T-MOTOR AUZ 17*12

The T-MOTOR AUZ 17*12 is a 17-inch, one-piece carbon-fiber propeller for electric fixed-wing UAVs and long-endurance cruising. Its matte composite structure incorporates a PMI sandwich core, weighs an average of 35 g per propeller and mounts through a center-locking connection on a Ø8mm motor shaft.

T-MOTORDrone motor

Material: Resin-based carbon-fiber composite with PMI sandwich core

Product overview

The T-MOTOR AUZ 17*12 is a one-piece carbon-fiber propeller for electric fixed-wing UAVs and long-endurance cruising. Its 17-inch (431.8mm) diameter and 12-inch (304.8mm) pitch combine with an average weight of 35 g per propeller. A resin-based carbon-fiber composite surrounds a PMI sandwich core, with prepreg compression-molded into a single structure and finished in matte. The laminate uses fiber orientations designed to resist bending and twisting under fixed-wing flight loads. Product porosity is below 1%.

A center-locking connection fits a Ø8mm motor shaft, and the recommended propulsion pairing is AT4130 + AUZ17*12. Recommended maximum speed is 9000 RPM, with recommended maximum thrust of 9.6 kg; limit speed is 10200 RPM and limit thrust is 12 kg. The operating temperature range is -30°C to 60°C. At 22 °C ambient temperature and 25 m altitude, the 9000 RPM test point delivers 9638 gf thrust at 2974.08 W output power and 3.24 gf/W thrust efficiency. Results vary with test equipment, methods, environment and test standards.

Motors & ESCs

Specifications

T-MOTOR AUZ 17*12 specifications
Specification	Value & conditions
Diameter	17 inches (431.8mm)
Material	Resin-based carbon-fiber composite with PMI sandwich core
Pitch	12 inches (304.8mm)
Surface finish	Matte
Average weight per propeller	35 g
Product type	One-piece carbon-fiber propeller
Recommended maximum speed	9000 RPM
Application	Fixed-wing UAVs
Recommended maximum thrust	9.6 kg
Mounting method and size	Center locking on a Ø8mm motor shaft
Limit speed	10200 RPM
Recommended motor and propeller pairing	AT4130 + AUZ17*12
Limit thrust	12 kg
Operating temperature	-30°C to 60°C
Manufacturing process and porosity	Prepreg and PMI core formed by one-piece compression molding; product porosity below 1%
Performance at 4600 RPM	Torque: 0.67 N·m; thrust: 2569 gf; output power: 322.37 W; thrust efficiency: 7.97 gf/W Ambient temperature 22 °C; altitude 25 m; speed 4600 RPM. Results vary with test equipment, methods, environment and test standards.
Performance at 5000 RPM	Torque: 0.79 N·m; thrust: 3068 gf; output power: 411.83 W; thrust efficiency: 7.45 gf/W Ambient temperature 22 °C; altitude 25 m; speed 5000 RPM. Results vary with test equipment, methods, environment and test standards.
Performance at 5400 RPM	Torque: 0.93 N·m; thrust: 3595 gf; output power: 523.41 W; thrust efficiency: 6.87 gf/W Ambient temperature 22 °C; altitude 25 m; speed 5400 RPM. Results vary with test equipment, methods, environment and test standards.
Performance at 5800 RPM	Torque: 1.09 N·m; thrust: 4152 gf; output power: 659.85 W; thrust efficiency: 6.29 gf/W Ambient temperature 22 °C; altitude 25 m; speed 5800 RPM. Results vary with test equipment, methods, environment and test standards.
Performance at 6200 RPM	Torque: 1.27 N·m; thrust: 4737 gf; output power: 823.88 W; thrust efficiency: 5.75 gf/W Ambient temperature 22 °C; altitude 25 m; speed 6200 RPM. Results vary with test equipment, methods, environment and test standards.
Performance at 6600 RPM	Torque: 1.47 N·m; thrust: 5351 gf; output power: 1018.23 W; thrust efficiency: 5.25 gf/W Ambient temperature 22 °C; altitude 25 m; speed 6600 RPM. Results vary with test equipment, methods, environment and test standards.
Performance at 7000 RPM	Torque: 1.70 N·m; thrust: 5993 gf; output power: 1245.63 W; thrust efficiency: 4.81 gf/W Ambient temperature 22 °C; altitude 25 m; speed 7000 RPM. Results vary with test equipment, methods, environment and test standards.
Performance at 7400 RPM	Torque: 1.95 N·m; thrust: 6665 gf; output power: 1508.82 W; thrust efficiency: 4.42 gf/W Ambient temperature 22 °C; altitude 25 m; speed 7400 RPM. Results vary with test equipment, methods, environment and test standards.
Performance at 7800 RPM	Torque: 2.22 N·m; thrust: 7365 gf; output power: 1810.53 W; thrust efficiency: 4.07 gf/W Ambient temperature 22 °C; altitude 25 m; speed 7800 RPM. Results vary with test equipment, methods, environment and test standards.
Performance at 8200 RPM	Torque: 2.51 N·m; thrust: 8094 gf; output power: 2153.48 W; thrust efficiency: 3.76 gf/W Ambient temperature 22 °C; altitude 25 m; speed 8200 RPM. Results vary with test equipment, methods, environment and test standards.
Performance at 8600 RPM	Torque: 2.82 N·m; thrust: 8851 gf; output power: 2540.42 W; thrust efficiency: 3.48 gf/W Ambient temperature 22 °C; altitude 25 m; speed 8600 RPM. Results vary with test equipment, methods, environment and test standards.
Performance at 9000 RPM	Torque: 3.16 N·m; thrust: 9638 gf; output power: 2974.08 W; thrust efficiency: 3.24 gf/W Ambient temperature 22 °C; altitude 25 m; speed 9000 RPM. Results vary with test equipment, methods, environment and test standards.
Performance at 9400 RPM	Torque: 3.51 N·m; thrust: 10453 gf; output power: 3457.18 W; thrust efficiency: 3.02 gf/W Ambient temperature 22 °C; altitude 25 m; speed 9400 RPM. Results vary with test equipment, methods, environment and test standards.
Performance at 9800 RPM	Torque: 3.89 N·m; thrust: 11297 gf; output power: 3992.46 W; thrust efficiency: 2.83 gf/W Ambient temperature 22 °C; altitude 25 m; speed 9800 RPM. Results vary with test equipment, methods, environment and test standards.
Performance at 10200 RPM	Torque: 4.29 N·m; thrust: 12170 gf; output power: 4582.65 W; thrust efficiency: 2.66 gf/W Ambient temperature 22 °C; altitude 25 m; speed 10200 RPM. Results vary with test equipment, methods, environment and test standards.