Product overview
The YRDRONE YU13815 is a Standard Series motor for multi-rotor UAV propulsion. Its 100 KV configuration uses a 36-slot, 42-pole arrangement within a body measuring 147.5+/-0.1 mm in diameter and 55+/-0.3 mm long. The motor weighs 1640+/-18 g, establishing its mass and dimensional requirements for propulsion integration. Recommended companion components are a 14-24S LiPo battery, a 14-24S / 200 A ESC and a 40*13.1 propeller. Custom KV, appearance and color options are available for OEM/ODM projects.
At 50 V, maximum continuous current and power are 145 A and 7250 W; the higher limits of 195 A and 9750 W apply for 15 seconds maximum. Temperature at maximum continuous current is 92 degrees Celsius. The magnet's maximum operating temperature is 180 degrees Celsius, with a recommended maximum of 150 degrees Celsius. With the 40*13.1 propeller, performance data cover 10–100% throttle and thrust of 627–37794 g at the respective measured voltages. Thrust varies with propeller, voltage and test conditions.
Specifications
| Specification | Value & conditions |
|---|---|
| Manufacturer and model | YRDRONE YU13815 multi-rotor UAV motor |
| Motor diameter | 147.5+/-0.1 mm100 KV version. |
| Motor length | 55+/-0.3 mm100 KV version. |
| Slots and poles | 36N42P100 KV version. |
| Motor KV | 100+/-5% RPM/V100 KV version. |
| Free-load current | 7.2 A maximumAt 20 V; 100 KV version. |
| Phase-to-phase resistance | 10+/-8% mΩAt 25 degrees Celsius; 100 KV version. |
| Maximum continuous current and power | 145 A / 7250 WAt 50 V; 100 KV version. |
| Temperature at maximum continuous current | 92 degrees CelsiusAt maximum continuous current; 100 KV version. |
| Maximum current and power | 195 A / 9750 WAt 50 V, for 15 seconds maximum; 100 KV version. |
| Motor weight | 1640+/-18 g100 KV version. |
| Recommended LiPo cells | 14-24S100 KV version. |
| Recommended ESC | 14-24S / 200 A100 KV version. |
| Recommended propeller | 40*13.1100 KV version. |
| Magnet operating temperature | Maximum 180 degrees Celsius; recommended maximum 150 degrees Celsius100 KV version. |
| Motor torque constant | Kt: 1254.6 g.cm/A100 KV version. |
| Motor constant | Cn: 0.02 rpm/g.cm100 KV version. |
| Customization options | Custom KV, appearance and colorOEM/ODM projects. |
| Performance at 10% throttle |
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| Performance at 20% throttle |
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| Performance at 30% throttle |
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| Performance at 40% throttle |
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| Performance at 50% throttle |
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| Performance at 60% throttle |
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| Performance at 70% throttle |
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| Performance at 80% throttle |
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| Performance at 90% throttle |
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| Performance at 100% throttle |
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| Thrust performance dependence | Thrust varies with propeller, voltage and test conditionsPropeller, voltage and test conditions affect thrust performance. |


