Jiyuan Rayi Innovation Science Technology Co., Ltd Jiyuan Rayi Innovation Science Technology Co., Ltd
T-Motor X-A14-24S KV37 Motor

T-Motor X-A14-24S KV37 Motor

T-Motor X-A14-24S KV37 is a high-voltage heavy-lift motor designed for large agricultural and coaxial multirotor UAVs. The specified setup combines the X-A14-24S motor, a 24S FOC 150A ESC and an EFZ5720 folding carbon-fiber propeller. It supports 24–28S LiPo batteries, provides 45–50kg rated thrust and reaches up to 113kg maximum thrust under the stated test configuration. With PWM/CAN control, a 37KV winding, IPX5 protection and a 60mm tube size, the system is intended for demanding UAV propulsion applications requiring high payload capacity and stable power delivery.

  • High-Voltage Heavy-Lift Motor

    24–28S LiPo · 45–50kg Rated Thrust

Heavy-Lift 24S Motor System for UAVs

T-Motor X-A14-24S motor system for 140–160kg coaxial multirotor drones

Propulsion for Heavy-Lift Multirotor Platforms

The X-A14-24S is designed for high-payload multirotor applications, including agricultural quadcopters, hexacopters and coaxial UAV platforms. The provided recommendation data lists 140–160kg take-off weight for quadcopters and 210–240kg take-off weight for hexacopters. Final propulsion selection should be confirmed according to the complete aircraft configuration, payload and operating conditions.

T-Motor X-A14-24S KV37 motor technical specifications

24S Power with Integrated Control Options

The X-A14-24S KV37 setup supports 24–28S LiPo batteries and uses a specified 24S FOC 150A ESC with PWM/CAN control. The system supports DroneCAN, UAV CAN and CubeCAN protocols. Its 60mm tube size, 1500±5mm wire length, 126V maximum voltage and 150A short-time peak current provide key integration references for high-voltage UAV propulsion design.

T-Motor X-A14-24S KV37 Motor

T-Motor X-A14-24S KV37 Motor

T-Motor X-A14-24S KV37 Motor

T-Motor X-A14-24S KV37 Motor

T-Motor X-A14-24S KV37 Motor

T-Motor X-A14-24S KV37 Motor

T-Motor X-A14-24S KV37 Motor





Technical Parameters

· Product Type: Heavy-lift UAV motor

· Model: X-A14-24S KV37

· Setup: A14-24S Motor + 24S FOC 150A ESC + EFZ5720 Propeller

· Recommended Battery: 24–28S LiPo

· Rated Thrust: 45–50kg

· Efficiency at Rated Thrust: 7.4g/W at 45kg

· Maximum Thrust: 113kg

· Motor KV: 37KV

· Stator Size: 138 × 25mm

· Control Method: PWM/CAN

· Supported Protocols: DroneCAN, UAV CAN and CubeCAN

· Maximum Voltage: 126V

· Peak Current: 150A for a short time

· Tube Size: 60mm

· Wire Length: 1500±5mm

· Protection Rating: IPX5

· Recommended Ambient Temperature: -20°C to 55°C

· Propeller: EFZ5720 Folding Carbon Fiber Propeller

· Propeller Length: 57 inches / 1447.8mm

· BEC: No

· Weight: 9700±2g including wires and propeller


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T-Motor X-A14-24S thrust efficiency and power analysis chart

High-Voltage Thrust and Efficiency Data

· Recommended battery: 24–28S LiPo

· Rated thrust: 45–50kg

· Maximum thrust: 113kg

· Rated-thrust efficiency: 7.4g/W at 45kg

· Motor KV: 37KV

· Control method: PWM/CAN

· Peak current: 150A for a short time

· Test data is based on the specified X-A14-24S KV37 + 24S FOC 150A + EFZ5720 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-A14-24S motor, 24S FOC 150A ESC and EFZ5720 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 EFZ5720 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 150A 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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