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Cobra
C-2217/7 Motor Propeller Data |
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Magnets |
Motor Wind |
Motor Kv |
No-Load Current |
Motor Resistance |
I Max |
P Max (4S) |
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14-Pole |
7-Turn Delta |
2500 RPM/Volt |
Io = 2.73 Amps @ 10v |
Rm = 0.020 Ohms |
50 Amps |
740 W |
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Stator |
Outside Diameter |
Body Length |
Total Shaft Length |
Shaft Diameter |
Motor Weight |
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12-Slot |
27.8 mm, 1.094 in. |
32.0 mm, 1.259 in. |
47.0 mm, 1.850 in. |
3.17 mm, 0.125 in. |
74.0 gm, 2.61 oz |
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Test
Data From |
Input |
6.0 V |
8.0 V |
10.0V |
12.0V |
Measured Kv value |
Measured Rm Value |
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Sample
Motor |
Io Value |
1.956 A |
2.252 A |
2.726 A |
2.862 A |
2563 RPM/Volt @ 10v |
0.0198 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 |
4.75x4.25 |
3 |
11.1 |
24.12 |
267.8 |
25,359 |
102.1 |
566 |
19.96 |
2.11 |
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APC |
4.75x4.75 |
3 |
11.1 |
26.98 |
299.5 |
25,022 |
112.6 |
562 |
19.82 |
1.88 |
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APC |
4.75x5.5-E |
3 |
11.1 |
29.93 |
332.2 |
24,635 |
128.3 |
526 |
18.55 |
1.58 |
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APC |
5x4.3-MR |
3 |
11.1 |
34.19 |
379.5 |
24,170 |
98.4 |
983 |
34.67 |
2.59 |
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APC |
5x4.5-MR |
3 |
11.1 |
34.97 |
388.1 |
24,021 |
102.4 |
967 |
34.11 |
2.49 |
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APC |
5x4.6-MR |
3 |
11.1 |
35.46 |
393.6 |
23,969 |
104.4 |
1031 |
36.37 |
2.62 |
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APC |
5x5-E |
3 |
11.1 |
30.89 |
342.9 |
24,461 |
115.8 |
599 |
21.13 |
1.75 |
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APC |
5.25x4.75-E |
3 |
11.1 |
35.01 |
388.6 |
23,918 |
107.6 |
804 |
28.36 |
2.07 |
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APC |
5.5x4.5-E |
3 |
11.1 |
35.59 |
395.1 |
23,820 |
101.5 |
856 |
30.19 |
2.17 |
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APC |
6x4-E |
3 |
11.1 |
40.33 |
447.6 |
23,344 |
88.4 |
1134 |
40.00 |
2.53 |
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APC |
6x4.3-MR |
3 |
11.1 |
50.15 |
556.7 |
21,685 |
88.3 |
1499 |
52.87 |
2.69 |
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APC |
6x4.5-MR |
3 |
11.1 |
47.96 |
532.3 |
21,991 |
93.7 |
1504 |
53.05 |
2.83 |
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APC |
6x5.5-E |
3 |
11.1 |
48.38 |
537.0 |
21,903 |
114.1 |
1067 |
37.64 |
1.99 |
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HQ |
4x4.5-BN |
3 |
11.1 |
20.89 |
231.9 |
25,822 |
110.0 |
614 |
21.66 |
2.65 |
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HQ |
5x4 |
3 |
11.1 |
20.29 |
225.3 |
25,925 |
98.2 |
768 |
27.09 |
3.41 |
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HQ |
5x4.5 |
3 |
11.1 |
21.61 |
239.8 |
25,714 |
109.6 |
773 |
27.27 |
3.22 |
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HQ |
5x4.5-BN |
3 |
11.1 |
34.18 |
379.4 |
24,167 |
103.0 |
1053 |
37.14 |
2.78 |
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HQ |
6x3 |
3 |
11.1 |
20.68 |
229.6 |
25,900 |
73.6 |
869 |
30.65 |
3.78 |
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HQ |
6x4.5 |
3 |
11.1 |
41.04 |
455.5 |
23,313 |
99.3 |
1410 |
49.74 |
3.10 |
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HQ |
6x4.5-BN |
3 |
11.1 |
52.69 |
584.8 |
21,377 |
91.1 |
1536 |
54.18 |
2.63 |
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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 |
4x4.5-MR |
4 |
14.8 |
31.21 |
461.9 |
32,783 |
139.7 |
850 |
29.98 |
1.84 |
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APC |
4.1x4.1-E |
4 |
14.8 |
24.16 |
357.5 |
33,728 |
131.0 |
623 |
21.98 |
1.74 |
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APC |
4.5x4.1-E |
4 |
14.8 |
31.25 |
462.5 |
32,705 |
127.0 |
866 |
30.55 |
1.87 |
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APC |
4.75x4.25 |
4 |
14.8 |
37.91 |
561.1 |
31,882 |
128.3 |
897 |
31.64 |
1.60 |
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APC |
4.75x4.75 |
4 |
14.8 |
42.14 |
623.7 |
31,320 |
140.9 |
886 |
31.25 |
1.42 |
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APC |
4.75x5.5-E |
4 |
14.8 |
45.68 |
676.0 |
30,850 |
160.7 |
823 |
29.03 |
1.22 |
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APC |
5x4.3-MR |
4 |
14.8 |
54.18 |
801.9 |
29,818 |
121.4 |
1505 |
53.09 |
1.88 |
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APC |
5x5-E |
4 |
14.8 |
47.66 |
705.4 |
30,538 |
144.6 |
917 |
32.35 |
1.30 |
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APC |
5.25x4.75-E |
4 |
14.8 |
55.34 |
819.1 |
29,571 |
133.0 |
1233 |
43.49 |
1.51 |
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HQ |
4x4.5-BN |
4 |
14.8 |
31.13 |
460.7 |
32,817 |
139.8 |
989 |
34.89 |
2.15 |
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HQ |
5x4 |
4 |
14.8 |
31.11 |
460.5 |
32,850 |
124.4 |
1250 |
44.09 |
2.71 |
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HQ |
5x4.5 |
4 |
14.8 |
33.76 |
499.6 |
32,447 |
138.3 |
1230 |
43.39 |
2.46 |
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HQ |
5x4.5-BN |
4 |
14.8 |
51.38 |
760.5 |
30,212 |
128.7 |
1640 |
57.85 |
2.16 |
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HQ |
6x3 |
4 |
14.8 |
32.99 |
488.3 |
32,624 |
92.7 |
1449 |
51.11 |
2.97 |
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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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