Nominal Pack Voltage
Series cell count multiplied by nominal cell voltage.
The Drone Battery Calculator estimates LiPo pack voltage, watt-hours, usable energy, average battery current and approximate flight time from cell count, battery capacity and average power draw. It can also estimate the mAh capacity needed for a target mission duration.
Use it for 3S, 4S, 6S and other drone packs, then compare the result with your aircraft's real hover power, battery limits, payload and reserve strategy before flying.
Planning estimates only — battery weight and changing flight power can materially change real endurance.
Enter the ratings for your battery and an average in-flight power estimate. The calculator separates nominal battery energy, your planned usable percentage and electrical efficiency so you can see exactly how each assumption changes the answer.
The Drone Battery Calculator reports both energy and endurance values so you can distinguish what the pack stores from what the aircraft can realistically use under the assumptions entered above.
Series cell count multiplied by nominal cell voltage.
Total label-equivalent energy before applying reserve or losses.
Nominal energy after applying your selected usable battery percentage.
Estimated endurance at constant average watts after the entered reserve and efficiency.
Approximate battery current associated with the entered average power.
Average current divided by pack capacity in amp-hours; peak demand can be much higher.
Calculated capacity before accounting for the extra weight of a different battery.
Usable energy after the additional efficiency assumption.
A 4S battery using 3.7V nominal cells is modeled as a 14.8V pack. At 5000mAh it stores about 74Wh nominally. With 80% usable capacity and 95% efficiency, about 56.24Wh is modeled as available to a 250W average load, giving approximately 13.5 minutes of flight time.
Current calculation: 74 Wh × 80% × 95% ÷ 250 W × 60 = 13.50 minutes.
The Drone Battery Calculator begins by converting the battery's cell count and nominal cell voltage into nominal pack voltage. A conventional 4S LiPo entered at 3.7V per cell becomes 14.8V nominal. The tool does not assume every lithium pack uses 3.7V, however. High-voltage lithium packs and other chemistries can use different nominal values, so the voltage field remains editable.
Next, capacity is converted from milliamp-hours to amp-hours and multiplied by pack voltage. That produces watt-hours, which are more useful than mAh alone when comparing battery energy. A 5000mAh 4S pack at 14.8V stores about 74Wh nominally. If you need only that conversion, the site's mAh to Wh Calculator or Watt Hour Calculator provides a more focused calculation.
The calculator then applies your chosen usable percentage. Drone pilots commonly keep some energy in reserve rather than planning around every theoretical watt-hour, but the correct margin depends on the aircraft, battery, flight profile, manufacturer instructions and operating goals. The input is therefore a planning assumption rather than a universal recommendation.
Finally, the model applies an efficiency percentage and divides available energy by average flight power. Average watts matter far more to endurance than a motor's advertised maximum wattage. A multirotor may draw very different power while hovering, climbing rapidly, flying forward in wind or carrying a payload. Whenever possible, use logged or measured average battery power from a representative flight.
Watt-hours divided by watts gives hours directly. This makes energy and runtime easier to compare between 3S, 4S, 6S and higher-voltage systems.
For a more general non-drone runtime calculation, compare the Battery Runtime Calculator.
Usable percentage represents the part of battery energy you plan to withdraw. Efficiency represents modeled electrical loss between battery energy and the power value being supplied.
If your average watts are measured directly at the battery, setting efficiency to 100% usually avoids subtracting those same electrical losses a second time.
The calculations are intentionally transparent so every result can be checked by hand. They assume nominal voltage and constant average power. Real drone voltage, current and power continuously change during a flight.
For a 4S pack using 3.7V nominal cells, pack voltage is 4 × 3.7 = 14.8V. A 6S pack using the same nominal cell value is 22.2V. Always use the nominal value appropriate to the actual battery rather than copying a voltage from an unrelated chemistry.
A 5000mAh battery equals 5Ah. At 14.8V, nominal energy is 5 × 14.8 = 74Wh. This same relationship is why two batteries with identical mAh ratings can store very different amounts of energy when their voltages differ. The Battery Capacity Calculator can help when converting among Ah, mAh and Wh.
At an 80% usable setting, a 74Wh pack contributes 59.2Wh to the next calculation step. The remaining 20% is treated as planned reserve in this model. It should not be interpreted as a specific low-voltage cutoff recommendation.
With 95% modeled efficiency, 59.2Wh becomes 56.24Wh. Efficiency is optional in the conceptual sense: if your entered power already describes battery-side watts, use 100% so losses are not counted twice.
With 56.24Wh delivered and a 250W average load, calculated endurance is roughly 13.5 minutes. That number is a mathematical baseline, not a guaranteed flight duration. Wind, battery temperature, maneuvers, voltage sag, payload, battery age and pilot reserve can all alter the result.
This reverses the runtime equation to estimate capacity for a mission target. It is most useful for comparing possibilities. A calculated requirement of 6000mAh does not mean replacing a 4000mAh pack with a heavier 6000mAh pack will produce the predicted duration, because the additional battery mass can increase the power required to stay airborne.
Battery watt-hours are only one part of endurance. These factors explain why a Drone Battery Calculator estimate can differ from an actual timed flight even when the battery label is entered correctly.
More capacity generally means more stored energy, but a larger pack also adds mass. The aircraft must create additional lift, which can increase hover power. Cameras, delivery payloads, guards and accessories have the same basic effect. This is why a heavier battery does not produce a perfectly proportional increase in flight time.
Runtime is highly sensitive to the watts entered. Smooth hover, aggressive acceleration, rapid climbing and high-speed forward flight can produce different averages. Logged battery voltage and current can provide a better estimate than adding motor nameplate ratings together.
A headwind, repeated direction changes and sustained climbing can raise energy consumption. A flight-time estimate based on calm hover data may therefore be optimistic for an outdoor mission that includes fast travel or significant altitude changes.
Battery temperature, age, cell balance and internal resistance can affect voltage behavior and available energy under load. An older pack may reach a voltage warning earlier than a fresh battery even when both have the same capacity printed on the label.
Propeller diameter, pitch, motor choice, operating RPM and airframe layout influence the electrical power required for thrust. A battery calculation cannot determine whether the propulsion combination itself is efficient or correctly matched.
A responsible mission normally includes enough energy to land without relying on the final theoretical watt-hour. The usable percentage field lets you model a reserve, while a dedicated battery depth-of-discharge calculation can help compare reserve percentages more directly.
These examples use the same equations as the calculator. They are mathematical comparisons rather than recommendations for a particular drone, ESC, motor or battery.
A conventional 4S pack entered at 3.7V per cell is 14.8V nominal. With 5000mAh, or 5Ah, nominal battery energy is 74Wh. At 80% planned usable energy, 59.2Wh remains in the model. Applying 95% efficiency gives 56.24Wh. Dividing 56.24Wh by 250W and multiplying by 60 produces an estimated 13.5 minutes.
The corresponding average battery current is approximately 17.8A when the 95% efficiency assumption is used. Dividing that current by 5Ah gives an average C-load of roughly 3.56C. This average should not be confused with the battery's required peak-discharge capability during rapid throttle changes.
A 3S battery using 3.7V nominal cells is 11.1V. At 2200mAh, nominal energy is about 24.42Wh. An 80% usable setting leaves 19.54Wh and 95% efficiency reduces modeled delivered energy to about 18.56Wh. At 180W average power, estimated endurance is roughly 6.2 minutes.
If you are comparing several small LiPo packs, the LiPo Battery Calculator adds chemistry-focused energy and discharge context, while the mAh-to-Wh tool is useful when all you need is pack energy.
Suppose a 6S aircraft averages 500W and uses 3.7V nominal cells. Pack voltage is 22.2V. With an 80% usable setting and 95% efficiency, the mathematical capacity required for 12 minutes is about 5,927mAh. That does not automatically mean a 6000mAh pack will provide a true 12-minute mission. If the new pack is substantially heavier than the battery used to measure 500W, the aircraft's average power may increase.
| Example Pack | Nominal Wh | Average Power | Usable / Efficiency | Estimated Time | Approx. Average Current |
|---|---|---|---|---|---|
| 3S 2200mAh | 24.42Wh | 180W | 80% / 95% | ≈ 6.19 min | ≈ 17.07A |
| 4S 5000mAh | 74Wh | 250W | 80% / 95% | ≈ 13.50 min | ≈ 17.78A |
| 6S 5000mAh | 111Wh | 500W | 80% / 95% | ≈ 10.12 min | ≈ 23.71A |
These comparisons also demonstrate why mAh cannot be evaluated without voltage. A 5000mAh 6S battery stores substantially more energy than a 5000mAh 4S battery because the 6S pack operates at a higher nominal voltage. The site's broader Lithium Battery Calculator is useful when comparing battery energy outside drone-specific applications.
The Drone Battery Calculator is designed for energy planning, not airworthiness approval. A mathematically correct runtime does not prove that a battery can safely supply the required current or that the aircraft is suitable for the proposed pack.
The calculator derives average C-load from average current divided by capacity in amp-hours. A drone can demand much more current during acceleration, recovery, rapid climb or aggressive maneuvering.
Battery suitability therefore requires the actual pack specification and current data from the aircraft. Use the LiPo Battery Calculator for additional discharge-rate calculations, but still confirm the battery manufacturer's ratings.
Use the charger, voltage limits, temperature limits and storage procedure specified for your exact battery. Do not charge a visibly damaged, swollen or otherwise abnormal pack. For product-specific storage and maintenance practices, consult the aircraft or battery manufacturer; DJI publishes a current battery routine maintenance guide for its supported camera-drone batteries.
If you travel by passenger aircraft with a drone or spare batteries, battery transport is a separate issue from flight-time calculations. Consult the FAA PackSafe drone and UAS guidance and your airline's current requirements before packing batteries.
A larger capacity value from the calculator should be treated as a starting point for evaluation. Check physical dimensions, connector type, pack voltage, discharge capability, aircraft balance, takeoff weight and manufacturer limits before changing battery size. Increasing energy while making the aircraft too heavy can reduce efficiency or compromise handling.
For battery-only conversions, the Battery Capacity Calculator is useful for separating electrical capacity from aircraft effects. For general battery endurance outside aviation, use the runtime calculator.
Use these published calculators together to check the individual conversions behind your drone battery estimate instead of relying on one number alone.
Calculate LiPo pack energy, runtime and discharge-related values for drones, RC vehicles and other high-current applications.
Use CalculatorConvert milliamp-hours and voltage into watt-hours so battery energy can be compared across different cell counts.
Use CalculatorCalculate stored electrical energy from voltage, capacity and related battery values.
Use CalculatorEstimate runtime for a battery powering a known load without drone-specific mission assumptions.
Use CalculatorConvert between mAh, Ah, Wh and related capacity measurements for clearer battery comparisons.
Use CalculatorEstimate energy, current, usable capacity and runtime for broader lithium battery applications.
Use CalculatorAnswers to common questions about LiPo pack voltage, mAh, watt-hours, flight-time estimates and battery sizing.
Convert battery capacity to watt-hours by multiplying amp-hours by nominal pack voltage. Apply the usable battery percentage and any efficiency assumption, then divide available watt-hours by average flight watts. Multiply hours by 60 to get minutes. The Drone Battery Calculator performs those steps automatically.
The S value is the number of cells connected in series. Series connection adds cell voltage. Using 3.7V nominal cells as an example, 3S is 11.1V nominal, 4S is 14.8V and 6S is 22.2V. Use the actual nominal cell value specified for your battery.
Using 3.7V nominal cells, a 4S pack is 14.8V. A 5000mAh battery is 5Ah, so nominal energy is 14.8 × 5 = 74Wh. Usable flight energy will be lower when a reserve or other losses are included.
The entered average power may be too low, or real flight conditions may require more power than the scenario used for the estimate. Wind, payload, battery temperature, voltage sag, battery age, aggressive maneuvers and the amount of reserve left before landing can all reduce measured endurance.
Not proportionally. More capacity adds energy but usually also adds mass. Extra mass can increase the thrust and power required to hover. There may eventually be little endurance benefit, and the aircraft may also have battery-size or takeoff-weight limits that must not be exceeded.
Use a representative average for the type of flight you are planning. Battery-side voltage and current logs from an actual flight can be particularly useful because watts can be estimated from volts multiplied by amps. Do not use the sum of every motor's maximum rating as an average hover value.
It shows average C-load as a screening value, but that is not enough to select a battery. Drone propulsion systems can draw much higher peak current during rapid throttle changes. Battery selection must consider measured or specified peak current, voltage sag, connector limits and the manufacturer's discharge specifications.
The basic energy equations work with other rechargeable lithium packs when the correct nominal cell voltage, capacity and usable-energy assumptions are entered. Do not automatically use 3.7V or LiPo-specific operating assumptions for a battery with different manufacturer specifications.
A 100% input is useful for seeing the mathematical upper bound, but it models no planned reserve. Real operating limits depend on the battery, aircraft and manufacturer guidance. Enter a usable percentage that reflects the reserve strategy appropriate to your system and mission.
No. It is the capacity required by the energy equation if average watts stay constant. A battery with more mAh can weigh more and change the aircraft's power requirement, balance and handling. Verify physical compatibility, weight, voltage, discharge capability and manufacturer limits separately.
Use the Drone Battery Calculator with your real pack label and representative average power data, then compare the result with logged flight performance. Refine one assumption at a time to understand how battery energy, reserve and aircraft power affect endurance.
Recalculate Drone Battery