Vertiq 81-17 110Kv (w/ Rotor Cover)

G26x8.5R

Philadelphia, PA USA | 15m | 2025-03-13 | 23.8 C | 30.05 in Hg | 25.9% Humidity

Commanded Voltage (V)	Supply Voltage (V)	Supply Current (A)	Input Power (W)	Speed (RPM)	Torque (Nm)	Motor-Controller Efficiency (%)	Thrust (g)	Propulsion Efficiency (g/W)
2.0	48.4	0.1	5	180	0.01	2.4	10	2.2
4.0	48.4	0.2	8	380	0.02	11.5	60	7.5
6.0	48.4	0.3	14	590	0.05	24.1	150	10.7
8.0	48.4	0.5	22	810	0.10	36.6	290	12.9
10.0	48.4	0.7	35	1020	0.15	47.2	470	13.4
12.0	48.4	1.1	53	1230	0.23	55.0	700	13.3
14.0	48.4	1.5	74	1450	0.31	63.0	950	12.9
16.0	48.4	2.1	101	1660	0.40	68.7	1250	12.3
18.0	48.3	2.8	134	1860	0.50	72.7	1580	11.8
20.0	48.3	3.7	178	2070	0.62	75.2	2000	11.2
22.0	48.3	4.8	230	2270	0.75	77.4	2420	10.5
24.0	48.2	5.9	285	2480	0.87	79.3	2830	9.9
26.0	48.2	7.3	351	2680	1.01	80.7	3280	9.4
28.0	48.1	8.9	428	2880	1.19	83.6	3840	9.0
30.0	48.1	10.8	517	3070	1.37	85.0	4390	8.5
32.0	48.0	12.8	613	3260	1.53	85.2	4970	8.1
34.0	48.0	14.9	715	3450	1.69	85.6	5500	7.7
36.0	47.9	17.2	824	3640	1.87	86.7	6070	7.4
38.0	47.8	20.0	958	3820	2.09	87.1	6730	7.0
40.0	47.7	23.3	1111	4000	2.33	87.7	7520	6.8
42.0	47.6	26.4	1255	4170	2.49	86.7	8100	6.5
44.0	47.5	30.0	1423	4340	2.73	87.1	8840	6.2
46.0	47.4	34.0	1609	4500	2.96	86.7	9670	6.0
48.0	47.3	36.6	1730	4610	3.17	88.5	10160	5.9

Published data is rated for continuous thrust at Normal Temperature and Pressure.

Performance is degraded at higher temperatures and lower pressures.

Performance may exceed published data temporarily, but cannot be sustained continuously.