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X-A14-18S Heavy-Lift Coaxial UAV Propulsion System (180–200kg Quad / 270–300kg Hexa)

By T-MOTOR ↗

The T-MOTOR X-A14-18S is a modular heavy-lift coaxial UAV propulsion assembly combining a KV49.6 brushless motor and 18S FOC 200A ESC. It offers optional 57-inch folding carbon fiber propellers, specifies 45-50kg rated thrust and a 60 mm tube size, and targets defined quadcopter and hexacopter weight ranges.

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T-MOTOR X-A14-18S coaxial UAV propulsion assembly with paired motors and mounting arm, without propellers
T-MOTOR X-A14-18S coaxial UAV propulsion assembly with paired motors and mounting arm, without propellers
Manufacturer and modelT-MOTOR X-A14-18S Heavy-Lift Coaxial UAV Propulsion System (180–200kg Quad / 270–300kg Hexa)
Integrated motorX-A14-18S KV49.6 brushless motor
Integrated ESC18S FOC 200A ESC
Recommended payload and takeoff weight100–120kg payload, 180–200kg takeoff weightQuadcopter configuration.
Recommended payload and takeoff weight170–200 kg payload, 270–300kg takeoff weightHexacopter configuration.
Rated thrust45-50kg

Product overview

The T-MOTOR X-A14-18S Heavy-Lift Coaxial UAV Propulsion System (180–200kg Quad / 270–300kg Hexa) is a propulsion assembly for integration into multirotor aircraft. It combines an X-A14-18S KV49.6 brushless motor with an 18S FOC 200A ESC in a modular arrangement of pre-matched components. Integration specifications include a 60 mm tube size. Arm-set selections comprise the motor and ESC combination, or that combination with EFZ57. The optional folding carbon fiber propeller is specified as EFZ57P, with a 57-inch diameter.

Recommended applications cover quadcopters with 100–120kg payload and 180–200kg takeoff weight, and hexacopters with 170–200 kg payload and 270–300kg takeoff weight. The general application description also identifies 140–160kg coaxial multirotor drones. Rated thrust is 45-50kg, and the recommended battery is 18S LiPo. Operating specifications include IPX5 ingress protection and a recommended temperature range of -20°C to 55°C. Propeller inclusion depends on the selected arm-set configuration.

Specifications

SpecificationValue & conditions
Manufacturer and modelT-MOTOR X-A14-18S Heavy-Lift Coaxial UAV Propulsion System (180–200kg Quad / 270–300kg Hexa)
Integrated motorX-A14-18S KV49.6 brushless motor
Integrated ESC18S FOC 200A ESC
Recommended payload and takeoff weight100–120kg payload, 180–200kg takeoff weightQuadcopter configuration.
Recommended payload and takeoff weight170–200 kg payload, 270–300kg takeoff weightHexacopter configuration.
Rated thrust45-50kg
Recommended battery18S LiPo
Tube size60 mm
Modular architecturePre-matched propulsion components for simplified installation and integration
PropellerEFZ57P folding carbon fiber propellerOptional propeller configuration.
Propeller diameter57-inchOptional propeller configuration.
Ingress protectionIPX5
Recommended operating temperature-20°C to 55°C
General application weight140–160kgCoaxial multirotor drone application.
Arm-set optionsX-A14-18S KV49.6+18S FOC 200A; X-A14-18S KV49.6+18S FOC 200A+EFZ57Selectable arm-set configurations.
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