The E2000 is DJI’s first tuned propulsion system specially engineered for industrial applications and aerial imagery. Using a combination of 6010 motors, 1240S/X ESCs, and R2170 propellers, the E2000 is designed to carry payloads of 1800–2500g per axis, giving it the power to carry substantial add-ons and advanced imaging equipment.
| Max Thrust | 5100 g/rotor (50 V, Sea Level) |
|---|---|
| Recommended Battery | 12S LiPo |
| Recommended Takeoff Weight | 1800 - 2500 g/rotor (Sea Level) |
| Powertrain Cable Length | 750 mm |
| Compatible Arm Tube Outer Diameter | 28 mm |
| Powertrain Weight (Single) | 430 g |
| Operating Temperature | -10° to 50° C |
| Stator Size | 60×10 mm |
|---|---|
| KV | 130 rpm/V |
| Weight | 230 g |
| Max Allowable Voltage | 52.2 V |
|---|---|
| Max Allowable Current (Persistent) | 25 A |
| Max Peak Current (3 sec) | 40 A |
| PWM Input Signal Level | 3.3 V / 5 V Compatible |
| Operating Pulse Width | 1120 to 1920 μs |
| Signal Frequency | 30 to 450 Hz |
| Battery | 12S LiPo |
| Diameter / Thread Pitch | 21 x 7.0 inch (533 x 178 mm) |
|---|---|
| Weight (single propeller) | 58 g |
| Max Thrust | 5100 g/rotor (50 V, Sea Level) |
|---|---|
| Recommended Battery | 12S LiPo |
| Recommended Takeoff Weight | 1800 - 2500 g/rotor (Sea Level) |
| Operating Temperature | -10° to 50° C |
| Stator Size | 60 x 10 mm |
|---|---|
| KV | 130 rpm/V |
| Weight | 230 g |
| Max Allowable Voltage | 52.2 V |
|---|---|
| Max Allowable Current (Continuous) | 25 A |
| Max Peak Current (3 sec) | 40 A |
| PWM Input Signal Level | 3.3 V / 5 V Compatible |
| Operating Pulse Width | 1120 to 1920 μs |
| Signal Frequency | 30 to 450 Hz |
| Battery | 12S LiPo |
| Dimensions | 85 mm x 44 mm x 18 mm |
| Cable Length | 750 mm |
| Weight (without cables) | 55 g |
| Weight (with cables) | 90 g |
| Diameter / Thread Pitch | 21 x 7.0 inch (533 x 178 mm) |
|---|---|
| Weight (single propeller) | 58 g |
The data above was measured with an input voltage of 44.4 V, at room temperature and sea level. The thrust was adjusted by the throttle.
η – Motor Efficiency, T – Thrust, I – Current, P – Input Power
The data above was measured with an input voltage of 44.4 V, at room temperature and sea level. The rotational speed was adjusted by the throttle.
The data above was measured at full throttle, at room temperature and sea level.
η – Efficiency, Τ– Torque, I – Current, P – Output Power
The data above was measured with an input voltage of 44.4 V and 100% duty cycle, at room temperature
and sea level. The rotational speed was adjusted by the payload torque.