Hobbywing XRotor X13 brushless power system is a robust plant protection system designed for 25-27kg/rotor single-rotor loads, with more than 53kg of maximum thrust. It is suitable for 50mm carbon fiber tube arms and is IPX6 waterproof, capable of withstanding rain pesticieds, salt spray, high temperatures, sand/dust, impacts, and mud/sand. Featuring FOC vector control and PMSM-based algorithm optimization, the system combines digital and analog throttle for increased flight stability, plus power-on auto-detection and safety functions such as voltage abnormality protection, over-current protection, stall protection, and others; all data is transmitted via CAN, and faults are logged for better analysis.
The whole power system has been assembled before leaves the factory. Unpack and take out the power kit to install on the rack of plant-protection plane as per the rotation direction of motor.
| Product Name |
|
XRotor X13-14S |
XRotor X13-18S |
| Specifications |
Max Thrust
Recommended Takeoff Weight
Recommended Battery
Operating Temperature
Total Weight
Ingress Protection |
57kg
25-27kg/rotor
12-14S( LiPo)
-20~50℃
4257g(Inc prop)
IPX6 |
57kg
25-27kg/rotor
18S( LiPo)
-20~50℃
4087g(Inc prop)
IPX6 |
| Motor |
KV Rating
Stator Size
Powertrain Arm Tube Outer Diameter
Bearing |
60rpm/V
138*25mm
50mm
Waterproof |
45rpm/V
138*25mm
50mm
Waterproof |
| ESC |
Recommended LiPo Battery
PWM Input Signal Level
Throttle Signal Frequency
Operating Pulse Width
Max. Input Voltage
Max. Input Current (Short duration)
BEC |
12-14S(LiPo)
3.3V/5V
50-500Hz
1050-1950us
65V
200A（Non-hermetic Ambient
Temperature ≤60℃）
No |
18S(LiPo)
3.3V/5V
50-500Hz
1050-1950us
81V
200A（Non-hermetic Ambient
Temperature ≤60℃）
No |
| Propeller |
Diameter×Pitch |
56*20" |
56*20" |
HW-X13-18S Graph:
X13-18S Techenical 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.
