Product overview
The YRDRONE LJ8020 KV180 is a brushless propulsion motor for fixed-wing drones, including VTOL UAV aircraft. Its cylindrical dimensions are 90 +/-0.1 mm in diameter and 75.8 +/-0.3 mm in length, with a weight of 883 +/-15 g. The motor uses a 24-slot, 28-pole configuration and has a speed constant of 180 +/-5% RPM/V. Recommended integration components include a 10–14S LiPo battery and a 2310 or 2409 propeller. Custom KV, appearance and color options are available for OEM/ODM projects.
Electrical integration must accommodate a maximum continuous current of 106 A and power of 4515.6 W at 42.6 V. The higher maximum rating of 120 A and 5112 W at the same voltage is limited to 15 seconds. Temperature at maximum continuous current is 88.5°C. The magnets have a maximum operating temperature of 150°C, with a recommended maximum of 120°C. Thrust performance depends on propeller selection, voltage and test conditions, so these operating variables remain material to propulsion selection.
Specifications
| Specification | Value & conditions |
|---|---|
| Product | YRDRONE LJ8020 KV180 brushless motor for fixed-wing drones |
| Application | Fixed-wing VTOL UAV propulsion |
| Motor diameter | 90 +/-0.1 mm |
| Motor length | 75.8 +/-0.3 mm |
| Slots and poles | 24N28P |
| Motor speed constant | 180 +/-5% RPM/V |
| No-load current | 4.6 A maximumAt 20 V. |
| Phase-to-phase resistance | 13 +/-8% mΩAt 25°C. |
| Maximum continuous current and power | 106 A / 4515.6 WAt 42.6 V. |
| Temperature | 88.5°CAt maximum continuous current. |
| Maximum current and power | 120 A / 5112 WAt 42.6 V; maximum 15 seconds. |
| Weight | 883 +/-15 g |
| Recommended LiPo cells | 10–14S |
| Recommended ESC | 14 seconds / 130 A |
| Recommended propellers | 2310 / 2409 |
| Maximum temperature | 150°C maximum; recommended maximum 120°CMagnet operating temperature. |
| Motor torque constant Kt | 666.55 g·cm/A |
| Motor constant Cn | 0.06 rpm/g·cm |
| Customization options | Custom KV, appearance and colorOEM/ODM projects. |
| Thrust dependence | Thrust performance varies with propeller, voltage and test conditions.Propeller, voltage and test conditions. |
