T-MOTOR AUZ 24*12

The T-MOTOR AUZ 24*12 is a 24-inch, one-piece carbon-fiber propeller for fixed-wing UAVs. Built with a resin-based carbon-fiber composite and PMI sandwich core, it features a matte finish, 12-inch pitch and center-locking attachment for a Ø10mm motor shaft.

T-MOTORDrone motor

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

Product overview

The T-MOTOR AUZ 24*12 is a one-piece carbon-fiber propeller for fixed-wing UAVs, with a 24-inch (609.6mm) diameter and 12-inch (304.8mm) pitch. Its resin-based carbon-fiber composite structure incorporates a PMI sandwich core, combining prepreg materials with one-piece compression molding. A matte finish completes the propeller, which has an average individual weight of 80 g. The center-locking mounting arrangement fits a Ø10mm motor shaft, and recommended motor combinations pair the AUZ24*12 with the AT7224, AT8020 or AT8030.

The propeller has a recommended maximum rotational speed of 7350 RPM and recommended maximum thrust of 24 kg. Its limit speed is 8200 RPM, with a limit thrust of 30 kg, and its operating temperature range extends from -30°C to 60°C. At an ambient temperature of 22 °C and altitude of 25 m, test performance at 5400 RPM is 12513 gf thrust, 2197.20 W output power, 3.89 N·m torque and 5.69 gf/W thrust efficiency. Test data are subject to variation with equipment, methods, environment and testing standards.

Motors & ESCs

Specifications

T-MOTOR AUZ 24*12 specifications
Specification	Value & conditions
Diameter	24 inches (609.6mm)
Material	Resin-based carbon-fiber composite with PMI sandwich core
Pitch	12 inches (304.8mm)
Surface finish	Matte
Average weight	80 gPer individual propeller.
Product type	One-piece carbon-fiber propeller
Recommended maximum speed	7350 RPM
Application	Fixed-wing UAVs
Recommended maximum thrust	24 kg
Mounting method and size	Center locking on a Ø10mm motor shaft
Limit speed	8200 RPM
Recommended motor combinations	AT7224, AT8020 or AT8030 with AUZ2412AUZ2412 propeller.
Limit thrust	30 kg
Operating temperature	-30°C minimum; 60°C maximum
Manufacturing construction	Prepreg with PMI core, compression molded as one piece
Performance at 3300 RPM	Torque 1.35 N·m; thrust 4399 gf; output power 465.48 W; thrust efficiency 9.45 gf/WAmbient temperature 22 °C; altitude 25 m. Test data are subject to variation with equipment, methods, environment and testing standards.
Performance at 3650 RPM	Torque 1.67 N·m; thrust 5437 gf; output power 636.81 W; thrust efficiency 8.54 gf/WAmbient temperature 22 °C; altitude 25 m. Test data are subject to variation with equipment, methods, environment and testing standards.
Performance at 4000 RPM	Torque 2.03 N·m; thrust 6601 gf; output power 848.95 W; thrust efficiency 7.78 gf/WAmbient temperature 22 °C; altitude 25 m. Test data are subject to variation with equipment, methods, environment and testing standards.
Performance at 4350 RPM	Torque 2.43 N·m; thrust 7890 gf; output power 1106.49 W; thrust efficiency 7.13 gf/WAmbient temperature 22 °C; altitude 25 m. Test data are subject to variation with equipment, methods, environment and testing standards.
Performance at 4700 RPM	Torque 2.87 N·m; thrust 9306 gf; output power 1413.99 W; thrust efficiency 6.58 gf/WAmbient temperature 22 °C; altitude 25 m. Test data are subject to variation with equipment, methods, environment and testing standards.
Performance at 5050 RPM	Torque 3.36 N·m; thrust 10846 gf; output power 1776.04 W; thrust efficiency 6.11 gf/WAmbient temperature 22 °C; altitude 25 m. Test data are subject to variation with equipment, methods, environment and testing standards.
Performance at 5400 RPM	Torque 3.89 N·m; thrust 12513 gf; output power 2197.20 W; thrust efficiency 5.69 gf/WAmbient temperature 22 °C; altitude 25 m. Test data are subject to variation with equipment, methods, environment and testing standards.
Performance at 5750 RPM	Torque 4.45 N·m; thrust 14304 gf; output power 2682.04 W; thrust efficiency 5.33 gf/WAmbient temperature 22 °C; altitude 25 m. Test data are subject to variation with equipment, methods, environment and testing standards.
Performance at 6100 RPM	Torque 5.06 N·m; thrust 16222 gf; output power 3235.16 W; thrust efficiency 5.01 gf/WAmbient temperature 22 °C; altitude 25 m. Test data are subject to variation with equipment, methods, environment and testing standards.
Performance at 6450 RPM	Torque 5.72 N·m; thrust 18265 gf; output power 3861.11 W; thrust efficiency 4.73 gf/WAmbient temperature 22 °C; altitude 25 m. Test data are subject to variation with equipment, methods, environment and testing standards.
Performance at 6800 RPM	Torque 6.41 N·m; thrust 20434 gf; output power 4564.48 W; thrust efficiency 4.48 gf/WAmbient temperature 22 °C; altitude 25 m. Test data are subject to variation with equipment, methods, environment and testing standards.
Performance at 7150 RPM	Torque 7.15 N·m; thrust 22728 gf; output power 5349.84 W; thrust efficiency 4.25 gf/WAmbient temperature 22 °C; altitude 25 m. Test data are subject to variation with equipment, methods, environment and testing standards.
Performance at 7500 RPM	Torque 7.92 N·m; thrust 25148 gf; output power 6221.76 W; thrust efficiency 4.04 gf/WAmbient temperature 22 °C; altitude 25 m. Test data are subject to variation with equipment, methods, environment and testing standards.
Performance at 7850 RPM	Torque 8.74 N·m; thrust 27694 gf; output power 7184.81 W; thrust efficiency 3.85 gf/WAmbient temperature 22 °C; altitude 25 m. Test data are subject to variation with equipment, methods, environment and testing standards.
Performance at 8200 RPM	Torque 9.60 N·m; thrust 30365 gf; output power 8243.59 W; thrust efficiency 3.68 gf/WAmbient temperature 22 °C; altitude 25 m. Test data are subject to variation with equipment, methods, environment and testing standards.