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Cobra
C-5330-22 205Kv 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 |
22-Turn Delta |
205 RPM/Volt |
Io = 1.55 Amps @ 20v |
Rm = 0.034 Ohms |
55 Amps |
2440 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. |
60.5 mm, 2.38 in. |
94.3 mm, 3.71 in. |
8.00 mm, 0.315 in. |
649 grams, 22.89 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 |
1.422 A |
1.545 A |
1.682 A |
1.811 A |
212.5 RPM/Volt @ 20V |
0.0337 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 |
15x10-E |
10 |
37.0 |
26.23 |
970.6 |
7,034 |
66.6 |
3,668 |
129.38 |
3.78 |
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APC |
16x8-E |
10 |
37.0 |
27.38 |
1013.1 |
6,871 |
52.1 |
4,259 |
150.23 |
4.20 |
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APC |
16x10-E |
10 |
37.0 |
31.59 |
1168.9 |
6,900 |
65.3 |
4,444 |
156.76 |
3.80 |
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APC |
16x12-E |
10 |
37.0 |
37.65 |
1393.2 |
6,784 |
77.1 |
4,088 |
144.20 |
2.93 |
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APC |
17x8-E |
10 |
37.0 |
30.98 |
1146.2 |
6,916 |
52.4 |
5,008 |
176.65 |
4.37 |
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APC |
17x10-E |
10 |
37.0 |
37.51 |
1387.8 |
6,783 |
64.2 |
5,275 |
186.07 |
3.80 |
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APC |
17x12-E |
10 |
37.0 |
42.09 |
1557.5 |
6,692 |
76.0 |
5,193 |
183.18 |
3.33 |
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APC |
18x8-E |
10 |
37.0 |
30.82 |
1140.3 |
6,913 |
52.4 |
5,892 |
207.83 |
5.17 |
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APC |
18x10-E |
10 |
37.0 |
37.77 |
1397.3 |
6,773 |
64.1 |
6,140 |
216.58 |
4.39 |
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APC |
18x12-E |
10 |
37.0 |
54.07 |
2000.6 |
6,481 |
73.6 |
6,099 |
215.13 |
3.05 |
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APC |
19x8-E |
10 |
37.0 |
46.34 |
1714.5 |
6,617 |
50.1 |
7,142 |
251.92 |
4.17 |
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APC |
19x10-E |
10 |
37.0 |
43.99 |
1627.5 |
6,658 |
63.0 |
7,238 |
255.31 |
4.45 |
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APC |
19x12-E |
10 |
37.0 |
52.48 |
1941.8 |
6,500 |
73.9 |
7,482 |
263.92 |
3.85 |
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APC |
20x8-E |
10 |
37.0 |
46.52 |
1721.2 |
6,600 |
50.0 |
7,943 |
280.18 |
4.61 |
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APC |
20x10-E |
10 |
37.0 |
55.48 |
2052.8 |
6,441 |
61.0 |
8,438 |
297.64 |
4.11 |
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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 |
23.15 |
1027.9 |
8,329 |
63.1 |
4,266 |
150.48 |
4.15 |
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APC |
15x10-E |
12 |
44.4 |
38.34 |
1702.4 |
8,133 |
77.0 |
4,904 |
172.98 |
2.88 |
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APC |
16x8-E |
12 |
44.4 |
42.46 |
1885.4 |
8,045 |
60.9 |
5,870 |
207.06 |
3.11 |
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APC |
16x10-E |
12 |
44.4 |
46.08 |
2046.1 |
7,961 |
75.4 |
5,929 |
209.14 |
2.90 |
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APC |
16x12-E |
12 |
44.4 |
51.59 |
2290.7 |
7,836 |
89.0 |
5,458 |
192.52 |
2.38 |
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APC |
17x8-E |
12 |
44.4 |
44.15 |
1960.0 |
8,000 |
60.6 |
6,628 |
233.79 |
3.38 |
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APC |
17x10-E |
12 |
44.4 |
53.26 |
2364.5 |
7,800 |
73.9 |
7,065 |
249.21 |
2.99 |
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APC |
17x12-E |
12 |
44.4 |
59.07 |
2622.8 |
7,694 |
87.4 |
6,877 |
242.58 |
2.62 |
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APC |
18x8-E |
12 |
44.4 |
43.00 |
1909.0 |
8,029 |
60.8 |
8,059 |
284.27 |
4.22 |
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APC |
18x10-E |
12 |
44.4 |
50.05 |
2222.2 |
7,722 |
73.1 |
8,032 |
283.32 |
3.61 |
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APC |
19x8-E |
12 |
44.4 |
65.51 |
2908.6 |
7,571 |
57.4 |
9,164 |
323.25 |
3.15 |
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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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