Want to Choose the Right Products for You?
Take a quick test to find the right propeller for you.
T-Motor X-A16L-24S KV35 is a high-voltage heavy-lift motor designed for large agricultural and coaxial multirotor UAVs. The specified setup combines the X-A16L-24S motor, a 24S FOC 260A ESC and an EFZ6324 folding carbon-fiber propeller. It supports 24–28S LiPo batteries, provides 70–75kg rated thrust and reaches up to 156kg maximum thrust under the stated test configuration. With PWM/CAN control, a 35KV winding, IPX5 protection and an 80mm tube size, the system is designed for demanding UAV propulsion applications requiring high payload capacity and stable power delivery.
High-Voltage Heavy-Lift Motor
24–28S LiPo · 70–75kg Rated Thrust
Heavy-Lift 24S Motor System for Large UAVs
Propulsion for Large Heavy-Lift UAVs
The X-A16L-24S is designed for large agricultural and coaxial multirotor UAV applications. The provided recommendation data lists 200–220kg load capacity and 280–300kg take-off weight for agricultural quadcopters, as well as 340–370kg load capacity and 420–450kg take-off weight for agricultural hexacopters. Final propulsion selection should be confirmed according to the complete aircraft configuration, payload and operating conditions.
24S Power for High-Payload Applications
The X-A16L-24S KV35 setup supports 24–28S LiPo batteries and uses a specified 24S FOC 260A ESC with PWM/CAN control. The system supports DroneCAN, UAV CAN and CubeCAN protocols. Its 80mm tube size, 2400±5mm wire length, 126V maximum voltage and 260A short-time peak current provide key integration references for large high-voltage UAV propulsion systems.






Technical Parameters
· Product Type: Heavy-lift UAV motor
· Model: X-A16L-24S KV35
· Setup: A16L-24S Motor + 24S FOC 260A ESC + EFZ6324 Propeller
· Recommended Battery: 24–28S LiPo
· Rated Thrust: 70–75kg
· Efficiency at Rated Thrust: 6.6g/W at 70kg
· Maximum Thrust: 156kg
· Motor KV: 35KV
· Stator Size: 155 × 35mm
· Control Method: PWM/CAN
· Supported Protocols: DroneCAN, UAV CAN and CubeCAN
· Maximum Voltage: 126V
· Peak Current: 260A for a short time
· Tube Size: 80mm
· Wire Length: 2400±5mm
· Protection Rating: IPX5
· Recommended Ambient Temperature: -20°C to 55°C
· Propeller: EFZ6324 Folding Carbon Fiber Propeller
· Propeller Length: 63 inches / 1600.2mm
· BEC: No
· Weight: 15100±2g including wires and propeller
Want to Choose the Right Products for You?
Take a quick test to find the right propeller for you.
High-Voltage Thrust for Large UAV Platforms
· Recommended battery: 24–28S LiPo
· Rated thrust: 70–75kg
· Maximum thrust: 156kg
· Rated-thrust efficiency: 6.6g/W at 70kg
· Motor KV: 35KV
· Control method: PWM/CAN
· Peak current: 260A for a short time
· Test data is based on the specified X-A16L-24S KV35 + 24S FOC 260A + EFZ6324 setup
· Test results are bench data for reference and do not replace complete aircraft-level propulsion testing
Configuration and Shipping Confirmation
· The specified setup includes the X-A16L-24S motor, 24S FOC 260A ESC and EFZ6324 folding carbon-fiber propeller.
· Please confirm whether the motor, ESC and propeller are supplied together or quoted separately.
· Please confirm the final package contents, mounting accessories, cables and installation hardware before ordering.
· The actual shipping configuration is subject to the final quotation and order confirmation.
· Aircraft-level matching should be confirmed according to battery voltage, flight-controller system, propeller configuration and payload requirements.
Need a Custom
Share your UAV requirements. We’ll help evaluate the right propeller solution.
Installation and System Matching Notice
· Confirm that the battery voltage is within the recommended 24–28S LiPo range before operation.
· The motor, ESC and EFZ6324 propeller should be matched according to the specified propulsion setup.
· Confirm the required control method and protocol, including PWM, DroneCAN, UAV CAN or CubeCAN.
· The 260A peak-current specification is for short-time operation under the stated conditions; complete aircraft-level thermal testing is required.
· Confirm the propeller rotation direction, mounting orientation and coaxial configuration before flight.
· The provided thrust and efficiency data is bench-test reference data and should not be treated as a guaranteed aircraft performance result.
· Keep the operating environment within the recommended temperature range of -20°C to 55°C.
· Confirm the final weight, package contents and installation hardware before purchase.