| Max Thrust | 17 kg/rotor (44.4 V, Sea Level) |
|---|---|
| Recommended Battery | 12S LiPo |
| Recommended Takeoff Weight | 6.0 - 8.0 kg/rotor (Sea Level) |
| Frame Arm Outer Diameter | 40 mm |
| Frame Arm Inner Diameter | 37mm |
| Operating Temperature | -10 to 50 ℃ |
| Stator Size | 100×15 mm |
|---|---|
| KV | 115 rpm/V |
| Weight | 654 g |
| Max Allowable Voltage | 52.2 V |
|---|---|
| Max Allowable Current (Continuous) | 100 A |
| Max Peak Current (< 3 sec) | 130 A |
| PWM Input Signal Level | 3.3 V / 5 V Compatible |
| Operating Pulse Width | 1120 to1920 μs |
| Signal Frequency | 30 Hz to 500 Hz |
| Battery | 12S LiPo |
| Diameter x Thread Pitch | 33×9 inch (840×230 mm) |
|---|---|
| Weight (Single Propeller) | 315 g |
The data above was measured with an input voltage of 44.4 V, at a temperature of 25℃ and sea level. The thrust was adjusted by the throttle.
The data above was measured at full throttle, at a temperature of 25℃ and sea level.
I – Current, P – Input Power, η – Electrical Efficiency, T – Thrust,
N – Rotational Speed
The data above was measured with an input voltage of 44.4 V, at a temperature of 25℃ and sea level. The rotational speed was adjusted by the throttle.
η – Efficiency, I – Current, P – Output Power, Τ – Torque, N – Rotational Speed
The data above contain theoretical values measured with an input voltage of 44.4 V,
for reference only. When operating at a temperature of 25℃ with no additional
cooling devices, the motor cannot operate with a current more than 85 A. It can
support short term operation (about 10 to 30 sec) with a current between 50 A
and 85 A, and continuous operation with a current under 50 A. The motor run time
should depend on the actual environmental temperature and cooling conditions.