Vertiq 81-08 G2 240Kv (w/ Rotor Cover)

P18x6.1R

Philadelphia, PA USA | 15m | 2025-03-05 | 24.9 C | 29.77 in Hg | 31.0% 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 4 370 0.00 3.7 10 2.4
4.0 48.4 0.2 11 840 0.02 13.4 60 5.4
6.0 48.4 0.5 22 1340 0.04 27.2 170 7.8
8.0 48.4 0.8 38 1840 0.08 40.4 330 8.7
10.0 48.4 1.3 63 2330 0.13 51.0 550 8.8
12.0 48.4 2.0 95 2810 0.19 60.2 830 8.7
14.0 48.3 2.9 139 3280 0.27 66.3 1170 8.4
16.0 48.3 4.0 192 3740 0.35 70.7 1530 8.0
18.0 48.2 5.4 259 4190 0.44 74.1 1940 7.5
20.0 48.2 7.0 339 4620 0.54 76.7 2390 7.0
22.0 48.2 8.9 428 5060 0.64 78.9 2860 6.7
24.0 48.1 11.2 538 5470 0.75 80.1 3390 6.3
26.0 48.0 13.6 655 5870 0.87 81.6 3900 6.0
28.0 47.9 16.3 781 6240 0.98 82.0 4420 5.7
30.0 47.8 19.3 921 6620 1.10 83.0 4970 5.4
32.0 47.8 22.5 1075 6930 1.23 82.8 5540 5.2
34.0 47.7 25.7 1226 7280 1.34 83.5 6030 4.9
36.0 47.5 29.6 1409 7570 1.48 83.2 6670 4.7
38.0 47.4 33.8 1601 7860 1.61 83.0 7300 4.6
40.0 47.3 37.6 1779 8130 1.73 82.6 7770 4.4
42.0 47.2 41.8 1972 8370 1.84 82.0 8340 4.2
44.0 47.0 46.2 2172 8630 1.96 81.6 8830 4.1

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.