Vertiq 81-08 G2 85Kv (w/ Rotor Cover)

FA36.2x11.8R

Philadelphia, PA USA | 15m | 2025-02-06 | 23.2 C | 29.95 in Hg | 25.4% 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 4 150 0.02 6.9 30 7.7
4.0 48.0 0.1 6 290 0.06 29.2 120 19.1
6.0 48.0 0.2 12 430 0.13 51.4 290 25.1
8.0 48.0 0.5 22 570 0.23 63.3 520 23.9
10.0 48.0 0.8 36 710 0.35 71.9 810 22.2
12.0 47.9 1.2 58 850 0.49 76.0 1140 19.8
14.0 47.9 1.8 84 990 0.65 80.1 1520 18.0
16.0 47.9 2.5 118 1120 0.82 81.4 1930 16.4
18.0 47.9 3.3 157 1240 1.00 82.4 2360 15.0
20.0 47.9 4.2 203 1350 1.18 82.0 2810 13.8
22.0 47.8 5.3 254 1460 1.35 81.5 3200 12.6
24.0 47.8 6.5 312 1550 1.55 80.8 3710 11.9
26.0 47.8 7.9 375 1640 1.74 79.8 4110 11.0
28.0 47.7 9.3 444 1730 1.93 78.9 4620 10.4
30.0 47.7 10.9 521 1800 2.13 77.1 5100 9.8
32.0 47.6 12.7 603 1880 2.30 75.0 5530 9.2

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.