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

P19x5.7R

Philadelphia, PA USA | 15m | 2025-03-05 | 23.4 C | 29.79 in Hg | 32.2% 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 48.4 0.1 5 370 0.00 4.0 10 2.1
4.0 48.4 0.2 11 840 0.02 15.9 70 6.3
6.0 48.5 0.5 23 1340 0.05 29.3 190 8.3
8.0 48.4 0.8 41 1840 0.09 41.5 370 9.1
10.0 48.4 1.4 66 2330 0.14 51.9 600 9.2
12.0 48.4 2.0 98 2800 0.20 60.6 890 9.1
14.0 48.4 3.0 144 3270 0.28 66.0 1230 8.6
16.0 48.3 4.1 200 3740 0.36 70.4 1620 8.1
18.0 48.3 5.5 266 4190 0.45 73.9 2030 7.6
20.0 48.2 7.3 350 4620 0.55 75.7 2470 7.1
22.0 48.2 9.1 441 5050 0.65 78.6 2970 6.7
24.0 48.1 11.5 551 5450 0.77 79.5 3480 6.3
26.0 48.0 13.9 668 5840 0.89 81.1 4030 6.0
28.0 47.9 16.7 800 6230 1.01 82.0 4580 5.7
30.0 47.8 19.8 947 6590 1.14 82.8 5180 5.5
32.0 47.7 23.0 1099 6910 1.26 83.0 5740 5.2
34.0 47.6 26.5 1263 7220 1.39 83.0 6280 5.0
36.0 47.5 30.3 1440 7530 1.51 82.6 6830 4.7
38.0 47.4 34.2 1622 7820 1.64 82.6 7420 4.6
40.0 47.3 38.2 1807 8110 1.76 82.7 7960 4.4
42.0 47.2 42.4 2001 8360 1.87 81.6 8380 4.2
44.0 47.0 47.3 2222 8580 1.99 80.5 8990 4.0

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.