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

FA34.2x11.2R

Philadelphia, PA USA | 15m | 2025-02-06 | 23.6 C | 30.03 in Hg | 23.2% 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 3 140 0.01 5.4 30 8.6
4.0 48.0 0.1 5 290 0.05 27.3 100 19.4
6.0 48.0 0.2 10 430 0.10 46.8 240 24.3
8.0 48.0 0.4 17 580 0.18 63.0 430 24.6
10.0 48.0 0.6 30 730 0.28 70.8 670 22.2
12.0 48.0 1.0 47 870 0.39 76.1 960 20.5
14.0 47.9 1.5 71 1010 0.52 78.3 1290 18.3
16.0 47.9 2.1 98 1150 0.67 81.7 1670 17.0
18.0 47.9 2.8 133 1280 0.82 82.2 2030 15.2
20.0 47.9 3.6 172 1400 0.98 83.1 2440 14.2
22.0 47.9 4.5 214 1520 1.12 83.3 2800 13.1
24.0 47.8 5.6 266 1630 1.30 83.3 3230 12.1
26.0 47.8 6.7 321 1730 1.47 82.8 3660 11.4
28.0 47.8 8.0 380 1820 1.63 81.8 4100 10.8
30.0 47.7 9.4 447 1910 1.81 81.0 4570 10.2
32.0 47.7 10.7 512 2000 1.96 79.9 4940 9.6
34.0 47.6 12.4 592 2070 2.14 78.3 5450 9.2
36.0 47.6 13.9 660 2160 2.26 77.5 5720 8.7

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.