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COMPONENT

AUZ 15*8

By T-MOTOR ↗

The T-MOTOR AUZ 15*8 is a one-piece carbon-fiber composite propeller for electric fixed-wing UAVs. It combines a PMI foam core, matte finish and flange mounting with an Ø8 mm center hole. Its 15-inch diameter and 8-inch pitch suit integration with the recommended AT4120 motor options, subject to mounting compatibility and stated speed and thrust limits.

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T-MOTOR AUZ 15*8 two-blade carbon-fiber propeller on a white background
T-MOTOR AUZ 15*8 two-blade carbon-fiber propeller on a white background
ProductT-MOTOR AUZ 15*8 carbon-fiber propeller for fixed-wing UAVs
Diameter15 inches (382.5 mm)
MaterialResin-based carbon-fiber composite with PMI foam core
Pitch8 inches (203.2 mm)
Surface treatmentMatte
Average single-blade weight24 g

Product overview

The T-MOTOR AUZ 15*8 is an electric fixed-wing UAV propulsion component with a one-piece straight propeller architecture. Its configuration combines a 15-inch diameter, 8-inch pitch and matte surface, with an average single-blade weight of 24 g. The structure uses resin-based carbon-fiber composite and a PMI foam core. Its molded construction and fixed-wing-oriented layup are designed to balance weight, stiffness and strength while resisting bending and torsion during flight.

Integration uses a flange mount with an Ø8 mm center hole, and the propeller mounting holes must match the motor. Recommended motor solutions are the AT4120 KV250 and AT4120 KV500. The recommended operating maxima are 8520 RPM and 4.8 kg thrust, distinct from the stated limits of 9470 RPM and 6 kg. The operating temperature range is −30°C to 60°C. Performance figures cover 3170–9470 RPM at an ambient temperature of 22°C and an altitude of 25 m.

Specifications

SpecificationValue & conditions
ProductT-MOTOR AUZ 15*8 carbon-fiber propeller for fixed-wing UAVs
Diameter15 inches (382.5 mm)
MaterialResin-based carbon-fiber composite with PMI foam core
Pitch8 inches (203.2 mm)
Surface treatmentMatte
Average single-blade weight24 g
Propeller architectureOne-piece straight propeller
Recommended maximum rotational speed8520 RPM
ApplicationFixed-wing UAV propeller
Recommended maximum thrust4.8 kg
Mounting interfaceFlange mount with Ø8 mm center holeMounting holes must be compatible with the motor.
Limit rotational speed9470 RPM
Limit thrust6 kg
Recommended motor solutionsAT4120 KV250 / AT4120 KV500
Operating temperature rangeMinimum −30°C; maximum 60°C
Performance at 3170 RPM
  • Torque: 0.13 N·m;
  • thrust: 558 gf;
  • output power: 44.81 W;
  • efficiency: 12.46 gf/W
Ambient temperature 22°C; altitude 25 m.
Performance at 3620 RPM
  • Torque: 0.17 N·m;
  • thrust: 750 gf;
  • output power: 65.19 W;
  • efficiency: 11.51 gf/W
Ambient temperature 22°C; altitude 25 m.
Performance at 4070 RPM
  • Torque: 0.22 N·m;
  • thrust: 972 gf;
  • output power: 91.69 W;
  • efficiency: 10.61 gf/W
Ambient temperature 22°C; altitude 25 m.
Performance at 4520 RPM
  • Torque: 0.26 N·m;
  • thrust: 1225 gf;
  • output power: 125.16 W;
  • efficiency: 9.79 gf/W
Ambient temperature 22°C; altitude 25 m.
Performance at 4970 RPM
  • Torque: 0.32 N·m;
  • thrust: 1508 gf;
  • output power: 166.49 W;
  • efficiency: 9.06 gf/W
Ambient temperature 22°C; altitude 25 m.
Performance at 5420 RPM
  • Torque: 0.38 N·m;
  • thrust: 1821 gf;
  • output power: 216.55 W;
  • efficiency: 8.41 gf/W
Ambient temperature 22°C; altitude 25 m.
Performance at 5870 RPM
  • Torque: 0.45 N·m;
  • thrust: 2164 gf;
  • output power: 276.19 W;
  • efficiency: 7.84 gf/W
Ambient temperature 22°C; altitude 25 m.
Performance at 6320 RPM
  • Torque: 0.52 N·m;
  • thrust: 2538 gf;
  • output power: 346.31 W;
  • efficiency: 7.33 gf/W
Ambient temperature 22°C; altitude 25 m.
Performance at 6770 RPM
  • Torque: 0.60 N·m;
  • thrust: 2942 gf;
  • output power: 427.75 W;
  • efficiency: 6.88 gf/W
Ambient temperature 22°C; altitude 25 m.
Performance at 7220 RPM
  • Torque: 0.69 N·m;
  • thrust: 3376 gf;
  • output power: 521.40 W;
  • efficiency: 6.47 gf/W
Ambient temperature 22°C; altitude 25 m.
Performance at 7670 RPM
  • Torque: 0.78 N·m;
  • thrust: 3841 gf;
  • output power: 628.13 W;
  • efficiency: 6.11 gf/W
Ambient temperature 22°C; altitude 25 m.
Performance at 8120 RPM
  • Torque: 0.88 N·m;
  • thrust: 4336 gf;
  • output power: 748.81 W;
  • efficiency: 5.79 gf/W
Ambient temperature 22°C; altitude 25 m.
Performance at 8570 RPM
  • Torque: 0.99 N·m;
  • thrust: 4861 gf;
  • output power: 884.30 W;
  • efficiency: 5.50 gf/W
Ambient temperature 22°C; altitude 25 m.
Performance at 9020 RPM
  • Torque: 1.10 N·m;
  • thrust: 5416 gf;
  • output power: 1035.48 W;
  • efficiency: 5.23 gf/W
Ambient temperature 22°C; altitude 25 m.
Performance at 9470 RPM
  • Torque: 1.21 N·m;
  • thrust: 6002 gf;
  • output power: 1203.21 W;
  • efficiency: 4.99 gf/W
Ambient temperature 22°C; altitude 25 m.
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