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T-MOTOR AUZ 16*10 fixed-wing UAV propeller

By T-MOTOR ↗

The T-MOTOR AUZ 16*10 is a one-piece carbon fiber composite propeller for electric fixed-wing UAV propulsion. Its published configuration combines a PMI foam core, matte finish and flange mounting. Procurement should verify motor fit, distinguish recommended operating maxima from absolute published limits, and treat the supplied performance data as condition-specific manufacturer measurements.

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T-MOTOR AUZ 16*10 two-blade carbon fiber fixed-wing UAV propeller.
T-MOTOR AUZ 16*10 two-blade carbon fiber fixed-wing UAV propeller.
Diameter16 inches (406.4 mm)
MaterialResin-based carbon fiber composite + PMI foam core
Pitch10 inches (254 mm)
Surface treatmentMatte
Average single-blade weight30.8 gAverage weight per single blade.
Propeller typeOne-piece straight propeller

Product overview

The T-MOTOR AUZ 16*10 is a propulsion component for electric fixed-wing UAVs, rather than a flight platform or airframe kit. Its published configuration is a matte, one-piece straight propeller made from resin-based carbon fiber composite with a PMI foam core. The manufacturer describes integrated molding and a layup intended to resist bending and torsion. The published diameter is 16 inches (406.4 mm), with a 10-inch (254 mm) pitch; buyers should confirm these dimensions for the selected configuration.

Integration centers on a flange mount with a Ø6 mm center hole and the manufacturer’s recommended AT-series motor options. Pitch selection should follow the intended flight envelope. For procurement, distinguish the recommended maxima of 8130 RPM and 6.4 kg thrust from the published limits of 9050 RPM and 8 kg. The performance table reports measurements at 22°C and 25 m altitude, with an explicit warning that equipment, methodology and environment can change results.

Specifications

SpecificationValue & conditions
Diameter16 inches (406.4 mm)
MaterialResin-based carbon fiber composite + PMI foam core
Pitch10 inches (254 mm)
Surface treatmentMatte
Average single-blade weight30.8 gAverage weight per single blade.
Propeller typeOne-piece straight propeller
Recommended maximum RPM8130 RPMRecommended maximum; distinct from the published limit RPM.
ApplicationFixed-wing UAV propeller
Recommended maximum thrust6.4 kgRecommended maximum; distinct from the published limit thrust.
Mounting interfaceFlange mount; Ø6 mm center holeConfirm compatibility between propeller mounting holes and the selected motor; the manufacturer directs users to the technical drawing.
Limit RPM9050 RPMPublished limit; the recommended maximum is 8130 RPM.
Limit thrust8 kgPublished limit; the recommended maximum thrust is 6.4 kg.
Recommended motorsAT4120 KV250 / AT4120 KV500 / AT4125 KV250 / AT4125 KV540 / AT4130 KV230Manufacturer-recommended motor solutions; verify mounting compatibility and the selected configuration.
Operating temperature range−30°C to 60°COperating-temperature endpoints published in the AUZ-series description.
Test data at 3450 RPM
  • Torque: 0.26 N·m;
  • thrust: 1084 gf;
  • output power: 93.32 W;
  • efficiency: 11.62 gf/W
Ambient temperature 22°C; altitude 25 m. Data may vary with testing equipment, methodology and environment.
Test data at 3850 RPM
  • Torque: 0.32 N·m;
  • thrust: 1353 gf;
  • output power: 128.23 W;
  • efficiency: 10.55 gf/W
Ambient temperature 22°C; altitude 25 m. Data may vary with testing equipment, methodology and environment.
Test data at 4250 RPM
  • Torque: 0.39 N·m;
  • thrust: 1657 gf;
  • output power: 171.96 W;
  • efficiency: 9.64 gf/W
Ambient temperature 22°C; altitude 25 m. Data may vary with testing equipment, methodology and environment.
Test data at 4650 RPM
  • Torque: 0.46 N·m;
  • thrust: 1996 gf;
  • output power: 225.56 W;
  • efficiency: 8.85 gf/W
Ambient temperature 22°C; altitude 25 m. Data may vary with testing equipment, methodology and environment.
Test data at 5050 RPM
  • Torque: 0.55 N·m;
  • thrust: 2369 gf;
  • output power: 290.13 W;
  • efficiency: 8.17 gf/W
Ambient temperature 22°C; altitude 25 m. Data may vary with testing equipment, methodology and environment.
Test data at 5450 RPM
  • Torque: 0.64 N·m;
  • thrust: 2777 gf;
  • output power: 366.73 W;
  • efficiency: 7.57 gf/W
Ambient temperature 22°C; altitude 25 m. Data may vary with testing equipment, methodology and environment.
Test data at 5850 RPM
  • Torque: 0.75 N·m;
  • thrust: 3220 gf;
  • output power: 456.44 W;
  • efficiency: 7.05 gf/W
Ambient temperature 22°C; altitude 25 m. Data may vary with testing equipment, methodology and environment.
Test data at 6250 RPM
  • Torque: 0.86 N·m;
  • thrust: 3697 gf;
  • output power: 560.33 W;
  • efficiency: 6.60 gf/W
Ambient temperature 22°C; altitude 25 m. Data may vary with testing equipment, methodology and environment.
Test data at 6650 RPM
  • Torque: 0.98 N·m;
  • thrust: 4209 gf;
  • output power: 679.48 W;
  • efficiency: 6.19 gf/W
Ambient temperature 22°C; altitude 25 m. Data may vary with testing equipment, methodology and environment.
Test data at 7050 RPM
  • Torque: 1.10 N·m;
  • thrust: 4756 gf;
  • output power: 814.96 W;
  • efficiency: 5.84 gf/W
Ambient temperature 22°C; altitude 25 m. Data may vary with testing equipment, methodology and environment.
Test data at 7450 RPM
  • Torque: 1.24 N·m;
  • thrust: 5337 gf;
  • output power: 967.85 W;
  • efficiency: 5.51 gf/W
Ambient temperature 22°C; altitude 25 m. Data may vary with testing equipment, methodology and environment.
Test data at 7850 RPM
  • Torque: 1.39 N·m;
  • thrust: 5953 gf;
  • output power: 1139.21 W;
  • efficiency: 5.23 gf/W
Ambient temperature 22°C; altitude 25 m. Data may vary with testing equipment, methodology and environment.
Test data at 8250 RPM
  • Torque: 1.54 N·m;
  • thrust: 6604 gf;
  • output power: 1330.13 W;
  • efficiency: 4.96 gf/W
Ambient temperature 22°C; altitude 25 m. This test point exceeds the recommended maximum of 8130 RPM. Data may vary with equipment, methodology and environment.
Test data at 8650 RPM
  • Torque: 1.70 N·m;
  • thrust: 7289 gf;
  • output power: 1541.67 W;
  • efficiency: 4.73 gf/W
Ambient temperature 22°C; altitude 25 m. This test point exceeds the recommended maximum of 8130 RPM. Data may vary with equipment, methodology and environment.
Test data at 9050 RPM
  • Torque: 1.87 N·m;
  • thrust: 8009 gf;
  • output power: 1774.92 W;
  • efficiency: 4.51 gf/W
Ambient temperature 22°C; altitude 25 m. This test point reaches the published limit RPM and exceeds the recommended maximum of 8130 RPM. Data may vary with equipment, methodology and environment.
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