T-MOTOR AUZ 26*16

The T-MOTOR AUZ 26*16 is a carbon-fiber propeller for electric fixed-wing UAVs. Its one-piece construction combines a resin-based composite with a PMI core, a matte finish and flange mounting. A dedicated airfoil and optimized mass distribution support aerodynamic efficiency and responsive speed changes across conventional, flying-wing and VTOL layouts.

T-MOTORDrone motor

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

Product overview

The T-MOTOR AUZ 26*16 is a one-piece straight propeller for electric fixed-wing UAVs, with a 26-inch (660.9mm) diameter and 16-inch (406.4mm) pitch. Its dedicated airfoil improves aerodynamic efficiency and reduces noise, while optimized mass distribution lowers rotational inertia for faster acceleration and deceleration response. Applications include surveying, logistics delivery, power-line inspection, agricultural crop protection, emergency rescue and security monitoring. It supports conventional fixed-wing, flying-wing and VTOL layouts, with AT8030 KV160 and AT1030 KV90 motors recommended.

The matte-finished propeller combines resin-based carbon-fiber composite with a PMI sandwich core. Its fixed-wing-specific layup uses prepreg and integral compression molding, with porosity below 1% and an average individual weight of 100 g. The flange interface has a Ø10mm center hole and six Ø5mm mounting holes on a Ø29mm bolt circle. Recommended maxima are 6830 RPM and 32 kg thrust; limit values are 7650 RPM and 40 kg. Operating temperature spans -30°C to 60°C, with moisture resistance, salt-spray protection and UV resistance.

Motors & ESCs

Specifications

T-MOTOR AUZ 26*16 specifications
Specification	Value & conditions
Product	T-MOTOR AUZ 26*16 carbon-fiber fixed-wing UAV propeller
Diameter	26 inches (660.9mm)
Material	Resin-based carbon-fiber composite with a PMI sandwich core
Pitch	16 inches (406.4mm)
Surface finish	Matte
Average individual propeller weight	100 g
Type	One-piece straight propeller
Recommended maximum rotational speed	6830 RPM
Application	Fixed-wing UAVs
Recommended maximum thrust	32 kg
Mounting interface	Propeller-hub flange connection; Ø10mm center hole; Ø29mm bolt circle; six Ø5mm mounting holes
Limit rotational speed	7650 RPM
Limit thrust	40 kg
Recommended motors	AT8030 KV160 / AT1030 KV90
Construction process	Layup designed for fixed-wing flight conditions, using prepreg, a PMI core and integral compression molding
Porosity	Below 1%
Operating temperature	-30°C to 60°C
Environmental protection	Moisture resistance, salt-spray protection and UV resistance
Aircraft layouts	Conventional fixed-wing, flying-wing and VTOL UAV layouts
Mission applications	Surveying and exploration, logistics delivery, power-line inspection, agricultural crop protection, emergency rescue and security monitoring
Aerodynamic design	Dedicated airfoil developed for electric fixed-wing UAVs to improve aerodynamic efficiency and reduce noise
Dynamic response design	Optimized center-of-mass distribution and reduced rotational inertia for faster acceleration and deceleration response
Performance measurements	RPM \| Torque (N·m) \| Thrust (gf) \| Output power (W) \| Thrust efficiency (gf/W) 2750 \| 1.82 \| 5119 \| 525.45 \| 9.74 3100 \| 2.28 \| 6611 \| 739.39 \| 8.94 3450 \| 2.84 \| 8256 \| 1024.68 \| 8.06 3800 \| 3.50 \| 10055 \| 1392.91 \| 7.22 4150 \| 4.27 \| 12009 \| 1855.71 \| 6.47 4500 \| 5.15 \| 14116 \| 2424.67 \| 5.82 4850 \| 6.13 \| 16377 \| 3111.40 \| 5.26 5200 \| 7.21 \| 18792 \| 3927.51 \| 4.78 5550 \| 8.40 \| 21360 \| 4884.61 \| 4.37 5900 \| 9.70 \| 24083 \| 5994.30 \| 4.02 6250 \| 11.10 \| 26960 \| 7268.19 \| 3.71 6600 \| 12.61 \| 29990 \| 8717.89 \| 3.44 6950 \| 14.23 \| 33175 \| 10355.00 \| 3.20 7300 \| 15.95 \| 36513 \| 12191.12 \| 3.00 7650 \| 17.77 \| 40005 \| 14237.88 \| 2.81Ambient temperature 22 °C; altitude 25 m. Measurements are subject to variation with test equipment, methods, environment and testing standards.