|
Propeller (D×P) |
Li-Po cell number |
Voltage (V) Current (A) |
Power (W) Thrust (kg) |
RPM |
|---|---|---|---|---|
| 9×6SF | 3cell |
12.6V 40A |
504W 1.2Kg |
8,470 |
| 9×6E | 3cell |
12.6V 29A |
365W 1.3kg |
10,850 |
| 9×7.5E | 3cell |
12.6V 36A |
454W 1.3Kg |
9,950 |
| 10×3.8SF | 3cell |
12.6V 40A |
504W 1.4kg |
8,960 |
| 10×4.7SF | 3cell |
12.6V 40A |
504W 1.4Kg |
8,750 |
| 10×5E | 3cell |
12.6V 30A |
378W 1.5kg |
10,600 |
| 10×7E | 3cell |
12.6V 40A |
504W 1.4kg |
9,380 |
| 11×3.8SF | 3cell |
12.6V 41A |
517W 1.8Kg |
9,000 |
| 11×3.8SF | 3cell |
12.6V 43A |
542W 1.4kg |
8,150 |
| 11×4.7SF | 3cell |
12.6V 48A |
605W 1.3kg |
7,250 |
| 11×5.5E | 3cell |
12.6V 38A |
479W 1.7Kg |
9,380 |
| 11×7E | 3cell |
12.6V 43A |
542W 1.5Kg |
8,380 |
* Propeller data is an example. Uses APC propeller. E after the pitch is for
electric. Others are for engines. The battery is the number of cells when using
a Li-Po battery. Note that each data is for reference only and may vary
depending on various conditions. It is necessary to actually measure and confirm
the current value with a measuring instrument or the like. Use within the
allowable range of the controller (ESC) or Li-Po battery.
Caution * Voltage is measured by the voltage when fully charged.
* ESC uses our ESC (OCA series)
* APC is used as the propeller.
* 17x8E * Propeller used is * XOAR
* SF: For electric slow flight. E: For
electric.