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T-MOTOR AUZ 15*10 fixed-wing UAV propeller

By T-MOTOR ↗

The T-MOTOR AUZ 15*10 is a one-piece carbon-fiber-composite propeller for fixed-wing UAV propulsion, with a PMI foam core and flange mounting interface. Procurement should, motor fit and package contents, while distinguishing recommended operating maxima from published limits and condition-specific manufacturer test data.

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T-MOTOR AUZ 15*10 carbon fiber fixed-wing UAV propeller with two blades and a central mounting hole.
T-MOTOR AUZ 15*10 carbon fiber fixed-wing UAV propeller with two blades and a central mounting hole.
Diameter15 inches (382.5 mm)
MaterialResin-based carbon-fiber composite with PMI foam core
Pitch10 inches (254 mm)
Surface treatmentMatte
Average single-blade weight26 gAverage weight per single blade.
Propeller architectureOne-piece straight propeller

Product overview

The T-MOTOR AUZ 15*10 is a propulsion component for electric fixed-wing UAV integration. Its specified construction combines resin-based carbon-fiber composite with a PMI foam core in a one-piece straight propeller with a matte finish. The manufacturer publishes a 15-inch diameter, 10-inch pitch and average single-blade weight of 26 g; these values should be confirmed for the selected configuration.

Integration centers on a flange mount with an 8 mm center hole and the manufacturer's recommended AT4120 KV250 or AT4120 KV500 motor options. Mounting-hole compatibility still requires verification. Procurement requirements should distinguish the recommended maxima of 7800 RPM and 5.6 kg thrust from the published limits of 8700 RPM and 7 kg. Performance figures are manufacturer test data recorded at 22°C ambient temperature and 25 m altitude, with stated sensitivity to equipment, methodology and environment; they should not be treated as guaranteed installed performance.

Specifications

SpecificationValue & conditions
Diameter15 inches (382.5 mm)
MaterialResin-based carbon-fiber composite with PMI foam core
Pitch10 inches (254 mm)
Surface treatmentMatte
Average single-blade weight26 gAverage weight per single blade.
Propeller architectureOne-piece straight propeller
Recommended maximum RPM7800 RPMRecommended maximum; distinct from the published limit RPM.
ApplicationFixed-wing UAV propeller
Recommended maximum thrust5.6 kgRecommended maximum; distinct from the published limit thrust.
Mounting interfaceFlange mount with Ø8 mm center holeVerify propeller mounting-hole compatibility with the selected motor and consult the manufacturer's drawing.
Limit RPM8700 RPMPublished limit; the recommended maximum is 7800 RPM.
Limit thrust7 kgPublished limit; the recommended maximum thrust is 5.6 kg.
Recommended motor solutionAT4120 KV250 / AT4120 KV500Manufacturer-recommended motor options; verify the mounting interface and selected power-system configuration.
Minimum operating temperature-30°COperating-temperature claim published for the AUZ series; confirm applicability to the selected configuration.
Maximum operating temperature60°COperating-temperature claim published for the AUZ series; confirm applicability to the selected configuration.
Test data at 3100 RPM
  • Torque: 0.20 N·m;
  • thrust: 838 gf;
  • output power: 66.17 W;
  • efficiency: 12.67 gf/W
Manufacturer test data at ambient temperature 22°C and altitude 25 m; results may vary with equipment, methodology, environment and testing standards.
Test data at 3500 RPM
  • Torque: 0.26 N·m;
  • thrust: 1076 gf;
  • output power: 94.65 W;
  • efficiency: 11.37 gf/W
Manufacturer test data at ambient temperature 22°C and altitude 25 m; results may vary with equipment, methodology, environment and testing standards.
Test data at 3900 RPM
  • Torque: 0.32 N·m;
  • thrust: 1345 gf;
  • output power: 130.74 W;
  • efficiency: 10.29 gf/W
Manufacturer test data at ambient temperature 22°C and altitude 25 m; results may vary with equipment, methodology, environment and testing standards.
Test data at 4300 RPM
  • Torque: 0.39 N·m;
  • thrust: 1646 gf;
  • output power: 175.38 W;
  • efficiency: 9.38 gf/W
Manufacturer test data at ambient temperature 22°C and altitude 25 m; results may vary with equipment, methodology, environment and testing standards.
Test data at 4700 RPM
  • Torque: 0.47 N·m;
  • thrust: 1978 gf;
  • output power: 229.49 W;
  • efficiency: 8.62 gf/W
Manufacturer test data at ambient temperature 22°C and altitude 25 m; results may vary with equipment, methodology, environment and testing standards.
Test data at 5100 RPM
  • Torque: 0.55 N·m;
  • thrust: 2342 gf;
  • output power: 294.02 W;
  • efficiency: 7.97 gf/W
Manufacturer test data at ambient temperature 22°C and altitude 25 m; results may vary with equipment, methodology, environment and testing standards.
Test data at 5500 RPM
  • Torque: 0.64 N·m;
  • thrust: 2738 gf;
  • output power: 369.91 W;
  • efficiency: 7.40 gf/W
Manufacturer test data at ambient temperature 22°C and altitude 25 m; results may vary with equipment, methodology, environment and testing standards.
Test data at 5900 RPM
  • Torque: 0.74 N·m;
  • thrust: 3166 gf;
  • output power: 458.08 W;
  • efficiency: 6.91 gf/W
Manufacturer test data at ambient temperature 22°C and altitude 25 m; results may vary with equipment, methodology, environment and testing standards.
Test data at 6300 RPM
  • Torque: 0.85 N·m;
  • thrust: 3625 gf;
  • output power: 559.49 W;
  • efficiency: 6.48 gf/W
Manufacturer test data at ambient temperature 22°C and altitude 25 m; results may vary with equipment, methodology, environment and testing standards.
Test data at 6700 RPM
  • Torque: 0.96 N·m;
  • thrust: 4115 gf;
  • output power: 675.06 W;
  • efficiency: 6.10 gf/W
Manufacturer test data at ambient temperature 22°C and altitude 25 m; results may vary with equipment, methodology, environment and testing standards.
Test data at 7100 RPM
  • Torque: 1.08 N·m;
  • thrust: 4638 gf;
  • output power: 805.74 W;
  • efficiency: 5.76 gf/W
Manufacturer test data at ambient temperature 22°C and altitude 25 m; results may vary with equipment, methodology, environment and testing standards.
Test data at 7500 RPM
  • Torque: 1.21 N·m;
  • thrust: 5192 gf;
  • output power: 952.46 W;
  • efficiency: 5.45 gf/W
Manufacturer test data at ambient temperature 22°C and altitude 25 m; results may vary with equipment, methodology, environment and testing standards.
Test data at 7900 RPM
  • Torque: 1.35 N·m;
  • thrust: 5778 gf;
  • output power: 1116.15 W;
  • efficiency: 5.18 gf/W
Manufacturer test data at ambient temperature 22°C and altitude 25 m; above the recommended maximum RPM and recommended maximum thrust. Results may vary with testing conditions.
Test data at 8300 RPM
  • Torque: 1.49 N·m;
  • thrust: 6396 gf;
  • output power: 1297.76 W;
  • efficiency: 4.93 gf/W
Manufacturer test data at ambient temperature 22°C and altitude 25 m; above the recommended maximum RPM and recommended maximum thrust. Results may vary with testing conditions.
Test data at 8700 RPM
  • Torque: 1.64 N·m;
  • thrust: 7045 gf;
  • output power: 1498.23 W;
  • efficiency: 4.70 gf/W
Manufacturer test data at ambient temperature 22°C and altitude 25 m; at the published limit RPM and above the recommended maximum RPM and thrust. The measured thrust exceeds the separately published 7 kg limit; confirm this discrepancy with the manufacturer.
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