Drone Propulsion Systems
Compare drone propulsion systems from Chinese manufacturers, including integrated motor, ESC and propeller arm sets and power combos, and request a quote.
Integrated drone propulsion sets combine matched drive components for multirotor airframes. Listings include motor-and-ESC combinations, propulsion modules and complete arm sets, with propellers included or supplied separately depending on the configuration.
111 models10 manufacturers
Arm sets (motor+ESC+prop)
View all 28 →28 models from 1 manufacturers
Arm sets (motor+ESC+prop)
MAD 8X-10 M8SC10 drone arm set
- KV options
- 85 KV; 100 KV
- Maximum thrust
- 10.6kgF/rotor
Arm sets (motor+ESC+prop)
MAD XP10 V2 Drone Arm Set 90KV
- Maximum thrust
- 24 kg
- Weight
- 1.59 kg
Arm sets (motor+ESC+prop)
MAD XP12 V2 Drone Arm Set 85KV
- Maximum thrust
- 38 kg
- Weight
- 2.3 kg
Arm sets (motor+ESC+prop)
MAD 5X08 5008 Drone Arm Set
- KV options
- 240 KV, 300 KV, 340 KV
Propulsion systems & power combos
View all 83 →83 models from 10 manufacturers
Propulsion systems & power combos
T-MOTOR 605-X Integrated Propulsion System (MN605-S Motor + Alpha 60A ESC Combo), 170KV/320KV
- Peak current
- 35 A
Propulsion systems & power combos
MAD HB40-64x20 drone Power Combo
Propulsion systems & power combos
Guoanda GAD-WX
Propulsion systems & power combos
AKSL G25U-18S
What to check before you buy
- Included components
- Check whether the set includes the motor, ESC, propeller, arm tube and wiring or only part of that assembly.
- Thrust at the working point
- Compare thrust and electrical input at the intended battery voltage and propeller, including hover duty.
- KV and voltage pairing
- Match the exact motor KV and ESC voltage option to the battery configuration and selected propeller.
- Arm attachment
- Check tube diameter, mounting adapters, cable exits and rotation direction for the airframe.
- Control and monitoring
- Check ESC command protocols and available speed, current and temperature telemetry.
- Thermal capacity
- Check continuous operation and cooling at mission load, since peak thrust may have a limited duration.