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Cobra
C-5340-16 200Kv Motor Propeller Data |
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Magnets |
Motor Wind |
Motor Kv |
No-Load Current |
Motor Resistance |
I Max |
P Max (12S) |
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14-Pole |
16-Turn Delta |
200 RPM/Volt |
Io = 3.05 Amps @ 40v |
Rm = 0.025 Ohms |
64 Amps |
2840 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. |
71.0 mm, 2.80 in. |
102.4 mm, 4.03 in. |
8.00 mm, 0.315 in. |
804 grams, 28.36 oz. |
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Test
Data From |
Input |
28.0 V |
32.0 V |
36.0V |
40.0V |
Measured Kv value |
Measured Rm Value |
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Sample
Motor |
Io Value |
2.44 A |
2.62 A |
2.99 A |
3.05 A |
205 RPM/Volt @ 40V |
0.025 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 |
16x8-E |
10 |
37.0 |
30.49 |
1128.2 |
7,083 |
53.7 |
4,573 |
161.31 |
4.05 |
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APC |
16x10-E |
10 |
37.0 |
34.46 |
1275.2 |
7,009 |
66.4 |
4,631 |
163.35 |
3.63 |
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APC |
16x12-E |
10 |
37.0 |
40.98 |
1516.1 |
6,880 |
78.2 |
4,294 |
151.46 |
2.83 |
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APC |
17x8-E |
10 |
37.0 |
33.28 |
1231.3 |
7,046 |
53.4 |
5,355 |
188.89 |
4.35 |
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APC |
17x10-E |
10 |
37.0 |
40.40 |
1494.7 |
6,926 |
65.6 |
5,673 |
200.11 |
3.80 |
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APC |
17x12-E |
10 |
37.0 |
46.20 |
1709.5 |
6,826 |
77.6 |
5,640 |
198.94 |
3.30 |
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APC |
18x8-E |
10 |
37.0 |
32.58 |
1205.3 |
6,932 |
52.5 |
6,151 |
216.97 |
5.10 |
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APC |
18x10-E |
10 |
37.0 |
38.66 |
1430.6 |
6,780 |
64.2 |
6,357 |
224.23 |
4.44 |
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APC |
18x12-E |
10 |
37.0 |
58.18 |
2152.5 |
6,631 |
75.4 |
6,714 |
236.83 |
3.12 |
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APC |
19x8-E |
10 |
37.0 |
47.15 |
1744.7 |
6,666 |
50.5 |
7,373 |
260.07 |
4.23 |
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APC |
19x10-E |
10 |
37.0 |
47.12 |
1743.6 |
6,807 |
64.5 |
7,757 |
273.62 |
4.45 |
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APC |
19x12-E |
10 |
37.0 |
55.32 |
2046.7 |
6,545 |
74.4 |
7,852 |
276.97 |
3.84 |
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APC |
20x8-E |
10 |
37.0 |
50.82 |
1880.3 |
6,754 |
51.2 |
8,682 |
306.25 |
4.62 |
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APC |
20x10-E |
10 |
37.0 |
59.91 |
2216.7 |
6,596 |
62.5 |
9,063 |
319.68 |
4.09 |
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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 |
15x8-E |
12 |
44.4 |
26.63 |
1182.3 |
8,621 |
65.3 |
4,580 |
161.55 |
3.87 |
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APC |
15x10-E |
12 |
44.4 |
41.43 |
1839.3 |
8,309 |
78.7 |
5,090 |
179.54 |
2.77 |
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APC |
16x8-E |
12 |
44.4 |
46.40 |
2060.3 |
8,232 |
62.4 |
6,167 |
217.53 |
2.99 |
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APC |
16x10-E |
12 |
44.4 |
50.27 |
2232.0 |
8,126 |
77.0 |
6,222 |
219.47 |
2.79 |
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APC |
16x12-E |
12 |
44.4 |
56.24 |
2497.2 |
7,999 |
90.9 |
5,788 |
204.16 |
2.32 |
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APC |
17x8-E |
12 |
44.4 |
48.07 |
2134.2 |
8,192 |
62.1 |
7,046 |
248.54 |
3.30 |
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APC |
17x10-E |
12 |
44.4 |
54.21 |
2406.7 |
7,902 |
74.8 |
7,365 |
259.79 |
3.06 |
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APC |
17x12-E |
12 |
44.4 |
64.39 |
2858.8 |
7,888 |
89.6 |
7,467 |
263.39 |
2.61 |
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APC |
18x8-E |
12 |
44.4 |
47.23 |
2096.9 |
8,209 |
62.2 |
8,785 |
309.88 |
4.19 |
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APC |
18x10-E |
12 |
44.4 |
57.52 |
2553.7 |
8,007 |
75.8 |
8,658 |
305.40 |
3.39 |
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APC |
19x8-E |
12 |
44.4 |
71.48 |
3173.6 |
7,747 |
58.7 |
9,951 |
351.01 |
3.14 |
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APC |
19x10-E |
12 |
44.4 |
66.78 |
2965.0 |
7,842 |
74.3 |
10,196 |
359.65 |
3.44 |
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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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512 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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