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Drone Power Consumption & Current Calculator

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Estimate electrical power in watts and battery current in amps

Power & Current Calculator

Assumptions
  • Battery current (A) = electrical power (W) ÷ average pack voltage (V)
  • Peak current estimated as 1.4× average (typical burst)
  • C-rate warnings at 8C (caution) and 12C (high risk)
When This Estimate Breaks Down
  • High C-rates cause voltage sag and heat buildup
  • Aggressive maneuvers may exceed peak estimates
  • Battery age and temperature affect actual performance

Power & Current Results

C-rate
1.0C
Estimated Power70.0WSelected flight mode · average pack voltage: 14.0 V
Average Current (Total from Battery)5.0A
Peak Current (Total from Battery)7.0A
Avg per Motor / Peak per Motor1.3 / 1.8A
Required for 10 min1042mAh
Est. Flight Time48.0min
ESC Recommendation2AEach ESC should be rated for at least 2 A (per motor)
💡 Total current is from battery pack. Per-motor current is for ESC sizing.
ConfidenceMEDIUM
Design RiskLOW
C-rate (1.0C) is within safe limits.
Check Motor Specs

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Estimated Power70.0 W

Understanding drone power consumption

Compare battery choices in the flight time calculator
  1. Watts, amps and watt-hours

    Power (W) is the rate of electrical energy use. Current (A) is the flow drawn from the battery. At the battery terminals, power = voltage × current, so current = power ÷ voltage. Energy (Wh) is power multiplied by time in hours; it describes how much energy a battery can supply.

    The result panel shows the electrical power estimated for the selected flight mode and the associated average battery current. It uses an average pack voltage of cell count × 3.5 V. This differs from the nominal battery label of cell count × 3.7 V.

  2. Example: a 2 kg drone with a 4S battery

    Select Standard mode, Hover, 2 kg, 4S, 5,000 mAh and 85% system efficiency. The estimated power is about 198 W. At an average pack voltage of 14 V, the average current is 198 ÷ 14 ≈ 14.1 A. With four motors, the model divides that total equally: about 3.5 A per motor.

    The battery has 5 Ah of nominal capacity. With 80% usable capacity, estimated hover time is 60 × (5 × 0.8) ÷ 14.1 ≈ 17 minutes. These rounded values illustrate the model; a measured power trace will vary during flight.

  3. Average current and peak current

    Average current is used for the endurance estimate. Peak current is estimated as 1.4× average current; this multiplier does not capture every motor-start or maneuvering transient. Check battery, motor and ESC data and measured loads before selecting hardware.

    For fixed power, a higher pack voltage means lower current, not lower power. If changing the battery also changes weight, update the weight input. The selected flight mode changes the power estimate, while battery age, temperature and voltage sag can make actual consumption differ.

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