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

SRZ18x6.1R

Philadelphia, PA USA | 15m | 2025-03-05 | 24.6 C | 29.72 in Hg | 32.6% 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 3.0 10 2.2
4.0 48.4 0.2 11 840 0.02 12.9 60 5.4
6.0 48.4 0.5 22 1340 0.04 26.5 170 7.8
8.0 48.4 0.8 38 1840 0.08 39.8 330 8.7
10.0 48.4 1.3 62 2330 0.13 50.7 560 9.0
12.0 48.4 2.0 95 2810 0.19 59.3 840 8.9
14.0 48.3 2.9 140 3280 0.26 64.6 1180 8.4
16.0 48.3 4.0 192 3750 0.34 69.6 1540 8.0
18.0 48.2 5.3 257 4200 0.43 74.4 1970 7.7
20.0 48.2 7.0 338 4640 0.53 76.0 2410 7.1
22.0 48.1 8.9 428 5070 0.63 78.6 2900 6.8
24.0 48.1 11.1 533 5480 0.74 79.9 3420 6.4
26.0 48.0 13.5 648 5880 0.85 80.8 3910 6.0
28.0 47.9 16.1 774 6260 0.97 82.0 4470 5.8
30.0 47.9 19.2 916 6610 1.09 82.2 5030 5.5
32.0 47.8 22.2 1061 6950 1.21 82.7 5580 5.3
34.0 47.7 25.5 1214 7270 1.32 83.0 6090 5.0
36.0 47.6 29.1 1383 7580 1.45 83.0 6700 4.8
38.0 47.4 32.9 1559 7900 1.56 82.8 7220 4.6
40.0 47.3 36.8 1743 8180 1.68 82.5 7740 4.4
42.0 47.2 40.8 1927 8460 1.79 82.1 8240 4.3
44.0 47.1 45.4 2139 8680 1.91 81.4 8810 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.