UM1010 ultra-light and long-flight motor suitable for aerial photography and mapping drones
Parameter:
Motor model: UM1010
Structure form: 36N42P
Weight: 399g
Stator core size: φ100*10mm
Dimensions: φ107.6* 26.1mm
Spindle diameter: φ17mm
Output shaft diameter: φ10mm
Dynamic balance standard: ≤10mg
UM1010 KV78
Recommended for lithium battery: 12S-14S
Recommended propeller: 32-36 inches
Multi-rotor take-off weight: 4KG-6.5KG/ shaft
UM1010 KV85
Recommended for lithium battery: 12S-14S
Recommended propeller: 32-36 inches
Multi-rotor take-off weight: 4KG-7KG/ shaft
UM1010 KV95
Recommended for lithium battery: 12S-14S
Recommended propeller: 32-34 inches
Multi-rotor take-off weight: 4KG-6.5KG/ shaft
DRAWING
TEST REPORT
|
Power configuration Measured data |
|||||||||
|
Motor |
ESC |
Propeller |
Applicable |
Applicable |
Rated power |
Max thrust |
Max power |
||
|
UM1010 KV78 |
60A |
P3410 |
Multi-rotor drone |
4.0KG-5.5KG/shaft |
470W |
11KG |
1404W |
||
|
Load test data |
Lithium Battery :12S |
||||||||
|
Voltage |
Thrust |
Current |
RPM |
Power |
Efficiency |
Torque |
Throttle |
||
|
44.68 |
2265 |
2.93 |
1259 |
130.91 |
17.3016 |
0.9930 |
40% |
||
|
44.64 |
2751 |
3.84 |
1387 |
171.42 |
16.0485 |
1.1803 |
45% |
||
|
44.60 |
3455 |
5.17 |
1541 |
230.58 |
14.9838 |
1.4290 |
50% |
||
|
44.55 |
4175 |
7.01 |
1697 |
312.30 |
13.3687 |
1.7575 |
55% |
||
|
44.51 |
4853 |
8.91 |
1840 |
396.58 |
12.2370 |
2.0584 |
60% |
||
|
44.44 |
5613 |
10.7 |
1959 |
475.51 |
11.8042 |
2.3181 |
65% |
||
|
44.37 |
6346 |
12.86 |
2081 |
570.60 |
11.1217 |
2.6186 |
70% |
||
|
44.31 |
7077 |
15.51 |
2202 |
687.25 |
10.2976 |
2.9806 |
75% |
||
|
44.23 |
7701 |
18.2 |
2329 |
804.99 |
9.5666 |
3.3008 |
80% |
||
|
44.09 |
8692 |
21.57 |
2439 |
951.02 |
9.1396 |
3.7238 |
85% |
||
|
44.01 |
9469 |
24.91 |
2548 |
1096.29 |
8.6373 |
4.1089 |
90% |
||
|
43.91 |
10149 |
28.35 |
2655 |
1244.85 |
8.1528 |
4.4777 |
95% |
||
|
43.74 |
11038 |
32.11 |
2749 |
1404.49 |
7.8591 |
4.8792 |
100% |
||
|
The above numbers are drawn from the solid oil chamber: sea level, E8-2023 test flat |
|||||||||
|
Power configuration Measured data |
|||||||||
|
Motor |
ESC |
Propeller |
Applicable |
Applicable |
Rated power |
Max thrust |
Max power |
||
|
UM1010 KV78 |
60A |
P3612 |
Multi-rotor drone |
4.5KG- 6.0KG/shaft |
550W |
12.1KG |
1663W |
||
|
Load test data |
Lithium Battery :12S |
||||||||
|
Voltagc |
Thrust |
Current |
RPM |
Power |
Efficiency |
Torque |
Throttle |
||
|
44.61 |
2679 |
3.42 |
1240 |
152.57 |
17.5596 |
1.1750 |
40% |
||
|
44.64 |
3291 |
4.67 |
1363 |
208.47 |
15.7865 |
1.4607 |
45% |
||
|
44.57 |
4041 |
6.28 |
1508 |
279.90 |
14.4373 |
1.7726 |
50% |
||
|
44.50 |
4895 |
8.33 |
1651 |
370.69 |
13.2053 |
2.1442 |
55% |
||
|
44.44 |
5687 |
10.55 |
1785 |
468.84 |
12.1299 |
2.5084 |
60% |
||
|
44.37 |
6382 |
12.89 |
1896 |
571.93 |
11.1587 |
2.8808 |
65% |
||
|
44.25 |
7322 |
15.72 |
1999 |
695.61 |
10.5260 |
3.3232 |
70% |
||
|
44.19 |
8184 |
18.75 |
2115 |
828.56 |
9.8773 |
3.7413 |
75% |
||
|
44.09 |
9095 |
22.3 |
2214 |
983.21 |
9.2503 |
4.2410 |
80% |
||
|
43.99 |
9884 |
26.05 |
2310 |
1145.94 |
8.6252 |
4.7375 |
85% |
||
|
43.86 |
10732 |
29.89 |
2416 |
1310.98 |
8.1863 |
5.1820 |
90% |
||
|
43.69 |
11652 |
34.06 |
2484 |
1488.08 |
7.8302 |
5.7211 |
95% |
||
|
43.58 |
12140 |
38.18 |
2573 |
1663.88 |
7.2962 |
6.1757 |
100% |
||
|
The above numbers are drawn from the solid oil chamber: sea level, E8-2023 test flat |
|||||||||
|
Power configuration Measured data |
|||||||||
|
Motor |
ESC |
Propeller |
Applicable |
Applicable |
Rated power |
Max thrust |
Max power |
||
|
UM1010 KV78 |
60A |
P3210 |
Multi-rotor drone |
4.0KG-5.5KG/shaft |
550W |
12.1KG |
1715W |
||
|
Load test data |
Lithium Battery :12S |
||||||||
|
Voltage |
Thrust |
Current |
RPM |
Power |
Efficiency |
Torque |
Throttle |
||
|
52.20 |
2297 |
2.97 |
1464 |
155.03 |
14.8161 |
1.0113 |
40% |
||
|
52.15 |
2950 |
4.05 |
1642 |
211.21 |
13.9673 |
1.2284 |
45% |
||
|
52.13 |
3708 |
5.66 |
1837 |
295.06 |
12.5671 |
1.5339 |
50% |
||
|
52.07 |
4422 |
7.23 |
2009 |
376.47 |
11.7461 |
1.7896 |
55% |
||
|
52.03 |
5236 |
9.09 |
2155 |
472.95 |
11.0709 |
2.0959 |
60% |
||
|
51.93 |
5999 |
11.05 |
2301 |
573.83 |
10.4544 |
2.3816 |
65% |
||
|
51.89 |
6838 |
13.63 |
2456 |
707.26 |
9.6683 |
2.7501 |
70% |
||
|
51.82 |
7625 |
16.01 |
2592 |
829.64 |
9.1908 |
3.0567 |
75% |
||
|
51.71 |
8490 |
18.77 |
2734 |
970.60 |
8.7472 |
3.3903 |
80% |
||
|
51.63 |
9315 |
21.98 |
2877 |
1134.83 |
8.2083 |
3.7670 |
85% |
||
|
51.52 |
10461 |
25.99 |
3001 |
1339.00 |
7.8125 |
4.2611 |
90% |
||
|
51.39 |
11418 |
30.04 |
3123 |
1543.76 |
7.3962 |
4.7207 |
95% |
||
|
51.30 |
12104 |
33.45 |
3255 |
1715.99 |
7.0537 |
5.0346 |
100% |
||
|
The above numbers are drawn from the solid oil chamber: sea level, E8-2023 test flat |
|||||||||
|
Power configuration Measured data |
|||||||||
|
Motor |
ESC |
Propeller |
Applicable |
Applicable |
Rated power |
Max thrust |
Max power |
||
|
UM1010 KV78 |
60A |
P3410 |
Multi-rotor drone |
4.5KG-6.0KG/shaft |
560W |
13.5KG |
2008W |
||
|
Load test data |
Lithium Battery :12S |
||||||||
|
Voltage |
Thrust |
Current |
RPM |
Power |
Efficiency |
Torque |
Throttle |
||
|
52.17 |
2893 |
3.66 |
1428 |
190.94 |
15.1512 |
1.2770 |
40% |
||
|
52.15 |
3610 |
4.91 |
1596 |
256.06 |
14.0985 |
1.5322 |
45% |
||
|
52.09 |
4482 |
6.8 |
1778 |
354.21 |
12.6534 |
1.9025 |
50% |
||
|
52.02 |
5421 |
8.8 |
1946 |
457.78 |
11.8420 |
2.2465 |
55% |
||
|
51.94 |
6215 |
11.16 |
2090 |
579.65 |
10.7220 |
2.6486 |
60% |
||
|
51.88 |
7078 |
13.39 |
2224 |
694.67 |
10.1890 |
2.9830 |
65% |
||
|
51.80 |
8018 |
16.27 |
2352 |
842.79 |
9.5137 |
3.4220 |
70% |
||
|
51.70 |
8869 |
19.15 |
2479 |
990.06 |
8.9581 |
3.8140 |
75% |
||
|
51.57 |
9797 |
22.81 |
2604 |
1176.31 |
8.3286 |
4.3140 |
80% |
||
|
51.49 |
10780 |
26.66 |
2731 |
1372.72 |
7.8530 |
4.8003 |
85% |
||
|
51.34 |
11885 |
31.18 |
2834 |
1600.78 |
7.4245 |
5.3943 |
90% |
||
|
51.23 |
12823 |
35.2 |
2936 |
1803.30 |
7.1109 |
5.8656 |
95% |
||
|
51.11 |
13543 |
39.29 |
3053 |
2008.11 |
6.7441 |
6.2815 |
100% |
||
|
The above numbers are drawn from the solid oil chamber: sea level, E8-2023 test flat |
|||||||||
|
Power configuration Measured data |
|||||||||
|
Motor |
ESC |
Propeller |
Applicable |
Applicable |
Rated power |
Max thrust |
Max power |
||
|
UM1010 KV85 |
60A |
P3210 |
Multi-rotor drone |
4.0KG-5.5KG/shaft |
550W |
10.9KG |
2461W |
||
|
Load test data |
Lithium Battery :12S |
||||||||
|
Voltage |
Thrust |
Current |
RPM |
Power |
Efficiency |
Torque |
Throttle |
||
|
44.67 |
2092 |
2.87 |
1379 |
128.20 |
16.3179 |
0.8878 |
40% |
||
|
44.66 |
2612 |
3.95 |
1543 |
176.41 |
14.8067 |
1.0918 |
45% |
||
|
44.60 |
3236 |
5.38 |
1727 |
239.95 |
13.4863 |
1.3269 |
50% |
||
|
44.56 |
3928 |
7.15 |
1898 |
318.60 |
12.3288 |
1.6031 |
55% |
||
|
44.50 |
4675 |
9.04 |
2044 |
402.28 |
11.6213 |
1.8795 |
60% |
||
|
44.43 |
5319 |
10.93 |
2183 |
485.62 |
10.9530 |
2.1244 |
65% |
||
|
44.36 |
6072 |
13.15 |
2320 |
583.33 |
10.4091 |
2.4012 |
70% |
||
|
44.28 |
6824 |
15.82 |
2462 |
700.51 |
9.7415 |
2.7172 |
75% |
||
|
44.20 |
7665 |
18.67 |
2594 |
825.21 |
9.2885 |
3.0381 |
80% |
||
|
44.09 |
8427 |
21.88 |
2739 |
964.69 |
8.7355 |
3.3636 |
85% |
||
|
44.01 |
9241 |
25.59 |
2863 |
1126.22 |
8.2054 |
3.7567 |
90% |
||
|
43.87 |
10110 |
29.7 |
2979 |
1302.94 |
7.7594 |
4.1769 |
95% |
||
|
43.73 |
10952 |
33.42 |
3106 |
1461.46 |
7.4939 |
4.4935 |
100% |
||
|
The above numbers are drawn from the solid oil chamber: sea level, E8-2023 test flat |
|||||||||
|
Power configuration Measured data |
|||||||||
|
Motor |
ESC |
Propeller |
Applicable |
Applicable |
Rated power |
Max thrust |
Max power |
||
|
UM1010 KV85 |
60A |
P3410 |
Multi-rotor drone |
4.5KG-6.0KG/shaft |
550W |
12.4KG |
1730W |
||
|
Load test data |
Lithium Battery :12S |
||||||||
|
Voltage |
Thrust |
Current |
RPM |
Power |
Efficiency |
Torque |
Throttle |
||
|
44.65 |
2645 |
3.67 |
1359 |
163.87 |
16.1413 |
1.1515 |
40% |
||
|
44.61 |
3254 |
4.86 |
1515 |
216.80 |
15.0089 |
1.3667 |
45% |
||
|
44.55 |
4076 |
6.78 |
1687 |
302.05 |
13.4945 |
1.7099 |
50% |
||
|
44.48 |
4937 |
8.98 |
1848 |
399.43 |
12.3601 |
2.0642 |
55% |
||
|
44.45 |
5705 |
11.05 |
1987 |
491.17 |
11.6151 |
2.3607 |
60% |
||
|
44.35 |
6456 |
13.7 |
2113 |
607.60 |
10.6255 |
2.7461 |
65% |
||
|
44.28 |
7129 |
16.29 |
2238 |
721.32 |
9.8833 |
3.0780 |
70% |
||
|
44.15 |
8133 |
19.56 |
2368 |
863.57 |
9.4178 |
3.4827 |
75% |
||
|
44.07 |
8836 |
22.96 |
2488 |
1011.85 |
8.7325 |
3.8839 |
80% |
||
|
43.96 |
9600 |
26.72 |
2611 |
1174.61 |
8.1729 |
4.2963 |
85% |
||
|
43.81 |
10904 |
31.11 |
2721 |
1362.93 |
8.0004 |
4.7835 |
90% |
||
|
43.70 |
11541 |
35.03 |
2823 |
1530.81 |
7.5391 |
5.1786 |
95% |
||
|
43.56 |
12431 |
39.72 |
2915 |
1730.20 |
7.1847 |
5.6684 |
100% |
||
|
The above numbers are drawn from the solid oil chamber: sea level, E8-2023 test flat |
|||||||||
|
Power configuration Measured data |
|||||||||
|
Motor |
ESC |
Propeller |
Applicable |
Applicable |
Rated power |
Max thrust |
Max power |
||
|
UM1010 KV85 |
60A |
P3612 |
Multi-rotor drone |
5.0KG-6.5KG/shaft |
580W |
13.7KG |
2068W |
||
|
Load test data |
Lithium Battery :12S |
||||||||
|
Voltage |
Thrust |
Current |
RPM |
Power |
Efficiency |
Torque |
Throttle |
||
|
44.62 |
3168 |
4.53 |
1336 |
202.13 |
15.6732 |
1.4449 |
40% |
||
|
44.54 |
3953 |
6.06 |
1479 |
269.91 |
14.6455 |
1.7428 |
45% |
||
|
44.52 |
4840 |
8.19 |
1636 |
364.62 |
13.2741 |
2.1284 |
50% |
||
|
44.42 |
5790 |
10.98 |
1792 |
487.73 |
11.8713 |
2.5992 |
55% |
||
|
44.35 |
6779 |
13.67 |
1911 |
606.26 |
11.1816 |
3.0297 |
60% |
||
|
44.25 |
7694 |
16.59 |
2035 |
734.11 |
10.4808 |
3.4451 |
65% |
||
|
44.16 |
8554 |
19.75 |
2142 |
872.16 |
9.8078 |
3.8885 |
70% |
||
|
44.04 |
9386 |
23.8 |
2263 |
1048.15 |
8.9548 |
4.4233 |
75% |
||
|
43.93 |
10378 |
28.01 |
2364 |
1230.48 |
8.4341 |
4.9708 |
80% |
||
|
43.76 |
11120 |
32.79 |
2458 |
1434.89 |
7.7497 |
5.5749 |
85% |
||
|
43.64 |
12227 |
37.15 |
2546 |
1621.23 |
7.5418 |
6.0812 |
90% |
||
|
43.46 |
12896 |
42.55 |
2623 |
1849.22 |
6.9737 |
6.7328 |
95% |
||
|
43.31 |
13784 |
47.75 |
2685 |
2068.05 |
6.6652 |
7.3556 |
100% |
||
|
The above numbers are drawn from the solid oil chamber: sea level, E8-2023 test flat |
|||||||||
|
Power configuration Measured data |
|||||||||
|
Motor |
ESC |
Propeller |
Applicable |
Applicable |
Rated power |
Max thrust |
Max power |
||
|
UM1010 KV85 |
60A |
P3210 |
Multi-rotor drone |
4.5KG-6.0KG/shaft |
580W |
13.6KG |
2096W |
||
|
Load test data |
Lithium Battery :12S |
||||||||
|
Voltage |
Thrust |
Current |
RPM |
Power |
Efficiency |
Torque |
Throttle |
||
|
52.17 |
2781 |
3.72 |
1588 |
194.07 |
14.3297 |
1.1671 |
40% |
||
|
52.13 |
3542 |
5.3 |
1809 |
276.29 |
12.8199 |
1.4586 |
45% |
||
|
52.09 |
4489 |
7.29 |
1998 |
379.74 |
11.8214 |
1.8151 |
50% |
||
|
52.02 |
5342 |
9.35 |
2171 |
486.39 |
10.9830 |
2.1396 |
55% |
||
|
51.94 |
6155 |
11.37 |
2337 |
590.56 |
10.4223 |
2.4133 |
60% |
||
|
51.85 |
6961 |
13.73 |
2481 |
711.90 |
9.7781 |
2.7403 |
65% |
||
|
51.80 |
7733 |
16.39 |
2642 |
849.00 |
9.1083 |
3.0689 |
70% |
||
|
51.70 |
8641 |
19.51 |
2809 |
1008.67 |
8.5668 |
3.4293 |
75% |
||
|
51.58 |
9735 |
23.39 |
2948 |
1206.46 |
8.0691 |
3.9083 |
80% |
||
|
51.46 |
10788 |
27.72 |
3092 |
1426.47 |
7.5627 |
4.4058 |
85% |
||
|
51.33 |
11790 |
31.77 |
3229 |
1630.75 |
7.2298 |
4.8231 |
90% |
||
|
51.19 |
12867 |
36.94 |
3331 |
1890.96 |
6.8045 |
5.4214 |
95% |
||
|
51.00 |
13649 |
41.11 |
3473 |
2096.61 |
6.5100 |
5.7652 |
100% |
||
|
The above numbers are drawn from the solid oil chamber: sea level, E8-2023 test flat |
|||||||||
|
Power configuration Measured data |
|||||||||
|
Motor |
ESC |
Propeller |
Applicable |
Applicable |
Rated power |
Max thrust |
Max power |
||
|
UM1010 KV85 |
60A |
P3410 |
Multi-rotor drone |
5.0KG-7.0KG/shaft |
650W |
15.1KG |
2479W |
||
|
Load test data |
Lithium Battery :12S |
||||||||
|
Voltage |
Thrust |
Current |
RPM |
Power |
Efficiency |
Torque |
Throttle |
||
|
52.15 |
3381 |
4.61 |
1538 |
240.41 |
14.0634 |
1.4928 |
40% |
||
|
52.11 |
4375 |
6.51 |
1738 |
339.24 |
12.8966 |
1.8640 |
45% |
||
|
52.04 |
5322 |
8.82 |
1930 |
458.99 |
11.5950 |
2.2712 |
50% |
||
|
51.93 |
6401 |
11.37 |
2090 |
590.44 |
10.8410 |
2.6980 |
55% |
||
|
51.87 |
7238 |
14.01 |
2236 |
726.70 |
9.9601 |
3.1037 |
60% |
||
|
51.76 |
8145 |
17.04 |
2382 |
881.99 |
9.2348 |
3.5361 |
65% |
||
|
51.69 |
9203 |
20.03 |
2501 |
1035.35 |
8.8888 |
3.9535 |
70% |
||
|
51.55 |
10240 |
24.36 |
2647 |
1255.76 |
8.1544 |
4.5306 |
75% |
||
|
51.45 |
11236 |
28.44 |
2779 |
1463.24 |
7.6789 |
5.0284 |
80% |
||
|
51.27 |
12114 |
32.95 |
2903 |
1689.35 |
7.1708 |
5.5574 |
85% |
||
|
51.14 |
13082 |
38.06 |
3017 |
1946.39 |
6.7212 |
6.1611 |
90% |
||
|
50.97 |
14124 |
43.18 |
3126 |
2200.88 |
6.4174 |
6.7238 |
95% |
||
|
50.81 |
15165 |
48.8 |
3204 |
2479.53 |
6.1161 |
7.3906 |
100% |
||
|
The above numbers are drawn from the solid oil chamber: sea level, E8-2023 test flat |
|||||||||
|
Power configuration Measured data |
|||||||||
|
Motor |
ESC |
Propeller |
Applicable |
Applicable |
Rated power |
Max thrust |
Max power |
||
|
UM1010 KV95 |
60A |
P3210 |
Multi-rotor drone |
4.0KG-6.0KG/shaft |
580W |
12.2KG |
1795W |
||
|
Load test data |
Lithium Battery :12S |
||||||||
|
Voltage |
Thrust |
Current |
RPM |
Power |
Efficiency |
Torque |
Throttle |
||
|
44.65 |
2420 |
3.72 |
1503 |
166.10 |
14.5697 |
1.0554 |
40% |
||
|
44.61 |
3167 |
5.32 |
1690 |
237.33 |
13.3446 |
1.3411 |
45% |
||
|
44.55 |
3934 |
7.12 |
1884 |
317.20 |
12.4024 |
1.6079 |
50% |
||
|
44.49 |
4628 |
9.11 |
2055 |
405.30 |
11.4186 |
1.8835 |
55% |
||
|
44.42 |
5453 |
11.5 |
2196 |
510.83 |
10.6748 |
2.2215 |
60% |
||
|
44.34 |
6135 |
13.89 |
2350 |
615.88 |
9.9613 |
2.5028 |
65% |
||
|
44.28 |
6903 |
16.41 |
2484 |
726.63 |
9.5000 |
2.7936 |
70% |
||
|
44.14 |
7838 |
19.82 |
2628 |
874.85 |
8.9592 |
3.1792 |
75% |
||
|
44.08 |
8606 |
23.3 |
2779 |
1027.06 |
8.3792 |
3.5295 |
80% |
||
|
43.93 |
9532 |
27.33 |
2927 |
1200.61 |
7.9393 |
3.9173 |
85% |
||
|
43.81 |
10407 |
31.45 |
3046 |
1377.82 |
7.5532 |
4.3198 |
90% |
||
|
43.64 |
11527 |
36.72 |
3147 |
1602.46 |
7.1933 |
4.8629 |
95% |
||
|
43.52 |
12292 |
41.25 |
3259 |
1795.20 |
6.8471 |
5.2606 |
100% |
||
|
The above numbers are drawn from the solid oil chamber: sea level, E8-2023 test flat |
|||||||||
|
Power configuration Measured data |
|||||||||
|
Motor |
ESC |
Propeller |
Applicable |
Applicable |
Rated power |
Max thrust |
Max power |
||
|
UM1010 KV95 |
60A |
P3410 |
Multi-rotor drone |
4.5KG-6.5KG/shaft |
620W |
13.5KG |
2077W |
||
|
Load test data |
Lithium Battery :12S |
||||||||
|
Voltage |
Thrust |
Current |
RPM |
Power |
Efficiency |
Torque |
Throttle |
||
|
44.63 |
3054 |
4.73 |
1464 |
211.10 |
14.4671 |
1.3771 |
40% |
||
|
44.59 |
3858 |
6.58 |
1638 |
293.40 |
13.1492 |
1.7106 |
45% |
||
|
44.49 |
4779 |
8.83 |
1824 |
392.85 |
12.1651 |
2.0568 |
50% |
||
|
44.43 |
5702 |
11.28 |
1980 |
501.17 |
11.3774 |
2.4173 |
55% |
||
|
44.35 |
6517 |
14.13 |
2126 |
626.67 |
10.3995 |
2.8150 |
60% |
||
|
44.24 |
7302 |
17.05 |
2256 |
754.29 |
9.6806 |
3.1930 |
65% |
||
|
44.15 |
8170 |
20.39 |
2390 |
900.22 |
9.0756 |
3.5971 |
70% |
||
|
44.06 |
9100 |
23.92 |
2505 |
1053.92 |
8.6345 |
4.0179 |
75% |
||
|
43.89 |
10114 |
28.49 |
2628 |
1250.43 |
8.0884 |
4.5440 |
80% |
||
|
43.76 |
10925 |
33.11 |
2752 |
1448.89 |
7.5402 |
5.0280 |
85% |
||
|
43.61 |
11894 |
38.02 |
2854 |
1658.05 |
7.1735 |
5.5481 |
90% |
||
|
43.45 |
12517 |
42.56 |
2955 |
1849.23 |
6.7688 |
5.9764 |
95% |
||
|
43.30 |
13516 |
47.97 |
3040 |
2077.10 |
6.5071 |
6.5251 |
100% |
||
|
The above numbers are drawn from the solid oil chamber: sea level, E8-2023 test flat |
|||||||||
|
Power configuration Measured data |
|||||||||
|
Motor |
ESC |
Propeller |
Applicable |
Applicable |
Rated power |
Max thrust |
Max power |
||
|
UM1010 KV95 |
60A |
P3210 |
Multi-rotor drone |
5KG-6.5KG/shaft |
630W |
14.9KG |
2539W |
||
|
Load test data |
Lithium Battery :12S |
||||||||
|
Voltage |
Thrust |
Current |
RPM |
Power |
Efficiency |
Torque |
Throttle |
||
|
52.14 |
3206 |
4.68 |
1723 |
244.02 |
13.1385 |
1.3525 |
40% |
||
|
52.08 |
4225 |
6.87 |
1947 |
357.79 |
11.8086 |
1.7550 |
45% |
||
|
52.02 |
5048 |
8.95 |
2148 |
465.58 |
10.8424 |
2.0700 |
50% |
||
|
51.96 |
6020 |
11.48 |
2331 |
596.50 |
10.0922 |
2.4438 |
55% |
||
|
51.85 |
6934 |
14.26 |
2479 |
739.38 |
9.3781 |
2.8484 |
60% |
||
|
51.74 |
8054 |
17.41 |
2625 |
900.79 |
8.9410 |
3.2772 |
65% |
||
|
51.65 |
8785 |
20.6 |
2801 |
1063.99 |
8.2567 |
3.6277 |
70% |
||
|
51.53 |
9882 |
24.77 |
2964 |
1276.40 |
7.7421 |
4.1126 |
75% |
||
|
51.42 |
10795 |
28.89 |
3106 |
1485.52 |
7.2668 |
4.5675 |
80% |
||
|
51.27 |
11893 |
33.56 |
3262 |
1720.62 |
6.9120 |
5.0374 |
85% |
||
|
51.12 |
12899 |
38.64 |
3382 |
1975.28 |
6.5302 |
5.5777 |
90% |
||
|
50.95 |
13993 |
44.35 |
3490 |
2259.63 |
6.1926 |
6.1832 |
95% |
||
|
50.78 |
14929 |
50.01 |
3605 |
2539.51 |
5.8787 |
6.7274 |
100% |
||
|
The above numbers are drawn from the solid oil chamber: sea level, E8-2023 test flat |
|||||||||