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T-MOTOR AX335-B brushless motor

By T-MOTOR ↗

The T-MOTOR AX335-B KV425 is a brushless UAV motor for fixed-wing cruising aircraft. Its published specifications support mechanical and electrical integration planning, while the AX-series description outlines cooling and interface features. Procurement should confirm the supplied interface and accessories, reconcile propeller recommendations, and retain the stated power-duration and bench-test qualifications.

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T-MOTOR AX335-B KV425 brushless motor with black ribbed housing, silver end covers and a projecting shaft.
T-MOTOR AX335-B KV425 brushless motor with black ribbed housing, silver end covers and a projecting shaft.
T-MOTOR AX335-B KV425 brushless motor with visible copper windings and a protruding shaft.
T-MOTOR AX335-B KV425 brushless motor with visible copper windings and a protruding shaft.
ModelAX335-B
Test itemKV425Specification table identifies the KV425 version.
Motor weight260gIncludes cable.
Motor dimensionsΦ39*76.5mm
Internal resistance50mΩ
LeadEnameled Wire*120mm

Product overview

The T-MOTOR AX335-B KV425 is a brushless propulsion component intended for fixed-wing cruising aircraft. The AX-series description presents two mechanical interfaces: a built-in rear shaft and an external propeller adapter. It does not explicitly assign either interface to the supplied AX335-B configuration, so mounting selection requires confirmation. Its physical design includes a hollowed, tilted front cover intended to improve cooling airflow, together with large bearings and military wire. These construction claims provide integration context.

Integration planning should account for the published motor envelope, cable-inclusive weight, lead length, shaft entries, battery range and ESC recommendations. The recommendation panel and detailed table give separate propeller guidance, which should be reconciled for the selected installation. This listing describes a motor component; its packing-list text does not enumerate supplied accessories or establish a complete flight platform or airframe kit. Maximum current and power carry duration qualifications. Published bench results are reference values, with surface temperature measured after one minute at full throttle.

Specifications

SpecificationValue & conditions
ModelAX335-B
Test itemKV425Specification table identifies the KV425 version.
Motor weight260gIncludes cable.
Motor dimensionsΦ39*76.5mm
Internal resistance50mΩ
LeadEnameled Wire*120mm
Motor configuration12N14P
Shaft diameterIN:5 OUT:5
Recommended battery/voltage6S-8SManufacturer recommendation; confirm the selected battery and motor configuration.
Rated voltage6-8S LiPoPublished rated voltage specifies a LiPo battery.
Idle current1.7AIdle current specified at 10V.
Peak current60APeak current specified for 180 seconds.
Rated power700W
Maximum power1500W(8S)Maximum power specified for 180 seconds with an 8S battery.
Recommended ESC/propeller60A(6S)/60A(8S)/12*20Manufacturer recommendation lists 60A ESCs for both 6S and 8S, alongside a 12*20 propeller; supplied accessories are not established.
Propeller recommendation12-13 inchesRecommendation panel gives this propeller range; the detailed specification table separately lists 12*20.
Takeoff weight2-3kg
Maximum thrust1.6kg
Mechanical interface designsBuilt-in rear shaft design and external propeller adapter designThe description covers two interface designs.
Cooling architectureHollowed and tilted front coverManufacturer describes the front-cover design as improving incoming airflow and cooling.
Wire and bearingsMilitary wire and large-size bearingsManufacturer construction description and overload-resistance claim.
Bench-test qualificationsReference-only bench data; surface temperature measured after one minute at 100% throttle; comparison with other motor types is not recommended.Applies to the published bench-test data and their temperature measurements.
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