XRotor X13-13825

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X13

Brand new thrust system for heavy-duty drones,
especially applicable for agricultural UAV drones.

Buy

Highly efficient system with
extremely fast response speeds

High torque. High efficiency. Fast response.

Series Motor
ESC
Propeller

The Digital Age

The comprehensive introduction of CAN communication
brings a closed loop between the flight controller and the thrust
systems. All data is exchanged on "CAN bus".

lmplement real-time data transmission between the
flight controller and ESC/Motor.

Digital Throttle
Dual throttle control,
redundant backup precise
control without interference.
Data Transmission
Easy to query flight status
and the thrust system data.
Remote Upgrade
Link the ESC with the flight controller to
realize OTA cloud upgrade. From then on,
you can enjoy the latest Hobbywing
technology anytime and anywhere.

* Hobbywing CAN protocol has successfully communicated with some flight controller.
For the closed source flight controller, contact the manufacturer for instructions.
For the open source Ardupilot flight controller, refer
https://ardupilot.org/copter/docs/common-hobbywing-dronecan-esc.html

4-Rotors-50L

X13 18S Performance Platform

Maximum thrust 57kg/rotor(sea level)
Rated thrust 27kg/rotor(sea level)
Efficiency up to 8.0g/W

X13-18S

7.2 minutes flight time 18S-30000mAh battery
4-Rotors 108kg take off weight

Appearance 2.0 design

Industrial, innovative layout providing
a very clean aesthetic.

Quick disassembly design
ESC and motor disassembly only takes 1 minute:

High reliability waterproof connector
Easy to install and maintain

ln the event of an external or internal
failure, Smart Protection automatically
restarts. This will reduce the likely
hood of an accident and allow safer flying
Built-in fault storage function, saving
fault information for easy analysis of causes.

Hundreds of tests, stable performance

In response to the rigorous and complex agricultural application operating
environment, a variety of test projects and working conditions
are set up to ensure flight safety.

High and low temperature test

Water-proof test

Hours laboratory aging test

Hours flight test

XRotor X13 CAD

Product Name

XRotor X13-14S

XRotor X13-18S

Specifications

Max Thrust	57kg（54V,sea level）	57kg（70V,sea level）
Thrust/rotor	25-27kg/rotor	25-27kg/rotor
Recommended Battery	12-14S( LiPo)	18S( LiPo)
Operating Temperature	-20~50℃	-20~50℃
Total Weight	4257g(Inc prop)	4087g(Inc prop)
Ingress Protection	IPX6	IPX6

Motor

KV Rating	60rpm/V	45rpm/V
Stator Size	138*25mm	138*25mm
Powertrain Arm Tube Outer Diameter	50mm	50mm
Bearing	Waterproof	Waterproof

ESC

Recommended LiPo Battery	12-14S(LiPo)	18S(LiPo)
PWM Input Signal Level	3.3V/5V	3.3V/5V
Throttle Signal Frequency	50-500Hz	50-500Hz
Operating Pulse Width	1050-1950us	1050-1950us
Max. Input Voltage	65V	81V
Max. Input Current (Short duration)	200A（Non-hermetic Ambient Temperature ≤60℃）	200A（Non-hermetic Ambient Temperature ≤60℃）
BEC	No	No

Propeller

Diameter×Pitch

56*20"

XRotor X13-18S Load performance parameters

XRotor X13-18S Technical Parameters

Voltage(V)	Propeller(Inch)	Throttle(%)	Thrust(g)	Current(A)	Power(W)	RPM(r/min)	Efficiency(g/W)	Torque(N-m)	Temperature(℃)
70	56*20"	32%	9254	10.5	721.7	991	12.8	6.11	90
		33%	9514	10.9	749.3	1004	12.7	6.28
		36%	11268	13.7	945.4	1091	11.9	7.40
		39%	13287	17.2	1190.0	1183	11.2	8.65
		42%	15487	21.4	1477.5	1275	10.5	9.99
		45%	17812	26.1	1802.7	1364	9.9	11.39
		48%	20221	31.3	2161.3	1450	9.4	12.82
		51%	22693	36.9	2550.9	1522	8.9	14.29
		54%	25218	43.0	2971.1	1611	8.5	15.79
		57%	27794	49.6	3423.3	1688	8.0	17.33
		60%	30426	56.6	3910.4	1762	7.8	18.91
		63%	33118	64.3	4436.6	1836	7.5	20.54
		66%	35874	72.5	5006.4	1908	7.2	22.22
		69%	38691	81.4	5623.4	1980	6.9	23.94
		72%	41557	91.1	6289.6	2050	6.6	25.69
		75%	44447	101.4	7002.5	2119	6.3	27.46
		78%	47319	112.3	7753.4	2186	6.1	29.22
		81%	50109	123.5	8524.6	2248	5.9	30.92
		84%	52731	134.5	9286.5	2305	5.7	32.52
		87%	55070	144.8	9995.8	2355	5.5	33.94
		90%	56981	153.4	10594.6	2396	5.4	35.10
		100%	57893	157.7	10886.6	2415	5.3	35.65

The above data are measured under the environment of room Temperature(℃) (25°C) and sea level altitude, changing the throttle input to adjust the thrust force.

XRotor X13-14S Load performance parameters

XRotor X13-14S Technical Parameters

Voltage(V)	Propeller(Inch)	Throttle(%)	Thrust(g)	Current(A)	Power(W)	RPM(r/min)	Efficiency(g/W)	Torque(N-m)	Temperature(℃)
54	56*20"	32%	9190	13.2	716.3	992	12.83	5.64	115
		33%	9456	13.8	745.1	1006	12.69	5.81
		36%	11189	17.4	941.2	1092	11.89	6.89
		39%	13104	21.7	1175.3	1181	11.15	8.07
		42%	15150	26.7	1445.2	1270	10.48	9.34
		45%	17295	32.3	1749.2	1357	9.89	10.66
		48%	19518	38.6	2086.1	1441	9.36	12.03
		51%	21811	45.4	2455.7	1522	8.88	13.44
		54%	24173	52.9	2858.5	1600	8.46	14.89
		57%	26609	61.0	3295.9	1675	8.07	16.38
		60%	29125	69.7	3769.9	1749	7.73	17.91
		63%	31726	79.2	4282.8	1821	7.41	19.48
		66%	34415	89.5	4836.6	1892	7.12	21.08
		69%	37186	100.5	5432.9	1962	6.84	22.72
		72%	40024	112.3	6072.3	2031	6.59	24.39
		75%	42902	124.9	6753.6	2099	6.35	26.06
		78%	45777	138.2	7472.6	2165	6.13	27.74
		81%	48588	152.0	8219.8	2228	5.91	29.39
		84%	51250	166.1	8976.8	2287	5.71	30.98
		87%	53657	179.6	9710.8	2340	5.53	32.47
		90%	55674	191.8	10368.9	2385	5.37	33.76
		100%	57398	202.9	10967.6	2423	5.23	34.9

The above data are measured under the environment of room Temperature(℃) (25°C) and sea level altitude, changing the throttle input to adjust the thrust force.

Support

Manuals & Documents

Disclaimer

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HOBBYWING shall not be liable for any direct, indirect, incidental, special or consequential damages, loss of profits or business interruption caused by the use or inability to use the services provided by the Website, even if HOBBYWING has been advised of the possibility of similar losses. The exclusions and limitations of the warranty liability of HOBBYWING shall be effective to the extent permitted by applicable law.

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X13-14S Manuals

X13-18S Manuals

HW-X13-14S 5620 Techenical Parameters

X13 .step

HW-X13-18S 5620 Techenical Parameters

X13 . dxf

Propeller's apater.Step

Propeller .dxf

X13 signal motot.setp

DATALINKV2

Name: DATALINKV2
Telemetry: USB, CAN, Serial
Voltage: 6-81V
Size: 57*40*13mm(without wires)
Weight: 27g

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XRotor X13-13825

Overview Specifications Support Accessories Detail Contact us Shop

Buy

XRotor X13 CAD

Product Name

XRotor X13-14S

XRotor X13-18S

Specifications

Max Thrust	57kg（54V,sea level）	57kg（70V,sea level）
Thrust/rotor	25-27kg/rotor	25-27kg/rotor
Recommended Battery	12-14S( LiPo)	18S( LiPo)
Operating Temperature	-20~50℃	-20~50℃
Total Weight	4257g(Inc prop)	4087g(Inc prop)
Ingress Protection	IPX6	IPX6

Motor

KV Rating	60rpm/V	45rpm/V
Stator Size	138*25mm	138*25mm
Powertrain Arm Tube Outer Diameter	50mm	50mm
Bearing	Waterproof	Waterproof

ESC

Recommended LiPo Battery	12-14S(LiPo)	18S(LiPo)
PWM Input Signal Level	3.3V/5V	3.3V/5V
Throttle Signal Frequency	50-500Hz	50-500Hz
Operating Pulse Width	1050-1950us	1050-1950us
Max. Input Voltage	65V	81V
Max. Input Current (Short duration)	200A（Non-hermetic Ambient Temperature ≤60℃）	200A（Non-hermetic Ambient Temperature ≤60℃）
BEC	No	No

Propeller

Diameter×Pitch

56*20"

XRotor X13-18S Load performance parameters

XRotor X13-18S Technical Parameters

Voltage(V)	Propeller(Inch)	Throttle(%)	Thrust(g)	Current(A)	Power(W)	RPM(r/min)	Efficiency(g/W)	Torque(N-m)	Temperature(℃)
70	56*20"	32%	9254	10.5	721.7	991	12.8	6.11	90
		33%	9514	10.9	749.3	1004	12.7	6.28
		36%	11268	13.7	945.4	1091	11.9	7.40
		39%	13287	17.2	1190.0	1183	11.2	8.65
		42%	15487	21.4	1477.5	1275	10.5	9.99
		45%	17812	26.1	1802.7	1364	9.9	11.39
		48%	20221	31.3	2161.3	1450	9.4	12.82
		51%	22693	36.9	2550.9	1522	8.9	14.29
		54%	25218	43.0	2971.1	1611	8.5	15.79
		57%	27794	49.6	3423.3	1688	8.0	17.33
		60%	30426	56.6	3910.4	1762	7.8	18.91
		63%	33118	64.3	4436.6	1836	7.5	20.54
		66%	35874	72.5	5006.4	1908	7.2	22.22
		69%	38691	81.4	5623.4	1980	6.9	23.94
		72%	41557	91.1	6289.6	2050	6.6	25.69
		75%	44447	101.4	7002.5	2119	6.3	27.46
		78%	47319	112.3	7753.4	2186	6.1	29.22
		81%	50109	123.5	8524.6	2248	5.9	30.92
		84%	52731	134.5	9286.5	2305	5.7	32.52
		87%	55070	144.8	9995.8	2355	5.5	33.94
		90%	56981	153.4	10594.6	2396	5.4	35.10
		100%	57893	157.7	10886.6	2415	5.3	35.65

The above data are measured under the environment of room Temperature(℃) (25°C) and sea level altitude, changing the throttle input to adjust the thrust force.

XRotor X13-14S Load performance parameters

XRotor X13-14S Technical Parameters

Voltage(V)	Propeller(Inch)	Throttle(%)	Thrust(g)	Current(A)	Power(W)	RPM(r/min)	Efficiency(g/W)	Torque(N-m)	Temperature(℃)
54	56*20"	32%	9190	13.2	716.3	992	12.83	5.64	115
		33%	9456	13.8	745.1	1006	12.69	5.81
		36%	11189	17.4	941.2	1092	11.89	6.89
		39%	13104	21.7	1175.3	1181	11.15	8.07
		42%	15150	26.7	1445.2	1270	10.48	9.34
		45%	17295	32.3	1749.2	1357	9.89	10.66
		48%	19518	38.6	2086.1	1441	9.36	12.03
		51%	21811	45.4	2455.7	1522	8.88	13.44
		54%	24173	52.9	2858.5	1600	8.46	14.89
		57%	26609	61.0	3295.9	1675	8.07	16.38
		60%	29125	69.7	3769.9	1749	7.73	17.91
		63%	31726	79.2	4282.8	1821	7.41	19.48
		66%	34415	89.5	4836.6	1892	7.12	21.08
		69%	37186	100.5	5432.9	1962	6.84	22.72
		72%	40024	112.3	6072.3	2031	6.59	24.39
		75%	42902	124.9	6753.6	2099	6.35	26.06
		78%	45777	138.2	7472.6	2165	6.13	27.74
		81%	48588	152.0	8219.8	2228	5.91	29.39
		84%	51250	166.1	8976.8	2287	5.71	30.98
		87%	53657	179.6	9710.8	2340	5.53	32.47
		90%	55674	191.8	10368.9	2385	5.37	33.76
		100%	57398	202.9	10967.6	2423	5.23	34.9

The above data are measured under the environment of room Temperature(℃) (25°C) and sea level altitude, changing the throttle input to adjust the thrust force.

Support

Manuals & Documents

Disclaimer

HOBBYWING shall not be liable for any direct or indirect damage or loss caused by any third party using illegal means to access the website to obtain the relevant passwords, information and content.

HOBBYWING reserves the right to correct, modify and update this statement at any time.

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