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Cobra
CP2814-1450 Motor Propeller Data |
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Magnets |
Motor Wind |
Motor Kv |
No-Load Current |
Motor Resistance |
I Max |
P Max (5S) |
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14-Pole |
10-Turn Delta |
1450 RPM/Volt |
Io = 4.08 Amps @ 15v |
Rm = 0.016 Ohms |
55 Amps |
1020 W |
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Stator |
Outside Diameter |
Body Length |
Total Shaft Length |
Shaft Diameter |
Motor
Weight |
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12-Slot |
35.1 mm, 1.38 in. |
36.0 mm, 1.42 in. |
41.5 mm, 1.63 in. |
5.00 mm, 0.197 in. |
120
gm, 4.23 oz |
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Test
Data From |
Input |
12.0 V |
15.0 V |
18.0V |
21.0V |
Measured
Kv value |
Measured
Rm Value |
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Sample
Motor |
Io Value |
3.521 A |
4.082 A |
4.294 A |
4.630 A |
1580
RPM/Volt @ 15V |
0.0163
Ohms |
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Prop |
Prop |
Li-Po |
Input |
Motor |
Watts |
Prop |
Pitch |
Thrust |
Thrust |
Thrust Eff. |
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Manf. |
Size |
Cells |
Voltage |
Amps |
Input |
RPM |
Speed |
Grams |
Ounces |
Grams/W |
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APC |
7x4-E |
3 |
11.1 |
24.80 |
275.2 |
15,690 |
59.4 |
1077 |
37.99 |
3.91 |
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APC |
7x5-E |
3 |
11.1 |
31.10 |
345.2 |
15,316 |
72.5 |
1092 |
38.52 |
3.16 |
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APC |
7x6-E |
3 |
11.1 |
33.04 |
366.8 |
15,275 |
86.8 |
1173 |
41.38 |
3.20 |
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APC |
8x4-E |
3 |
11.1 |
38.09 |
422.8 |
15,004 |
56.8 |
1486 |
52.42 |
3.51 |
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APC |
8x6-E |
3 |
11.1 |
59.93 |
665.3 |
13,707 |
77.9 |
1654 |
58.34 |
2.49 |
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Prop |
Prop |
Li-Po |
Input |
Motor |
Watts |
Prop |
Pitch |
Thrust |
Thrust |
Thrust Eff. |
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Manf. |
Size |
Cells |
Voltage |
Amps |
Input |
RPM |
Speed |
Grams |
Ounces |
Grams/W |
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APC |
6x4-E |
4 |
14.8 |
23.19 |
343.3 |
21,327 |
80.8 |
967 |
34.11 |
2.82 |
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APC |
6x4.3-MR |
4 |
14.8 |
32.30 |
478.0 |
20,756 |
84.5 |
1407 |
49.63 |
2.94 |
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APC |
6x4.5-MR |
4 |
14.8 |
30.23 |
447.4 |
20,885 |
89.0 |
1390 |
49.03 |
3.11 |
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APC |
6x5.5-E |
4 |
14.8 |
28.88 |
427.4 |
20,973 |
109.2 |
1051 |
37.07 |
2.46 |
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APC |
6x6-E |
4 |
14.8 |
33.49 |
495.6 |
20,667 |
117.4 |
1073 |
37.85 |
2.17 |
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APC |
7x4-E |
4 |
14.8 |
44.04 |
651.7 |
19,932 |
75.5 |
1776 |
62.65 |
2.72 |
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APC |
7x5-E |
4 |
14.8 |
53.96 |
798.6 |
19,345 |
91.6 |
1766 |
62.29 |
2.21 |
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APC |
7x6-E |
4 |
14.8 |
56.67 |
838.7 |
19,260 |
109.4 |
1888 |
66.60 |
2.25 |
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Prop |
Prop |
Li-Po |
Input |
Motor |
Watts |
Prop |
Pitch |
Thrust |
Thrust |
Thrust Eff. |
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Manf. |
Size |
Cells |
Voltage |
Amps |
Input |
RPM |
Speed |
Grams |
Ounces |
Grams/W |
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APC |
6x4-E |
5 |
18.5 |
38.24 |
707.4 |
26,353 |
99.8 |
1478 |
52.13 |
2.09 |
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APC |
6x4.3-MR |
5 |
18.5 |
52.19 |
965.5 |
25,513 |
103.9 |
2153 |
75.94 |
2.23 |
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APC |
6x4.5-MR |
5 |
18.5 |
47.42 |
877.3 |
25,837 |
110.1 |
2145 |
75.66 |
2.44 |
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APC |
6x5.5-E |
5 |
18.5 |
46.54 |
861.0 |
25,858 |
134.7 |
1568 |
55.31 |
1.82 |
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APC |
6x6-E |
5 |
18.5 |
52.55 |
972.1 |
25,418 |
144.4 |
1579 |
55.70 |
1.62 |
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© 2018 Innov8tive Designs,
Inc. |
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This
chart, and the data contained within it, are the property of Innov8tive
Designs, Inc., and may not be reproduced without permission from the
author. |
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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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