|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
BadAss
BA-2814-1560 Motor Propeller Data |
|
|
|
|
|
Magnets |
Motor Wind |
Motor Kv |
No-Load Current |
Motor Resistance |
I Max |
P Max (6S) |
|
|
|
|
|
14-Pole |
10-Turn Delta |
1560 RPM/Volt |
Io = 2.93 Amps @ 10v |
Rm = 0.020 Ohms |
65 Amps |
1440 W |
|
|
|
|
|
|
|
|
|
|
|
Stator |
Outside Diameter |
Body Length |
Total Shaft Length |
Shaft Diameter |
Motor
Weight |
|
|
|
|
|
12-Slot |
35.6 mm, 1.402 in. |
34.0 mm, 1.339 in. |
55.5 mm, 2.185 in. |
5.00 mm, 0.197 in. |
117
gm, 4.13 oz |
|
|
|
|
|
|
|
|
|
|
|
Test
Data From |
Input |
8.0 V |
10.0 V |
12.0V |
14.0V |
Measured
Kv value |
Measured
Rm Value |
|
|
|
|
|
Sample
Motor |
Io Value |
2.712 A |
2.925 A |
3.131 A |
3.333 A |
1518
RPM/Volt @ 10V |
0.0203
Ohms |
|
|
|
|
|
|
|
|
|
|
|
3-cell
Li-Po Test Data |
|
|
|
|
|
Prop |
Prop |
Li-Po |
Input |
Motor |
Input |
Prop |
Pitch Speed |
Thrust |
Thrust |
Thrust Eff. |
|
|
|
|
|
Manf. |
Size |
Cells |
Voltage |
Amps |
Watts |
RPM |
in MPH |
Grams |
Ounces |
Grams/W |
|
|
|
|
|
APC |
7x6-E |
3 |
11.1 |
28.26 |
313.7 |
14,734 |
83.7 |
1076 |
37.95 |
3.43 |
|
|
|
|
|
APC |
7x7-E |
3 |
11.1 |
34.29 |
380.6 |
14,313 |
94.9 |
1061 |
37.43 |
2.79 |
|
|
|
|
|
APC |
8x4-E |
3 |
11.1 |
31.83 |
353.3 |
14,475 |
54.8 |
1356 |
47.81 |
3.84 |
|
|
|
|
|
APC |
8x6-E |
3 |
11.1 |
44.57 |
494.7 |
13,569 |
77.1 |
1526 |
53.83 |
3.09 |
|
|
|
|
|
APC |
8x8-E |
3 |
11.1 |
60.38 |
670.2 |
12,368 |
93.7 |
1300 |
45.86 |
1.94 |
|
|
|
|
|
APC |
9x4.5-E |
3 |
11.1 |
44.63 |
495.4 |
13,559 |
57.8 |
1892 |
66.74 |
3.82 |
|
|
|
|
|
APC |
9x6-E |
3 |
11.1 |
50.98 |
565.9 |
13,083 |
74.3 |
1808 |
63.76 |
3.19 |
|
|
|
|
|
APC |
9x7.5-E |
3 |
11.1 |
72.62 |
806.0 |
11,775 |
83.6 |
1803 |
63.58 |
2.24 |
|
|
|
|
|
APC |
10x5-E |
3 |
11.1 |
58.68 |
651.3 |
12,450 |
58.9 |
2164 |
76.34 |
3.32 |
|
|
|
|
|
APC |
10x5.8-F2B |
3 |
11.1 |
62.83 |
697.4 |
11,996 |
65.9 |
2362 |
83.30 |
3.39 |
|
|
|
|
|
APC |
10x6-E |
3 |
11.1 |
63.36 |
703.3 |
12,083 |
68.7 |
2220 |
78.29 |
3.16 |
|
|
|
|
|
APC |
10x7-E |
3 |
11.1 |
72.71 |
807.0 |
11,700 |
77.6 |
2260 |
79.73 |
2.80 |
|
|
|
|
|
MAS |
7x4x3 |
3 |
11.1 |
22.77 |
252.8 |
15,109 |
57.2 |
955 |
33.67 |
3.78 |
|
|
|
|
|
MAS |
8x6x3 |
3 |
11.1 |
44.15 |
490.1 |
13,622 |
77.4 |
1724 |
60.83 |
3.52 |
|
|
|
|
|
MAS |
9x7x3 |
3 |
11.1 |
63.75 |
707.6 |
12,094 |
80.2 |
2253 |
79.48 |
3.18 |
|
|
|
|
|
MAS |
10x5x3 |
3 |
11.1 |
59.55 |
661.0 |
12,502 |
59.2 |
2386 |
84.15 |
3.61 |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
4-cell
Li-Po Test Data |
|
|
|
|
|
Prop |
Prop |
Li-Po |
Input |
Motor |
Input |
Prop |
Pitch Speed |
Thrust |
Thrust |
Thrust Eff. |
|
|
|
|
|
Manf. |
Size |
Cells |
Voltage |
Amps |
Watts |
RPM |
in MPH |
Grams |
Ounces |
Grams/W |
|
|
|
|
|
APC |
6x6-E |
4 |
14.8 |
28.86 |
427.1 |
19,938 |
113.3 |
968 |
34.15 |
2.27 |
|
|
|
|
|
APC |
7x4-E |
4 |
14.8 |
37.67 |
557.5 |
19,274 |
73.0 |
1671 |
58.95 |
3.00 |
|
|
|
|
|
APC |
7x5-E |
4 |
14.8 |
45.82 |
678.1 |
18,635 |
88.2 |
1606 |
56.66 |
2.37 |
|
|
|
|
|
APC |
7x6-E |
4 |
14.8 |
47.33 |
700.4 |
18,521 |
105.2 |
1728 |
60.95 |
2.47 |
|
|
|
|
|
APC |
7x7-E |
4 |
14.8 |
56.29 |
833.1 |
17,787 |
117.9 |
1641 |
57.88 |
1.97 |
|
|
|
|
|
APC |
8x4-E |
4 |
14.8 |
53.93 |
798.2 |
17,923 |
67.9 |
2125 |
74.96 |
2.66 |
|
|
|
|
|
APC |
8x6-E |
4 |
14.8 |
73.21 |
1083.5 |
16,588 |
94.3 |
2316 |
81.69 |
2.14 |
|
|
|
|
|
APC |
9x4.5-E |
4 |
14.8 |
73.51 |
1087.9 |
16,610 |
70.8 |
3004 |
105.97 |
2.76 |
|
|
|
|
|
MAS |
7x4x3 |
4 |
14.8 |
36.28 |
536.9 |
19,371 |
73.4 |
1596 |
56.30 |
2.97 |
|
|
|
|
|
MAS |
8x6x3 |
4 |
14.8 |
68.87 |
1019.3 |
17,067 |
97.0 |
2750 |
97.00 |
2.70 |
|
|
|
|
|
|
|
|
|
|
|
5-cell
Li-Po Test Data |
|
|
|
|
|
Prop |
Prop |
Li-Po |
Input |
Motor |
Input |
Prop |
Pitch Speed |
Thrust |
Thrust |
Thrust Eff. |
|
|
|
|
|
Manf. |
Size |
Cells |
Voltage |
Amps |
Watts |
RPM |
in MPH |
Grams |
Ounces |
Grams/W |
|
|
|
|
|
APC |
5x4.5-E |
5 |
18.5 |
28.90 |
534.6 |
25,833 |
110.1 |
1116 |
39.35 |
2.09 |
|
|
|
|
|
APC |
5x4.6-E |
5 |
18.5 |
28.29 |
523.4 |
25,895 |
112.8 |
1182 |
41.69 |
2.26 |
|
|
|
|
|
APC |
6x4-E |
5 |
18.5 |
33.18 |
613.8 |
25,486 |
96.5 |
1341 |
47.32 |
2.19 |
|
|
|
|
|
APC |
6x4.3E |
5 |
18.5 |
43.44 |
803.7 |
24,597 |
100.2 |
1909 |
67.33 |
2.38 |
|
|
|
|
|
APC |
6x4.5-E |
5 |
18.5 |
40.25 |
744.5 |
24,879 |
106.0 |
1887 |
66.57 |
2.53 |
|
|
|
|
|
APC |
6x5.5-E |
5 |
18.5 |
39.67 |
734.0 |
24,936 |
129.9 |
1411 |
49.76 |
1.92 |
|
|
|
|
|
APC |
6x6-E |
5 |
18.5 |
45.26 |
837.3 |
24,414 |
138.7 |
1440 |
50.78 |
1.72 |
|
|
|
|
|
APC |
7x4-E |
5 |
18.5 |
61.65 |
1140.6 |
22,964 |
87.0 |
2369 |
83.57 |
2.08 |
|
|
|
|
|
APC |
7x5-E |
5 |
18.5 |
68.55 |
1268.2 |
21,875 |
103.6 |
2241 |
79.03 |
1.77 |
|
|
|
|
|
MAS |
7x4x3 |
5 |
18.5 |
55.54 |
1027.4 |
23,507 |
89.0 |
2223 |
78.42 |
2.16 |
|
|
|
|
|
|
|
|
|
|
|
6-cell
Li-Po Test Data |
|
|
|
|
|
Prop |
Prop |
Li-Po |
Input |
Motor |
Input |
Prop |
Pitch Speed |
Thrust |
Thrust |
Thrust Eff. |
|
|
|
|
|
Manf. |
Size |
Cells |
Voltage |
Amps |
Watts |
RPM |
in MPH |
Grams |
Ounces |
Grams/W |
|
|
|
|
|
APC |
5x4.3E |
6 |
22.2 |
37.63 |
835.5 |
30,111 |
122.6 |
1524 |
53.76 |
1.82 |
|
|
|
|
|
APC |
5x4.5-E |
6 |
22.2 |
40.99 |
910.0 |
29,881 |
127.3 |
1511 |
53.31 |
1.66 |
|
|
|
|
|
APC |
5x4.6-E |
6 |
22.2 |
39.32 |
873.0 |
29,957 |
130.5 |
1599 |
56.40 |
1.83 |
|
|
|
|
|
APC |
6x4-E |
6 |
22.2 |
45.69 |
1014.4 |
29,401 |
111.4 |
1774 |
62.58 |
1.75 |
|
|
|
|
|
APC |
6x4.3E |
6 |
22.2 |
59.34 |
1317.3 |
28,140 |
114.6 |
2540 |
89.61 |
1.93 |
|
|
|
|
|
APC |
6x4.5-E |
6 |
22.2 |
53.35 |
1184.3 |
28,709 |
122.3 |
2535 |
89.43 |
2.14 |
|
|
|
|
|
APC |
6x5.5-E |
6 |
22.2 |
53.89 |
1196.4 |
28,650 |
149.2 |
1819 |
64.16 |
1.52 |
|
|
|
|
|
APC |
6x6-E |
6 |
22.2 |
60.18 |
1336.0 |
28,081 |
159.6 |
1846 |
65.10 |
1.38 |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
© 2019 Innov8tive Designs,
Inc. |
|
|
|
|
|
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. |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Propeller Chart Color Code Explanation |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
The
prop is to small to get good performance from the motor. (Less than 50%
power) |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
The
prop is sized right to get good power from the motor. (50 to 80% power) |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
The
prop can be used, but full throttle should be kept to short bursts. (80 to
100% power) |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
The
prop is too big for the motor and should not be used. (Over 100% power) |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
PLEASE NOTE: |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
The Data contained in this Prop Chart is
based on actual measurements, taken in a controlled test environment, at an
altitude of |
|
|
|
|
|
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 |
|
|
|
|
|
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 |
|
|
|
|
|
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 |
|
|
|
|
|
always test your actual power system with a
watt meter before flying your model to make sure that you are not exceeding
the |
|
|
|
|
|
recommended current and power ratings of the
motor being used. The prop
recommendations in this chart assume that the motor |
|
|
|
|
|
receives adequate cooling throughout its
operation. If your motor is being used
inside a cowl or fuselage, you must ensure that |
|
|
|
|
|
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 |
|
|
|
|
|
more than 80% of the motors maximum
recommended current value to ensure safe operation under all conditions. |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|