Axisflying C206 2006
| Stator | 2006 |
|---|---|
| KV options | 1960, 2750 |
| Weight | 22.0 g |
| Shaft | 1.5mm |
| Max cells | 4-6S |
| Configuration | 12N14P |
| Dimensions | 24.7x19.9 mm |
| Mount | 9x9mm (4-M2) |
| Winding resistance | 88 (2100KV) mOhm |
| Max thrust | 869 g |
| Price (approx.) | 29.99 USD |
Thrust data (Axisflying bench test)
| KV | Prop | Battery | Throttle | Current | RPM | Thrust | Efficiency |
|---|---|---|---|---|---|---|---|
| 1960 | DT90-3 | 6S | 30 | 3.13 A | 18931 | 217 g | 2.9 g/W |
| 1960 | DT90-3 | 6S | 40 | 4.61 A | 21858 | 293 g | 2.7 g/W |
| 1960 | DT90-3 | 6S | 50 | 6.09 A | 24358 | 368 g | 2.5 g/W |
| 1960 | DT90-3 | 6S | 60 | 7.68 A | 26515 | 441 g | 2.4 g/W |
| 1960 | DT90-3 | 6S | 70 | 10.05 A | 29157 | 537 g | 2.2 g/W |
| 1960 | DT90-3 | 6S | 80 | 13.66 A | 32412 | 665 g | 2.0 g/W |
| 1960 | DT90-3 | 6S | 90 | 17.63 A | 35382 | 796 g | 1.9 g/W |
| 1960 | DT90-3 | 6S | 100 | 19.9 A | 36924 | 869 g | 1.8 g/W |
| 2100 | DT90-3 | 6S | 20 | 1.86 A | 15323 | 151 g | 3.4 g/W |
| 2100 | DT90-3 | 6S | 30 | 3.6 A | 19356 | 246 g | 2.8 g/W |
| 2100 | DT90-3 | 6S | 40 | 5.47 A | 22679 | 339 g | 2.6 g/W |
| 2100 | DT90-3 | 6S | 50 | 6.92 A | 25156 | 430 g | 2.6 g/W |
| 2100 | DT90-3 | 6S | 60 | 8.94 A | 27591 | 527 g | 2.5 g/W |
| 2100 | DT90-3 | 6S | 70 | 12.2 A | 30841 | 660 g | 2.3 g/W |
| 2100 | DT90-3 | 6S | 80 | 16.36 A | 34084 | 811 g | 2.1 g/W |
| 2100 | DT90-3 | 6S | 90 | 21.29 A | 37122 | 967 g | 1.9 g/W |
| 2100 | DT90-3 | 6S | 100 | 23.89 A | 38489 | 1047 g | 1.8 g/W |
| 2100 | DT90-4 | 6S | 20 | 1.93 A | 14190 | 148 g | 3.2 g/W |
| 2100 | DT90-4 | 6S | 30 | 3.69 A | 18052 | 248 g | 2.8 g/W |
| 2100 | DT90-4 | 6S | 40 | 5.53 A | 20887 | 335 g | 2.5 g/W |
| 2100 | DT90-4 | 6S | 50 | 7.39 A | 23343 | 422 g | 2.4 g/W |
| 2100 | DT90-4 | 6S | 60 | 9.96 A | 26065 | 527 g | 2.2 g/W |
| 2100 | DT90-4 | 6S | 70 | 14.11 A | 29308 | 670 g | 2.0 g/W |
| 2100 | DT90-4 | 6S | 80 | 19.0 A | 32188 | 817 g | 1.8 g/W |
| 2100 | DT90-4 | 6S | 90 | 24.58 A | 34659 | 963 g | 1.7 g/W |
| 2100 | DT90-4 | 6S | 100 | 27.59 A | 35977 | 1023 g | 1.6 g/W |
| 2500 | DT90-3 | 6S | 20 | 2.91 A | 17574 | 197 g | 2.8 g/W |
| 2500 | DT90-3 | 6S | 30 | 5.58 A | 21264 | 278 g | 2.1 g/W |
| 2500 | DT90-3 | 6S | 40 | 7.8 A | 24770 | 398 g | 2.1 g/W |
| 2500 | DT90-3 | 6S | 50 | 10.56 A | 28093 | 526 g | 2.1 g/W |
| 2500 | DT90-3 | 6S | 60 | 13.51 A | 30907 | 629 g | 2.0 g/W |
| 2500 | DT90-3 | 6S | 70 | 18.04 A | 34331 | 770 g | 1.8 g/W |
| 2500 | DT90-3 | 6S | 80 | 23.3 A | 37786 | 936 g | 1.7 g/W |
| 2500 | DT90-3 | 6S | 90 | 29.64 A | 40752 | 1092 g | 1.6 g/W |
| 2500 | DT90-3 | 6S | 100 | 32.92 A | 41942 | 1153 g | 1.5 g/W |
| 2500 | DT90-4 | 6S | 20 | 3.15 A | 16944 | 205 g | 2.7 g/W |
| 2500 | DT90-4 | 6S | 30 | 5.68 A | 20141 | 305 g | 2.2 g/W |
| 2500 | DT90-4 | 6S | 40 | 8.12 A | 23432 | 447 g | 2.3 g/W |
| 2500 | DT90-4 | 6S | 50 | 10.97 A | 26117 | 577 g | 2.2 g/W |
| 2500 | DT90-4 | 6S | 60 | 14.86 A | 28958 | 720 g | 2.0 g/W |
| 2500 | DT90-4 | 6S | 70 | 20.72 A | 32071 | 886 g | 1.8 g/W |
| 2500 | DT90-4 | 6S | 80 | 26.89 A | 35431 | 1076 g | 1.7 g/W |
| 2500 | DT90-4 | 6S | 90 | 33.68 A | 37908 | 1238 g | 1.6 g/W |
| 2500 | DT90-4 | 6S | 100 | 37.73 A | 39114 | 1311 g | 1.5 g/W |
Manufacturer bench figures (Axisflying bench, 6S, throttle sweep per KV on the DT90-3 and DT90-4 props; 1960/2100/2500 KV tested, 26-28 degC ambient); real-world thrust varies with ESC, battery sag and prop condition.
C206 2006 vs other 2006 motors on 6S
The same thrust costs different power on different motors. Each line is one maker's own bench series (6S, its own prop), drawn as grams of thrust per watt against thrust, so a higher line makes that thrust for less battery current. Throttle percent is left out on purpose: it means something different on every maker's rig.
| Motor | KV | Prop | Peak thrust | At 650 g | At 1300 g | |
|---|---|---|---|---|---|---|
| Axisflying C206 2006 | 2500 | DT90-4 | 1311 g at 887 W | 309 W (2.1 g/W) | 873 W (1.49 g/W) | |
| VCI HOBBY Spark 2006 | 1850 | GF 5125-3 | 1340 g at 597 W | 224 W (2.91 g/W) | 573 W (2.27 g/W) |
Power at 650 g and 1300 g is read off each maker's curve, straight-line between its two nearest bench points; 1300 g is the highest thrust every motor here reached. Different props and rigs move these curves as much as the motor does, so compare rows on a similar prop. How to read a bench table: reading motor bench tables.
Thrust-to-weight with this motor
Four Axisflying C206 2006 motors at 869 g max thrust each give 3476 g: 2:1, the minimum to fly, up to 1738 g all-up; 4:1 (freestyle) up to 869 g; 8:1 (racing) up to 434.5 g.
RPM & prop speed on this motor
Props in this motor's class
| Prop | Size | Blades | Weight |
|---|---|---|---|
| Gemfan Long Range 5126-2 Durable 1.5mm T-Mount | 5.1x2.7 | 2 | 2.6 g |
| HQProp DP 5.1x2.5x3 | 5.1x2.5 | 3 | 3.1 g |
| HQProp Juicy J37 | 4.9x3.7 | 3 | 3.4 g |
| HQProp Juicy J40 | 5.1x4.0 | 3 | 3.4 g |
| Gemfan 4935 Sbang 3-Blade | 4.9x3.5 | 3 | 3.45 g |
Where this data comes from
Axisflying's C206-V1 sheet covers 1960, 2100 and 2500 KV; our retail source lists a 2750 KV version the manufacturer publishes no data for, so the table does not cover it. 22.8 g with wire, 24.7x19.9 mm, 12N14P, 1.5 mm shaft, 4-6S, 88 mOhm at 2100 KV. Motor temperature at full throttle 44-83 degC. Efficiency is printed to one decimal on this sheet, unlike Axisflying's 5in motor sheets. max_thrust_g is the sold winding's own best (owner ruling 2026-10-20: it comes from a winding the page sells; rows of other windings stay).