Product overview
The T-MOTOR VZ24*8.2 is a propulsion component for VTOL fixed-wing UAVs operating in multicopter mode, including logistics delivery applications. Its one-piece straight architecture combines a resin-based carbon fiber composite structure with a PMI foam core and matte finish. The propeller measures 24 inches (609.6 mm) in diameter with an 8.2-inch (208.3 mm) pitch, and its average single-blade weight is 54 g. This configuration brings the VZ series’ emphasis on stiffness and weight control to the aircraft’s vertical-lift propulsion installation.
Integration centers on a flange mount with a Ø10 mm center hole, Ø18 mm and Ø20 mm bolt circles, and six Ø3 mm mounting holes; the motor interface must match these dimensions. The recommended propulsion solution is VL7015+KV190+V80A. Recommended maximum operation is 6800 RPM and 16.8 kg thrust, with separate limits of 7600 RPM and 21 kg thrust. At 22 °C and 25 m altitude, the performance table gives 16887 gf thrust at 6800 RPM, requiring 3223.15 W of output power.
Specifications
| Specification | Value & conditions |
|---|---|
| Diameter | 24 inches (609.6 mm) |
| Material | Resin-based carbon fiber composite + PMI foam core |
| Pitch | 8.2 inches (208.3 mm) |
| Surface treatment | Matte |
| Average single-blade weight | 54 g |
| Propeller architecture | One-piece straight propeller |
| Recommended maximum speed | 6800 RPM |
| Application | VTOL fixed-wing UAVs, multicopter mode |
| Recommended maximum thrust | 16.8 kg |
| Mounting interface | Flange mount; Ø10 mm center hole; Ø18 mm and Ø20 mm bolt circles; six Ø3 mm mounting holes |
| Limit speed | 7600 RPM |
| Recommended propulsion solution | VL7015+KV190+V80A |
| Limit thrust | 21 kg |
| Performance at 2000 RPM | Torque 0.43 N·m; thrust 1434 gf; output power 89.31 W; efficiency 16.05 gf/WAmbient temperature 22 °C; altitude 25 m; rotational speed 2000 RPM. |
| Performance at 2400 RPM | Torque 0.54 N·m; thrust 1940 gf; output power 135.85 W; efficiency 14.28 gf/WAmbient temperature 22 °C; altitude 25 m; rotational speed 2400 RPM. |
| Performance at 2800 RPM | Torque 0.70 N·m; thrust 2588 gf; output power 204.08 W; efficiency 12.68 gf/WAmbient temperature 22 °C; altitude 25 m; rotational speed 2800 RPM. |
| Performance at 3200 RPM | Torque 0.89 N·m; thrust 3379 gf; output power 299.21 W; efficiency 11.29 gf/WAmbient temperature 22 °C; altitude 25 m; rotational speed 3200 RPM. |
| Performance at 3600 RPM | Torque 1.13 N·m; thrust 4311 gf; output power 426.42 W; efficiency 10.11 gf/WAmbient temperature 22 °C; altitude 25 m; rotational speed 3600 RPM. |
| Performance at 4000 RPM | Torque 1.41 N·m; thrust 5386 gf; output power 590.91 W; efficiency 9.11 gf/WAmbient temperature 22 °C; altitude 25 m; rotational speed 4000 RPM. |
| Performance at 4400 RPM | Torque 1.73 N·m; thrust 6602 gf; output power 797.90 W; efficiency 8.27 gf/WAmbient temperature 22 °C; altitude 25 m; rotational speed 4400 RPM. |
| Performance at 4800 RPM | Torque 2.09 N·m; thrust 7961 gf; output power 1052.57 W; efficiency 7.56 gf/WAmbient temperature 22 °C; altitude 25 m; rotational speed 4800 RPM. |
| Performance at 5200 RPM | Torque 2.50 N·m; thrust 9462 gf; output power 1360.12 W; efficiency 6.96 gf/WAmbient temperature 22 °C; altitude 25 m; rotational speed 5200 RPM. |
| Performance at 5600 RPM | Torque 2.94 N·m; thrust 11105 gf; output power 1725.76 W; efficiency 6.43 gf/WAmbient temperature 22 °C; altitude 25 m; rotational speed 5600 RPM. |
| Performance at 6000 RPM | Torque 3.43 N·m; thrust 12890 gf; output power 2154.67 W; efficiency 5.98 gf/WAmbient temperature 22 °C; altitude 25 m; rotational speed 6000 RPM. |
| Performance at 6400 RPM | Torque 3.96 N·m; thrust 14817 gf; output power 2652.07 W; efficiency 5.59 gf/WAmbient temperature 22 °C; altitude 25 m; rotational speed 6400 RPM. |
| Performance at 6800 RPM | Torque 4.53 N·m; thrust 16887 gf; output power 3223.15 W; efficiency 5.24 gf/WAmbient temperature 22 °C; altitude 25 m; rotational speed 6800 RPM. |
| Performance at 7200 RPM | Torque 5.14 N·m; thrust 19098 gf; output power 3873.11 W; efficiency 4.93 gf/WAmbient temperature 22 °C; altitude 25 m; rotational speed 7200 RPM. |
| Performance at 7600 RPM | Torque 5.79 N·m; thrust 21452 gf; output power 4607.15 W; efficiency 4.66 gf/WAmbient temperature 22 °C; altitude 25 m; rotational speed 7600 RPM. |
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