These motors are more common in high-speed systems, ducted fans and some fixed-wing applications. A gearbox may be used where high motor speed needs to be converted into lower propeller speed and greater torque. ## **Motor KV Rating** One of the most common motor specifications is KV. KV represents the approximate number of revolutions per minute the motor tries to produce per volt when running without a load. For example, a 500 KV motor operating from 20 volts would theoretically have a no-load speed of around 10,000 RPM. In real flight, propeller load reduces the actual speed significantly. ## **High-KV Motors** High-KV motors rotate faster for a given voltage. They are generally paired with smaller propellers. These combinations can provide high responsiveness and are common on smaller or faster drones. However, high rotational speed can increase noise and reduce efficiency if the motor and propeller are poorly matched. ## **Low-KV Motors** Low-KV motors rotate more slowly for a given voltage. They are generally paired with larger propellers. Large propellers can move more air efficiently and are therefore common on long-endurance and heavy-lift drones. Many industrial multirotors use relatively low-KV propulsion systems operating at higher battery voltages. ## **Torque** Torque describes the rotational force produced by the motor. Larger propellers require greater torque to accelerate and maintain rotation. A motor may be capable of very high RPM but still be unsuitable for a large propeller if it cannot produce sufficient torque. Motor design, winding configuration and operating current all influence torque capability. ## **RPM** RPM means revolutions per minute and describes how quickly the motor and propeller are rotating. Higher RPM can generate more thrust, but it also increases power consumption and aerodynamic losses. The ideal operating RPM depends on propeller diameter, pitch and mission requirements. Professional propulsion systems are designed to operate efficiently across the normal flight envelope rather than simply reaching maximum RPM. ## **Motor Size** Brushless drone motors are often described using numbers representing stator dimensions. For example, a motor described as 3510 may have an approximate stator diameter of 35 millimetres and height of 10 millimetres. Larger stators can normally produce more torque and handle more power. However, motor naming conventions can vary between manufacturers, so technical data should always be checked carefully. ## **Motor Weight** Motor weight matters because drones need to lift their own propulsion system. A more powerful motor may generate additional thrust but also add mass. The optimum design balances motor weight with thrust requirement and efficiency. For multirotors, this calculation must be repeated across several motors, so small weight differences can become significant. ## **Thrust** Thrust is the force generated by the propeller and motor combination. Manufacturers often publish thrust test data for different propellers and battery voltages. This information is more useful than motor power alone because it shows how the complete propulsion system performs. Motor selection should therefore be based on tested motor-and-propeller combinations wherever possible. ## **Thrust-to-Weight Ratio** A drone needs more total maximum thrust than its take-off weight. If total thrust only equals aircraft weight, the drone has no reserve for climbing, manoeuvring or controlling the aircraft in wind. Professional multirotors are therefore designed with a significant thrust margin. The required ratio depends on aircraft type, mission and desired performance. ## **Hover Throttle** An efficient multirotor is normally designed so that hovering does not require maximum motor output. The aircraft should have enough remaining thrust for control authority, climbing and disturbance rejection. Very high hover throttle may indicate an underpowered propulsion system. Very low hover throttle may mean the aircraft carries excessive motor and propulsion weight. ## **Propeller Matching** The motor and propeller need to be matched carefully. A larger or higher-pitch propeller creates greater aerodynamic load. If the propeller is too demanding, the motor can draw