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Cobra
C-5320-18 370Kv Motor Propeller Data |
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Magnets |
Motor Wind |
Motor Kv |
No-Load Current |
Motor Resistance |
I Max |
P Max (8S) |
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14-Pole |
18-Turn Delta |
370 RPM/Volt |
Io = 2.50 Amps @ 20v |
Rm = 0.023 Ohms |
75 Amps |
2220 W |
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Stator |
Outside Diameter |
Body Length |
Total Shaft Length |
Shaft Diameter |
Motor Weight |
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12-Slot |
63.0 mm,
2.48 in. |
50.5 mm, 1.99 in. |
84.3 mm, 3.32 in. |
8.00 mm, 0.315 in. |
490 grams, 17.28 oz. |
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Test
Data From |
Input |
16.0 V |
20.0 V |
24.0V |
28.0V |
Measured Kv value |
Measured Rm Value |
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Sample
Motor |
Io Value |
2.157 A |
2.495 A |
2.883 A |
3.497 A |
369.6 RPM/Volt @ 20V |
0.0227 Ohms |
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Prop |
Prop |
Li-Po |
Input |
Motor |
Input |
Prop |
Pitch Speed |
Thrust |
Thrust |
Thrust Eff. |
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Manf. |
Size |
Cells |
Voltage |
Amps |
Watts |
RPM |
in MPH |
Grams |
Ounces |
Grams/W |
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APC |
15x6-E |
6 |
22.2 |
26.54 |
589.3 |
7,406 |
42.1 |
3,208 |
113.16 |
5.44 |
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APC |
15x8-E |
6 |
22.2 |
29.91 |
664.0 |
7,398 |
56.0 |
3,297 |
116.30 |
4.97 |
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APC |
15x10-E |
6 |
22.2 |
43.99 |
976.6 |
7,085 |
67.1 |
3,703 |
130.62 |
3.79 |
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APC |
16x8-E |
6 |
22.2 |
36.45 |
809.1 |
7,277 |
55.1 |
3,767 |
132.88 |
4.66 |
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APC |
16x10-E |
6 |
22.2 |
53.05 |
1177.7 |
6,905 |
65.4 |
4,403 |
155.31 |
3.74 |
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APC |
16x12-E |
6 |
22.2 |
62.97 |
1397.9 |
6,724 |
76.4 |
3,959 |
139.65 |
2.83 |
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APC |
17x8-E |
6 |
22.2 |
52.02 |
1154.8 |
6,950 |
52.7 |
4,907 |
173.09 |
4.25 |
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APC |
17x10-E |
6 |
22.2 |
62.14 |
1379.5 |
6,738 |
63.8 |
5,078 |
179.12 |
3.68 |
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APC |
17x12-E |
6 |
22.2 |
69.59 |
1544.8 |
6,580 |
74.8 |
4,956 |
174.82 |
3.21 |
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APC |
18x8-E |
6 |
22.2 |
52.62 |
1168.3 |
6,934 |
52.5 |
5,778 |
203.81 |
4.95 |
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APC |
18x10-E |
6 |
22.2 |
63.51 |
1409.9 |
6,687 |
63.3 |
6,038 |
212.98 |
4.28 |
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APC |
18x12-E |
6 |
22.2 |
87.31 |
1938.4 |
6,523 |
74.1 |
5,622 |
198.31 |
2.90 |
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APC |
19x8-E |
6 |
22.2 |
74.60 |
1656.1 |
6,527 |
49.4 |
6,766 |
238.66 |
4.09 |
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APC |
19x10-E |
6 |
22.2 |
72.43 |
1607.9 |
6,538 |
61.9 |
6,908 |
243.67 |
4.30 |
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APC |
19x12-E |
6 |
22.2 |
86.20 |
1913.6 |
6,515 |
74.0 |
7,017 |
247.51 |
3.67 |
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APC |
20x8-E |
6 |
22.2 |
76.45 |
1697.2 |
6,562 |
49.7 |
7,580 |
267.37 |
4.47 |
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Prop |
Prop |
Li-Po |
Input |
Motor |
Input |
Prop |
Pitch Speed |
Thrust |
Thrust |
Thrust Eff. |
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Manf. |
Size |
Cells |
Voltage |
Amps |
Watts |
RPM |
in MPH |
Grams |
Ounces |
Grams/W |
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APC |
15x6-E |
7 |
25.9 |
37.08 |
960.2 |
8,500 |
48.3 |
4,366 |
154.00 |
4.55 |
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APC |
15x8-E |
7 |
25.9 |
40.59 |
1051.4 |
8,413 |
63.7 |
4,304 |
151.82 |
4.09 |
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APC |
15x10-E |
7 |
25.9 |
60.84 |
1575.8 |
7,990 |
75.7 |
4,690 |
165.43 |
2.98 |
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APC |
16x8-E |
7 |
25.9 |
66.78 |
1729.7 |
7,889 |
59.8 |
5,489 |
193.62 |
3.17 |
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APC |
16x10-E |
7 |
25.9 |
73.47 |
1902.8 |
7,787 |
73.7 |
5,558 |
196.05 |
2.92 |
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APC |
16x12-E |
7 |
25.9 |
83.78 |
2169.9 |
7,686 |
87.3 |
5,012 |
176.79 |
2.31 |
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APC |
17x8-E |
7 |
25.9 |
70.75 |
1832.5 |
7,873 |
59.6 |
6,219 |
219.37 |
3.39 |
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APC |
17x10-E |
7 |
25.9 |
84.51 |
2188.9 |
7,633 |
72.3 |
6,436 |
227.02 |
2.94 |
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APC |
18x8-E |
7 |
25.9 |
69.42 |
1798.1 |
7,850 |
59.5 |
7,415 |
261.55 |
4.12 |
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APC |
18x10-E |
7 |
25.9 |
83.79 |
2170.1 |
7,650 |
72.4 |
7,749 |
273.34 |
3.57 |
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Prop |
Prop |
Li-Po |
Input |
Motor |
Input |
Prop |
Pitch Speed |
Thrust |
Thrust |
Thrust Eff. |
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Manf. |
Size |
Cells |
Voltage |
Amps |
Watts |
RPM |
in MPH |
Grams |
Ounces |
Grams/W |
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APC |
15x6-E |
8 |
29.6 |
49.72 |
1471.6 |
9,445 |
53.7 |
5,381 |
189.81 |
3.66 |
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APC |
15x8-E |
8 |
29.6 |
53.14 |
1572.9 |
9,384 |
71.1 |
5,307 |
187.20 |
3.37 |
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APC |
15x10-E |
8 |
29.6 |
81.15 |
2402.0 |
9,027 |
85.5 |
5,647 |
199.19 |
2.35 |
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Propeller Chart Color Code Explanation |
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The
prop is to small to get good performance from the motor. (Less than 50%
power) |
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The
prop is sized right to get good power from the motor. (50 to 80% power) |
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The
prop can be used, but full throttle should be kept to short bursts. (80 to
100% power) |
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The
prop is too big for the motor and should not be used. (Over 100% power) |
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PLEASE NOTE: |
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The Data contained in this Prop Chart is
based on actual measurements, taken in a controlled test environment, at an
altitude of |
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584 feet above sea level. The test voltages used are based on the
standard output of a Li-Po battery under load, which is 3.70 volts |
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per cell.
If you are using a battery that is larger in capacity than normal, or
has a very high C-rating, then your actual voltages will |
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be higher than those shown in the chart, and
this will result in a higher current and power value for every prop
used. You should |
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always test your actual power system with a
watt meter before flying your model to make sure that you are not exceeding
the |
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recommended current and power ratings of the
motor being used. The prop
recommendations in this chart assume that the motor |
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receives adequate cooling throughout its
operation. If your motor is being used
inside a cowl or fuselage, you must ensure that |
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the motor receives sufficient airflow, and
does not get too hot during operation.
It is always best to use a prop size that pulls no |
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more than 80% of the motors maximum
recommended current value to ensure safe operation under all conditions. |
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