Vertiq 81-08 G2 140Kv (w/ Rotor Cover)

P24x7.2R

Philadelphia, PA USA | 15m | 2025-02-06 | 23.2 C | 29.82 in Hg | 28.8% 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 48.0 0.1 4 250 0.01 3.8 30 7.4
4.0 48.0 0.1 7 510 0.02 16.6 80 11.1
6.0 48.0 0.3 12 780 0.05 33.3 170 13.9
8.0 48.0 0.4 21 1060 0.09 48.7 320 15.0
10.0 48.0 0.7 36 1340 0.15 58.7 540 15.1
12.0 47.9 1.2 56 1620 0.22 67.7 790 14.1
14.0 47.9 1.8 86 1900 0.32 73.9 1110 13.0
16.0 47.9 2.5 122 2160 0.41 76.7 1470 12.0
18.0 47.9 3.4 164 2420 0.52 79.9 1840 11.2
20.0 47.8 4.5 213 2680 0.63 82.3 2240 10.5
22.0 47.8 5.7 275 2910 0.75 83.4 2660 9.7
24.0 47.7 7.1 340 3140 0.86 83.5 3090 9.1
26.0 47.7 8.7 414 3360 0.99 84.4 3570 8.6
28.0 47.6 10.3 492 3570 1.12 84.9 3980 8.1
30.0 47.6 12.3 584 3760 1.25 84.4 4500 7.7
32.0 47.5 14.1 672 3960 1.38 84.9 4940 7.3
34.0 47.5 16.2 769 4140 1.49 84.2 5350 7.0
36.0 47.4 18.3 869 4320 1.61 84.0 5780 6.6
38.0 47.4 20.9 992 4470 1.77 83.4 6370 6.4
40.0 47.3 23.4 1107 4620 1.88 82.3 6710 6.1
42.0 47.2 25.9 1223 4790 1.99 81.8 7140 5.8
44.0 47.1 28.7 1354 4930 2.12 80.7 7500 5.5

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.