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Scorpion
SII-4025-440 Motor Propeller 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 |
13-Turn Delta |
440 RPM/Volt |
Io = 1.10 Amps @ 10v |
Rm = 0.025 Ohms |
85 Amps |
2000 W |
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Stator |
Outside Diameter |
Body Length |
Total Shaft Length |
Shaft Diameter |
Motor Weight |
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12-Slot |
48.9 mm, 1.925 in. |
54.1 mm, 2.129 in. |
85 mm, 3.346 in. |
5.98 mm, 0.235 in. |
353 gm, 11.96 oz |
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Test Data
From |
Input |
12.0 V |
16.0 V |
20.0V |
24.0V |
Measured Kv value |
Measured Rm Value |
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Sample Motor |
Io Value |
1.19 A |
1.37 A |
1.56 A |
1.76 A |
451 RPM/Volt |
0.023 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 |
13x10-E |
5 |
18.5 |
35.73 |
661.0 |
7,253 |
68.7 |
2339 |
82.50 |
3.54 |
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APC |
14x10-E |
5 |
18.5 |
32.61 |
603.3 |
7,345 |
69.6 |
2923 |
103.10 |
4.84 |
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APC |
14x12-E |
5 |
18.5 |
48.30 |
893.6 |
6,935 |
78.8 |
2603 |
91.82 |
2.91 |
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APC |
15x8-E |
5 |
18.5 |
34.50 |
638.3 |
7,296 |
55.3 |
3336 |
117.67 |
5.23 |
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APC |
15x10-E |
5 |
18.5 |
49.98 |
924.7 |
6,883 |
65.2 |
3654 |
128.89 |
3.95 |
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APC |
16x8-E |
5 |
18.5 |
53.74 |
994.2 |
6,803 |
51.5 |
4297 |
151.57 |
4.32 |
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APC |
16x10-E |
5 |
18.5 |
56.20 |
1039.7 |
6,564 |
62.2 |
4214 |
148.64 |
4.05 |
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APC |
16x12-E |
5 |
18.5 |
69.56 |
1286.8 |
6,396 |
72.7 |
3742 |
131.99 |
2.91 |
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APC |
17x8-E |
5 |
18.5 |
57.58 |
1065.2 |
6,704 |
50.8 |
4786 |
168.82 |
4.49 |
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APC |
17x10-E |
5 |
18.5 |
68.01 |
1258.3 |
6,418 |
60.8 |
4846 |
170.94 |
3.85 |
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APC |
17x12-E |
5 |
18.5 |
76.29 |
1411.3 |
6,226 |
70.8 |
4655 |
164.20 |
3.30 |
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APC |
18x8-E |
5 |
18.5 |
59.28 |
1096.6 |
6,649 |
50.4 |
5591 |
197.21 |
5.10 |
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APC |
18x10-E |
5 |
18.5 |
68.52 |
1267.6 |
6,420 |
60.8 |
5688 |
200.64 |
4.49 |
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APC |
18x12-E |
5 |
18.5 |
86.56 |
1601.4 |
5,735 |
65.2 |
4834 |
170.51 |
3.02 |
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APC |
19x8-E |
5 |
18.5 |
79.52 |
1471.2 |
6,111 |
46.3 |
6161 |
217.32 |
4.19 |
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APC |
19x10-E |
5 |
18.5 |
77.21 |
1428.5 |
6,174 |
58.5 |
6313 |
222.68 |
4.42 |
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APC |
19x12-E |
5 |
18.5 |
88.62 |
1639.4 |
5,873 |
66.7 |
6231 |
219.79 |
3.80 |
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APC |
20x8-E |
5 |
18.5 |
80.35 |
1486.5 |
6,084 |
46.1 |
6796 |
239.72 |
4.57 |
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APC |
20x10-E |
5 |
18.5 |
92.28 |
1707.2 |
5,813 |
55.0 |
7003 |
247.02 |
4.10 |
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MAS |
14x7x3 |
5 |
18.5 |
35.15 |
650.3 |
7,263 |
48.1 |
3493 |
123.21 |
5.37 |
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MAS |
14x9x3 |
5 |
18.5 |
42.06 |
778.2 |
7,081 |
60.3 |
3874 |
136.65 |
4.98 |
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MAS |
15x7x3 |
5 |
18.5 |
43.82 |
810.7 |
7,038 |
46.7 |
4145 |
146.21 |
5.11 |
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MAS |
16x8x3 |
5 |
18.5 |
51.34 |
949.8 |
6,839 |
51.8 |
4767 |
168.15 |
5.02 |
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MAS |
16x10x3 |
5 |
18.5 |
64.80 |
1198.8 |
6,519 |
61.7 |
5446 |
192.10 |
4.54 |
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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 |
13x8-E |
6 |
22.2 |
36.43 |
808.7 |
8,744 |
66.2 |
3290 |
116.05 |
4.07 |
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APC |
13x10-E |
6 |
22.2 |
47.67 |
1058.3 |
8,245 |
78.1 |
3049 |
107.55 |
2.88 |
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APC |
14x7-E |
6 |
22.2 |
43.28 |
960.8 |
8,535 |
56.6 |
3903 |
137.67 |
4.06 |
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APC |
14x8.5-E |
6 |
22.2 |
44.45 |
986.9 |
8,516 |
68.5 |
3977 |
140.28 |
4.03 |
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APC |
14x10-E |
6 |
22.2 |
43.32 |
961.7 |
8,356 |
79.1 |
3748 |
132.21 |
3.90 |
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APC |
14x12-E |
6 |
22.2 |
64.89 |
1440.6 |
7,945 |
90.3 |
3405 |
120.11 |
2.36 |
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APC |
15x4-E |
6 |
22.2 |
32.72 |
726.4 |
8,861 |
33.6 |
3944 |
139.12 |
5.43 |
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APC |
15x6-E |
6 |
22.2 |
44.65 |
991.1 |
8,507 |
48.3 |
4603 |
162.36 |
4.64 |
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APC |
15x8-E |
6 |
22.2 |
48.45 |
1075.6 |
8,413 |
63.7 |
4457 |
157.21 |
4.14 |
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APC |
15x10-E |
6 |
22.2 |
67.22 |
1492.4 |
7,707 |
73.0 |
4578 |
161.48 |
3.07 |
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APC |
16x8-E |
6 |
22.2 |
72.46 |
1608.5 |
7,562 |
57.3 |
5315 |
187.48 |
3.30 |
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APC |
16x10-E |
6 |
22.2 |
82.53 |
1832.2 |
7,465 |
70.7 |
5406 |
190.69 |
2.95 |
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APC |
16x12-E |
6 |
22.2 |
92.57 |
2055.0 |
7,180 |
81.6 |
4787 |
168.85 |
2.33 |
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APC |
17x8-E |
6 |
22.2 |
80.01 |
1776.3 |
7,524 |
57.0 |
5936 |
209.38 |
3.34 |
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APC |
17x10-E |
6 |
22.2 |
91.89 |
2040.0 |
7,171 |
67.9 |
6076 |
214.32 |
2.98 |
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APC |
18x8-E |
6 |
22.2 |
82.53 |
1832.2 |
7,501 |
56.8 |
7346 |
259.12 |
4.01 |
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MAS |
13x8x3 |
6 |
22.2 |
40.23 |
893.1 |
8,646 |
65.5 |
3992 |
140.81 |
4.47 |
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MAS |
14x7x3 |
6 |
22.2 |
45.46 |
1009.3 |
8,309 |
55.1 |
4613 |
162.72 |
4.57 |
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MAS |
14x9x3 |
6 |
22.2 |
56.73 |
1259.3 |
8,168 |
69.6 |
5274 |
186.03 |
4.19 |
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MAS |
15x7x3 |
6 |
22.2 |
59.39 |
1318.5 |
8,080 |
53.6 |
5674 |
200.14 |
4.30 |
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MAS |
16x8x3 |
6 |
22.2 |
65.83 |
1461.4 |
7,746 |
58.7 |
6250 |
220.46 |
4.28 |
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MAS |
16x10x3 |
6 |
22.2 |
85.77 |
1904.1 |
7,361 |
69.7 |
7168 |
252.84 |
3.76 |
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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 |
12x8-E |
7 |
25.9 |
39.25 |
1016.6 |
10,189 |
77.2 |
3187 |
112.42 |
3.14 |
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APC |
12x10-E |
7 |
25.9 |
48.75 |
1262.7 |
9,892 |
93.7 |
3319 |
117.07 |
2.63 |
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APC |
12x12-E |
7 |
25.9 |
51.60 |
1336.4 |
9,807 |
111.4 |
3150 |
111.11 |
2.36 |
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APC |
13x4-E |
7 |
25.9 |
26.49 |
686.2 |
10,824 |
41.0 |
3487 |
123.00 |
5.08 |
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APC |
13x6.5-E |
7 |
25.9 |
46.34 |
1200.2 |
9,965 |
61.3 |
4211 |
148.54 |
3.51 |
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APC |
13x8-E |
7 |
25.9 |
50.04 |
1296.1 |
9,859 |
74.7 |
4274 |
150.76 |
3.30 |
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APC |
13x10-E |
7 |
25.9 |
66.14 |
1713.1 |
9,342 |
88.5 |
3941 |
139.01 |
2.30 |
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APC |
14x7-E |
7 |
25.9 |
60.25 |
1560.5 |
9,554 |
63.3 |
5040 |
177.78 |
3.23 |
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APC |
14x8.5-E |
7 |
25.9 |
60.19 |
1559.0 |
9,552 |
76.9 |
4960 |
174.96 |
3.18 |
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APC |
14x10-E |
7 |
25.9 |
58.38 |
1512.0 |
9,390 |
88.9 |
4792 |
169.03 |
3.17 |
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APC |
15x4-E |
7 |
25.9 |
42.88 |
1110.5 |
9,868 |
37.4 |
5095 |
179.72 |
4.59 |
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APC |
15x6-E |
7 |
25.9 |
58.57 |
1517.0 |
9,388 |
53.3 |
5612 |
197.96 |
3.70 |
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APC |
15x8-E |
7 |
25.9 |
65.24 |
1689.6 |
9,399 |
71.2 |
5585 |
197.00 |
3.31 |
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APC |
15x10-E |
7 |
25.9 |
93.87 |
2431.3 |
8,548 |
80.9 |
5614 |
198.03 |
2.31 |
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APC |
16x8-E |
7 |
25.9 |
97.11 |
2515.1 |
8,390 |
63.6 |
6547 |
230.94 |
2.60 |
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MAS |
12x6x3 |
7 |
25.9 |
30.66 |
794.0 |
10,264 |
58.3 |
3515 |
123.99 |
4.43 |
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MAS |
12x8x3 |
7 |
25.9 |
46.11 |
1194.4 |
9,968 |
75.5 |
4655 |
164.20 |
3.90 |
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MAS |
13x8x3 |
7 |
25.9 |
51.67 |
1338.4 |
9,802 |
74.3 |
5176 |
182.58 |
3.87 |
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MAS |
14x7x3 |
7 |
25.9 |
60.90 |
1577.3 |
9,546 |
63.3 |
6133 |
216.33 |
3.89 |
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MAS |
14x9x3 |
7 |
25.9 |
72.22 |
1870.5 |
9,177 |
78.2 |
6738 |
237.67 |
3.60 |
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MAS |
15x7x3 |
7 |
25.9 |
76.00 |
1968.3 |
9,064 |
60.1 |
7341 |
258.94 |
3.73 |
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MAS |
16x8x3 |
7 |
25.9 |
83.33 |
2158.4 |
8,611 |
65.2 |
7792 |
274.85 |
3.61 |
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MAS |
16x10x3 |
7 |
25.9 |
104.31 |
2701.6 |
8,120 |
76.9 |
8793 |
310.16 |
3.25 |
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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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512 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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