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T-Motor X-A16L-24S KV35 Motor

T-Motor X-A16L-24S KV35 Motor

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

T-Motor X-A16L-24S motor system for 280–300kg coaxial multirotor drones

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.

T-Motor X-A16L-24S KV35 motor technical specifications

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.

T-Motor X-A16L-24S KV35 Motor

T-Motor X-A16L-24S KV35 Motor


T-Motor X-A16L-24S KV35 Motor

T-Motor X-A16L-24S KV35 Motor

T-Motor X-A16L-24S KV35 Motor

T-Motor X-A16L-24S KV35 Motor





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


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T-Motor X-A16L-24S thrust efficiency and power analysis chart

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.


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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.


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