T-MOTOR AUZ 20*10

The T-MOTOR AUZ 20*10 is a one-piece carbon-fiber propeller for electric fixed-wing UAVs. It combines a resin-based composite structure with a PMI sandwich core, matte finish and flange mounting interface. Its 20-inch diameter and 10-inch pitch are paired with recommended AT7215 motor options.

T-MOTORDrone motor

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

Product overview

The T-MOTOR AUZ 20*10 is a one-piece straight propeller for electric fixed-wing UAVs, with a 20-inch (510mm) diameter and 10-inch (254mm) pitch. Its matte-finished carbon-fiber composite structure incorporates a PMI sandwich core and weighs an average of 45.4 g per propeller. A propeller-hub flange connection with a Ø10mm center hole provides the mounting interface. Recommended motor pairings are the AT7215 KV200, KV220, KV245 and KV270. Recommended maximum speed is 7940 RPM, with recommended maximum thrust of 13.6 kg.

Prepreg compression molding forms the integrated structure, with porosity below 1%. The propeller operates from -30°C to 60°C. Its limit speed is 9050 RPM and limit thrust is 17 kg. Performance measurements at an ambient temperature of 22 °C and altitude of 25 m cover speeds from 4150 to 9050 RPM. At 4150 RPM, thrust is 3688 gf with 416.14 W output power and 8.86 gf/W thrust efficiency; at 9050 RPM, these values are 17083 gf, 5471.93 W and 3.12 gf/W.

Motors & ESCs

Specifications

T-MOTOR AUZ 20*10 specifications
Specification	Value & conditions
Diameter	20 inches (510mm)
Material	Resin-based carbon-fiber composite with a PMI sandwich core
Pitch	10 inches (254mm)
Surface finish	Matte
Average weight per propeller	45.4 g
Propeller type	One-piece straight propeller
Recommended maximum speed	7940 RPM
Application	Fixed-wing UAVs
Recommended maximum thrust	13.6 kg
Mounting interface	Propeller-hub flange connection; Ø10mm center hole
Limit speed	9050 RPM
Limit thrust	17 kg
Recommended motors	AT7215 KV200 / AT7215 KV220 / AT7215 KV245 / AT7215 KV270
Operating temperature	Minimum -30°C; maximum 60°C
Porosity	Below 1%Prepreg compression-molded construction.
Performance at 4150 RPM	Torque 0.96 N·m; thrust 3688 gf; output power 416.14 W; thrust efficiency 8.86 gf/W4150 RPM; ambient temperature 22 °C; altitude 25 m.
Performance at 4500 RPM	Torque 1.12 N·m; thrust 4476 gf; output power 527.43 W; thrust efficiency 8.49 gf/W4500 RPM; ambient temperature 22 °C; altitude 25 m.
Performance at 4850 RPM	Torque 1.31 N·m; thrust 5289 gf; output power 664.82 W; thrust efficiency 7.96 gf/W4850 RPM; ambient temperature 22 °C; altitude 25 m.
Performance at 5200 RPM	Torque 1.53 N·m; thrust 6129 gf; output power 831.39 W; thrust efficiency 7.37 gf/W5200 RPM; ambient temperature 22 °C; altitude 25 m.
Performance at 5550 RPM	Torque 1.77 N·m; thrust 6995 gf; output power 1030.23 W; thrust efficiency 6.79 gf/W5550 RPM; ambient temperature 22 °C; altitude 25 m.
Performance at 5900 RPM	Torque 2.05 N·m; thrust 7887 gf; output power 1264.42 W; thrust efficiency 6.24 gf/W5900 RPM; ambient temperature 22 °C; altitude 25 m.
Performance at 6250 RPM	Torque 2.35 N·m; thrust 8805 gf; output power 1537.05 W; thrust efficiency 5.73 gf/W6250 RPM; ambient temperature 22 °C; altitude 25 m.
Performance at 6600 RPM	Torque 2.68 N·m; thrust 9748 gf; output power 1851.20 W; thrust efficiency 5.27 gf/W6600 RPM; ambient temperature 22 °C; altitude 25 m.
Performance at 6950 RPM	Torque 3.04 N·m; thrust 10718 gf; output power 2209.96 W; thrust efficiency 4.85 gf/W6950 RPM; ambient temperature 22 °C; altitude 25 m.
Performance at 7300 RPM	Torque 3.42 N·m; thrust 11714 gf; output power 2616.40 W; thrust efficiency 4.48 gf/W7300 RPM; ambient temperature 22 °C; altitude 25 m.
Performance at 7650 RPM	Torque 3.84 N·m; thrust 12736 gf; output power 3073.62 W; thrust efficiency 4.14 gf/W7650 RPM; ambient temperature 22 °C; altitude 25 m.
Performance at 8000 RPM	Torque 4.28 N·m; thrust 13784 gf; output power 3584.70 W; thrust efficiency 3.85 gf/W8000 RPM; ambient temperature 22 °C; altitude 25 m.
Performance at 8350 RPM	Torque 4.75 N·m; thrust 14858 gf; output power 4152.72 W; thrust efficiency 3.58 gf/W8350 RPM; ambient temperature 22 °C; altitude 25 m.
Performance at 8700 RPM	Torque 5.25 N·m; thrust 15957 gf; output power 4780.77 W; thrust efficiency 3.34 gf/W8700 RPM; ambient temperature 22 °C; altitude 25 m.
Performance at 9050 RPM	Torque 5.77 N·m; thrust 17083 gf; output power 5471.93 W; thrust efficiency 3.12 gf/W9050 RPM; ambient temperature 22 °C; altitude 25 m.