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YAHREE YU13819 KV39

By Yahree Aeropower Tech Co., Ltd. ↗

The YAHREE YU13819 KV39 is a multi-rotor UAV propulsion motor with a 36-slot, 42-pole architecture and a recommended 49-inch folding propeller. It supports recommended 14–24S battery integration and is rated for 12000 W continuous operation at 100 V, with an 18000 W peak limited to 15 seconds.

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Product identity and purposeYAHREE YU13819 KV39 multi-rotor motor
Motor diameter147.5 ± 0.1 mm
Motor length50 ± 0.3 mm
Slots and poles36N42P
Motor speed constant39 rpm/V ± 5%
No-load current2.5 A maximumAt 20 V.

Product overview

The YAHREE YU13819 KV39 is a propulsion motor for multi-rotor UAV integration. Its 36-slot, 42-pole architecture has a diameter of 147.5 ± 0.1 mm, a length of 50 ± 0.3 mm and a weight of 1795 ± 18 g. The KV39 version has a speed constant of 39 rpm/V ± 5%. Recommended integration equipment comprises a 14–24S LiPo battery, a 14–24S / 200 A ESC and a 49-inch folding propeller. These are equipment recommendations rather than a specified package of included accessories.

Electrical sizing distinguishes continuous operation from short peak demand: the motor is rated at 120 A / 12000 W continuously at 100 V, with 180 A / 18000 W allowed for a maximum of 15 seconds. Temperature at maximum continuous current is 93°C. The magnets have a maximum operating temperature of 180°C, with 150°C recommended as the upper limit. With the 49-inch folding propeller, full-throttle thrust is 47012 g at 99.81 V and 84.5 A. Thrust depends on propeller, voltage and test conditions; OEM/ODM projects can specify custom KV, appearance and color.

Specifications

SpecificationValue & conditions
Product identity and purposeYAHREE YU13819 KV39 multi-rotor motor
Motor diameter147.5 ± 0.1 mm
Motor length50 ± 0.3 mm
Slots and poles36N42P
Motor speed constant39 rpm/V ± 5%
No-load current2.5 A maximumAt 20 V.
Phase-to-phase resistance36 mΩ ± 8%At 25°C.
Maximum continuous current and power120 A / 12000 WAt 100 V.
Motor temperature93°CAt maximum continuous current.
Maximum current and power180 A / 18000 WAt 100 V; 15 seconds maximum.
Motor weight1795 ± 18 g
Recommended LiPo battery14–24S
Recommended ESC14–24S / 200 A
Recommended propeller49-inch folding propeller
Maximum magnet operating temperature180°CRecommended maximum: 150°C.
Torque constantKt: 2639.9 g·cm/A
Motor constantCn: 0.01 rpm/g·cm
Performance at 30% throttle
  • Voltage: 100.58 V;
  • thrust: 6890 g;
  • current: 5.6 A;
  • power: 565.2596 W;
  • reported efficiency: 12.19
YU13819 with a 49-inch folding propeller; 30% throttle.
Performance at 40% throttle
  • Voltage: 100.49 V;
  • thrust: 12286 g;
  • current: 12.0 A;
  • power: 1207.8898 W;
  • reported efficiency: 10.17
YU13819 with a 49-inch folding propeller; 40% throttle.
Performance at 50% throttle
  • Voltage: 100.36 V;
  • thrust: 20564 g;
  • current: 24.6 A;
  • power: 2470.8632 W;
  • reported efficiency: 8.32
YU13819 with a 49-inch folding propeller; 50% throttle.
Performance at 60% throttle
  • Voltage: 100.23 V;
  • thrust: 26290 g;
  • current: 35.4 A;
  • power: 3543.1305 W;
  • reported efficiency: 7.42
YU13819 with a 49-inch folding propeller; 60% throttle.
Performance at 70% throttle
  • Voltage: 100.09 V;
  • thrust: 33490 g;
  • current: 50.1 A;
  • power: 5011.5063 W;
  • reported efficiency: 6.68
YU13819 with a 49-inch folding propeller; 70% throttle.
Performance at 80% throttle
  • Voltage: 99.88 V;
  • thrust: 42874 g;
  • current: 73.2 A;
  • power: 7308.2196 W;
  • reported efficiency: 5.87
YU13819 with a 49-inch folding propeller; 80% throttle.
Performance at 90% throttle
  • Voltage: 99.8 V;
  • thrust: 46953 g;
  • current: 84.5 A;
  • power: 8433.1 W;
  • reported efficiency: 5.57
YU13819 with a 49-inch folding propeller; 90% throttle.
Performance at 100% throttle
  • Voltage: 99.81 V;
  • thrust: 47012 g;
  • current: 84.5 A;
  • power: 8437.9374 W;
  • reported efficiency: 5.57
YU13819 with a 49-inch folding propeller; 100% throttle.
Customization optionsCustom KV, appearance and colorOEM/ODM projects.
Thrust performance dependencyThrust varies with propeller, voltage and test conditions.Propeller, voltage and test conditions.

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