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BadAss
BA-2826-1360 Performance Test Data |
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Magnets |
Motor Wind |
Motor Kv |
No-Load Current |
Motor Resistance |
I Max |
P Max (6S) |
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14-Pole |
6-Turn Delta |
1360 RPM/Volt |
Io = 3.70 Amps @ 10v |
Rm = 0.013 Ohms |
95 Amps |
2110W |
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Stator |
Outside Diameter |
Body Length |
Total Shaft Length |
Shaft Diameter |
Motor
Weight |
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12-Slot |
35.6 mm, 1.402 in. |
46.0 mm, 1.811 in. |
66.5 mm, 2.657 in. |
5.00 mm, 0.197 in. |
186
gm, 6.56 oz |
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Test
Data From |
Input |
10.0 V |
12.0 V |
14.0V |
16.0V |
Measured
Kv value |
Measured
Rm Value |
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Sample
Motor |
Io Value |
3.049 A |
3.508 A |
3.710 A |
3.982 A |
1366
RPM/Volt @ 10V |
0.0126
Ohms |
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3-cell
Li-Po Test Data |
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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 |
7x7-E |
3 |
11.1 |
30.88 |
342.8 |
13,840 |
91.7 |
1009 |
35.59 |
2.94 |
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APC |
8x6-E |
3 |
11.1 |
44.40 |
492.8 |
13,252 |
75.3 |
1510 |
53.25 |
3.06 |
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APC |
8x8-E |
3 |
11.1 |
57.26 |
635.6 |
12,736 |
96.5 |
1416 |
49.94 |
2.23 |
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APC |
9x4.5-E |
3 |
11.1 |
40.17 |
445.8 |
13,427 |
57.2 |
1859 |
65.56 |
4.17 |
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APC |
9x6-E |
3 |
11.1 |
47.93 |
532.1 |
13,122 |
74.6 |
1828 |
64.48 |
3.44 |
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APC |
9x7.5-E |
3 |
11.1 |
70.59 |
783.5 |
12,218 |
86.8 |
1945 |
68.60 |
2.48 |
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APC |
9x9-E |
3 |
11.1 |
79.21 |
879.2 |
11,892 |
101.4 |
1920 |
67.72 |
2.18 |
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APC |
10x5-E |
3 |
11.1 |
57.36 |
636.7 |
12,750 |
60.4 |
2279 |
80.38 |
3.58 |
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APC |
10x5.8-F2B |
3 |
11.1 |
62.05 |
688.8 |
12,627 |
69.4 |
2615 |
92.24 |
3.80 |
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APC |
10x6-E |
3 |
11.1 |
64.36 |
714.4 |
12,498 |
71.0 |
2409 |
84.97 |
3.37 |
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APC |
10x6-F |
3 |
11.1 |
50.68 |
562.5 |
12,988 |
73.8 |
2185 |
77.08 |
3.88 |
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APC |
10x7-E |
3 |
11.1 |
73.60 |
816.9 |
12,118 |
80.3 |
2482 |
87.56 |
3.04 |
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APC |
10x8-E |
3 |
11.1 |
81.18 |
901.1 |
11,830 |
89.6 |
2511 |
88.58 |
2.79 |
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APC |
10x10-E |
3 |
11.1 |
95.66 |
1061.8 |
10,826 |
102.5 |
2022 |
71.32 |
1.90 |
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APC |
11x5.5-E |
3 |
11.1 |
78.75 |
874.1 |
11,912 |
62.0 |
3141 |
110.81 |
3.59 |
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APC |
11x7-E |
3 |
11.1 |
91.43 |
1014.8 |
11,382 |
75.4 |
3140 |
110.77 |
3.09 |
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APC |
11x8-E |
3 |
11.1 |
99.68 |
1106.4 |
11,000 |
83.3 |
2901 |
102.33 |
2.62 |
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APC |
11x8-F |
3 |
11.1 |
82.00 |
910.2 |
11,765 |
89.1 |
3090 |
108.99 |
3.39 |
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MAS |
8x6x3 |
3 |
11.1 |
40.21 |
446.4 |
13,442 |
76.4 |
1675 |
59.08 |
3.75 |
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MAS |
9x7x3 |
3 |
11.1 |
62.77 |
696.7 |
12,517 |
83.0 |
2454 |
86.56 |
3.52 |
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MAS |
10x5x3 |
3 |
11.1 |
57.30 |
636.1 |
12,737 |
60.3 |
2531 |
89.27 |
3.98 |
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MAS |
10x7x3 |
3 |
11.1 |
80.03 |
888.3 |
11,851 |
78.6 |
3045 |
107.41 |
3.43 |
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MAS |
11x7x3 |
3 |
11.1 |
93.38 |
1036.5 |
11,248 |
74.6 |
3436 |
121.21 |
3.32 |
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4-cell
Li-Po Test Data |
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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 |
7x5-E |
4 |
14.8 |
39.93 |
591.0 |
18,227 |
86.3 |
1543 |
54.44 |
2.61 |
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APC |
7x6-E |
4 |
14.8 |
40.98 |
606.5 |
18,183 |
103.3 |
1652 |
58.27 |
2.72 |
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APC |
7x7-E |
4 |
14.8 |
51.81 |
766.7 |
17,684 |
117.2 |
1648 |
58.12 |
2.15 |
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APC |
8x4-E |
4 |
14.8 |
48.66 |
720.2 |
17,825 |
67.5 |
2084 |
73.50 |
2.89 |
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APC |
8x6-E |
4 |
14.8 |
78.93 |
1168.2 |
16,411 |
93.2 |
2335 |
82.36 |
2.00 |
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APC |
8x8-E |
4 |
14.8 |
94.05 |
1392.0 |
15,750 |
119.3 |
2150 |
75.82 |
1.54 |
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APC |
9x4.5-E |
4 |
14.8 |
68.95 |
1020.4 |
16,912 |
72.1 |
3106 |
109.57 |
3.04 |
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APC |
9x6-E |
4 |
14.8 |
81.53 |
1206.7 |
16,350 |
92.9 |
2904 |
102.42 |
2.41 |
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MAS |
8x6x3 |
4 |
14.8 |
63.92 |
946.0 |
17,153 |
97.5 |
2776 |
97.92 |
2.93 |
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MAS |
9x7x3 |
4 |
14.8 |
98.28 |
1454.6 |
15,567 |
103.2 |
3595 |
126.81 |
2.47 |
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MAS |
10x5x3 |
4 |
14.8 |
90.18 |
1334.7 |
15,934 |
75.4 |
4071 |
143.58 |
3.05 |
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5-cell
Li-Po Test Data |
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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 |
7x5-E |
5 |
18.5 |
61.41 |
1136.0 |
21,840 |
103.4 |
2223 |
78.41 |
1.96 |
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APC |
7x6-E |
5 |
18.5 |
63.09 |
1167.1 |
21,758 |
123.6 |
2344 |
82.66 |
2.01 |
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APC |
7x7-E |
5 |
18.5 |
77.08 |
1426.0 |
21,085 |
139.8 |
2323 |
81.94 |
1.63 |
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APC |
8x4-E |
5 |
18.5 |
74.46 |
1377.5 |
21,253 |
80.5 |
2971 |
104.79 |
2.16 |
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MAS |
8x6x3 |
5 |
18.5 |
93.54 |
1730.5 |
20,263 |
115.1 |
3684 |
129.94 |
2.13 |
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© 2019 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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