T-MOTOR AUZ 26*12

The T-MOTOR AUZ 26*12 is a one-piece carbon-fiber composite propeller for electric fixed-wing UAVs. Its 26-inch diameter and 12-inch pitch combine with a PMI sandwich core and matte finish. Average weight is 104 g per propeller, with AT8030 KV160 and AT1030 KV90 recommended as motor pairings.

T-MOTORDrone motor

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

Product overview

The T-MOTOR AUZ 26*12 is a one-piece straight propeller for electric fixed-wing UAVs, with a 26-inch diameter and 12-inch pitch. Its resin-based carbon-fiber composite construction incorporates a PMI sandwich core, using prepreg and one-piece compression molding. The propeller has a matte finish and an average weight of 104 g per propeller. Its mounting interface uses a propeller-hub flange with a Ø10mm center hole and six Ø5mm mounting holes arranged on a Ø29mm bolt circle.

Recommended motor pairings are the AT8030 KV160 and AT1030 KV90. Recommended maximum speed is 6920 RPM and recommended maximum thrust is 28.8 kg; limit speed is 7800 RPM and limit thrust is 36 kg. The operating temperature range is -30°C to 60°C. At 6900 RPM, 22 °C ambient temperature and 25 m altitude, test results are 28687 gf thrust, 10.23 N·m torque, 7393.05 W output power and 3.88 gf/W thrust efficiency. Test data can vary with equipment, methods, environment and testing standards.

Motors & ESCs

Specifications

T-MOTOR AUZ 26*12 specifications
Specification	Value & conditions
Diameter	26 inches (660.9mm)
Material	Resin-based carbon-fiber composite with PMI sandwich core
Pitch	12 inches (304.8mm)
Surface finish	Matte
Average weight	104 gPer propeller.
Type	One-piece straight propeller
Recommended maximum speed	6920 RPM
Application	Fixed-wing UAVs
Recommended maximum thrust	28.8 kg
Mounting interface	Propeller-hub flange connection; Ø10mm center hole; Ø29mm bolt circle; six Ø5mm mounting holes
Limit speed	7800 RPM
Limit thrust	36 kg
Recommended motors	AT8030 KV160 / AT1030 KV90
Operating temperature	-30°C to 60°C
Construction process	Prepreg and PMI core with one-piece compression molding
Performance at 3600 RPM	Torque: 2.44 N·m; thrust: 7266 gf; output power: 921.22 W; thrust efficiency: 7.89 gf/W 3600 RPM; ambient temperature 22 °C; altitude 25 m. Test data can vary with equipment, methods, environment and testing standards.
Performance at 3900 RPM	Torque: 2.84 N·m; thrust: 8820 gf; output power: 1160.99 W; thrust efficiency: 7.60 gf/W 3900 RPM; ambient temperature 22 °C; altitude 25 m. Test data can vary with equipment, methods, environment and testing standards.
Performance at 4200 RPM	Torque: 3.30 N·m; thrust: 10452 gf; output power: 1453.01 W; thrust efficiency: 7.19 gf/W 4200 RPM; ambient temperature 22 °C; altitude 25 m. Test data can vary with equipment, methods, environment and testing standards.
Performance at 4500 RPM	Torque: 3.83 N·m; thrust: 12164 gf; output power: 1803.10 W; thrust efficiency: 6.75 gf/W 4500 RPM; ambient temperature 22 °C; altitude 25 m. Test data can vary with equipment, methods, environment and testing standards.
Performance at 4800 RPM	Torque: 4.41 N·m; thrust: 13954 gf; output power: 2217.09 W; thrust efficiency: 6.29 gf/W 4800 RPM; ambient temperature 22 °C; altitude 25 m. Test data can vary with equipment, methods, environment and testing standards.
Performance at 5100 RPM	Torque: 5.06 N·m; thrust: 15822 gf; output power: 2700.79 W; thrust efficiency: 5.86 gf/W 5100 RPM; ambient temperature 22 °C; altitude 25 m. Test data can vary with equipment, methods, environment and testing standards.
Performance at 5400 RPM	Torque: 5.76 N·m; thrust: 17770 gf; output power: 3260.03 W; thrust efficiency: 5.45 gf/W 5400 RPM; ambient temperature 22 °C; altitude 25 m. Test data can vary with equipment, methods, environment and testing standards.
Performance at 5700 RPM	Torque: 6.53 N·m; thrust: 19796 gf; output power: 3900.62 W; thrust efficiency: 5.08 gf/W 5700 RPM; ambient temperature 22 °C; altitude 25 m. Test data can vary with equipment, methods, environment and testing standards.
Performance at 6000 RPM	Torque: 7.37 N·m; thrust: 21901 gf; output power: 4628.40 W; thrust efficiency: 4.73 gf/W 6000 RPM; ambient temperature 22 °C; altitude 25 m. Test data can vary with equipment, methods, environment and testing standards.
Performance at 6300 RPM	Torque: 8.26 N·m; thrust: 24084 gf; output power: 5449.18 W; thrust efficiency: 4.42 gf/W 6300 RPM; ambient temperature 22 °C; altitude 25 m. Test data can vary with equipment, methods, environment and testing standards.
Performance at 6600 RPM	Torque: 9.21 N·m; thrust: 26346 gf; output power: 6368.79 W; thrust efficiency: 4.14 gf/W 6600 RPM; ambient temperature 22 °C; altitude 25 m. Test data can vary with equipment, methods, environment and testing standards.
Performance at 6900 RPM	Torque: 10.23 N·m; thrust: 28687 gf; output power: 7393.05 W; thrust efficiency: 3.88 gf/W 6900 RPM; ambient temperature 22 °C; altitude 25 m. Test data can vary with equipment, methods, environment and testing standards.
Performance at 7200 RPM	Torque: 11.31 N·m; thrust: 31106 gf; output power: 8527.77 W; thrust efficiency: 3.65 gf/W 7200 RPM; ambient temperature 22 °C; altitude 25 m. Test data can vary with equipment, methods, environment and testing standards.
Performance at 7500 RPM	Torque: 12.45 N·m; thrust: 33605 gf; output power: 9778.79 W; thrust efficiency: 3.44 gf/W 7500 RPM; ambient temperature 22 °C; altitude 25 m. Test data can vary with equipment, methods, environment and testing standards.
Performance at 7800 RPM	Torque: 13.65 N·m; thrust: 36182 gf; output power: 11151.93 W; thrust efficiency: 3.24 gf/W 7800 RPM; ambient temperature 22 °C; altitude 25 m. Test data can vary with equipment, methods, environment and testing standards.