High energy density, high-power and long-range lithium battery solutions for cargo UAVs, delivery drones, logistics drones and heavy-payload unmanned aircraft.
LithoTop develops customized lithium battery packs for cargo and delivery drones requiring high payload capability, stable takeoff power, long flight range, low battery weight and reliable repeated operation.
Cargo and delivery drones are increasingly used for last-mile delivery, medical transport, industrial logistics, emergency response, remote-area supply, offshore operations and autonomous transportation.
Unlike small consumer UAVs, cargo drones must lift not only the aircraft itself, but also payloads, delivery containers, communication systems, GPS/GNSS, obstacle-avoidance sensors, flight controllers and redundant electronics.
Battery engineering therefore requires a careful balance between battery weight, payload capacity, flight range, discharge current, peak takeoff power, reserve energy and charging time.
LithoTop develops high-rate LiPo batteries, high energy density LiPo batteries and custom Li-ion UAV battery packs for prototype development, flight testing and OEM production.
Battery solutions for commercial logistics UAVs, heavy-payload drones, autonomous delivery aircraft and long-range unmanned transportation systems.

Battery selection depends on propulsion power, payload, aircraft architecture, target range, maximum battery weight and peak current.
Providing complete aircraft, propulsion, flight and mechanical data enables a more accurate battery configuration and weight evaluation.
| Parameter | Typical Customization Range |
|---|---|
| Nominal Voltage | 22.2V–88.8V or Custom |
| Configuration | 6S–24S or Custom |
| Capacity | 5,000mAh–50,000mAh or Custom |
| Battery Chemistry | High-Rate LiPo / High Energy LiPo / Li-ion / Advanced High-Energy Options |
| Continuous Discharge Rate | 5C–50C, Depending on Cell Platform |
| Burst Discharge Rate | Up to 100C, Subject to Cell and Pack Design |
| Continuous Current | Customized According to Propulsion Load |
| Peak Current | Customized According to Takeoff Demand and Duration |
| Charging | Standard / Fast Charging Optional |
| Smart Monitoring | Optional |
| BMS / Protection | Optional According to Battery Architecture |
| Communication | CAN / Custom |
| Temperature Sensor | NTC Optional |
| Housing | Heat Shrink / Composite / Plastic / Custom |
| Connector | XT90-S / AS120 / AS150 / QS8 / Custom |
| Operating Temperature | Standard / Low Temperature Options |
| Certification Support | UN38.3 / MSDS |
* Custom Lipo Battery from LithoTop Now !
Send us your aircraft weight, payload, propulsion system, hover current, takeoff current, required voltage, target flight range, battery size, maximum battery weight and connector requirements. LithoTop will evaluate a custom UAV battery solution balancing energy density, discharge power, payload efficiency and flight time.
Cargo and delivery drones commonly use high-rate LiPo batteries because they can provide the high current required during takeoff, climbing and heavy-payload flight. High-energy LiPo or Li-ion battery packs may also be selected when longer flight range and lower battery weight are the primary design targets.
Battery capacity should be selected according to aircraft takeoff weight, payload, average flight power, hover current, required flight time and reserve energy. Increasing capacity can extend flight time, but it also increases battery weight. The final design should therefore optimize usable energy, payload capacity and total aircraft weight rather than simply selecting the largest possible battery.
The required discharge rate depends on continuous propulsion current, takeoff current, payload and peak-current duration. Cargo UAV projects may require anything from moderate discharge capability to high-rate 20C, 30C, 50C or higher cell platforms. Continuous and peak current should be calculated from the actual propulsion system rather than selecting the battery only by its advertised C-rating.
Yes. LithoTop can develop multi-series UAV battery packs such as 6S, 8S, 12S, 14S, 16S, 18S, 24S and project-specific configurations. The final voltage must be matched to the motor, ESC, power distribution system, charger and aircraft electrical architecture.
Yes. For long-range delivery UAVs, LithoTop can evaluate high-energy-density LiPo and Li-ion cell platforms together with lightweight pack structures, optimized wiring and suitable connectors. The design must still provide enough current capability for takeoff, climbing, maneuvering and emergency power demand.
Fast charging can be evaluated on selected cell platforms. The allowable charging rate depends on cell chemistry, battery temperature, pack capacity and cycle-life target. For commercial drone fleets, the battery and charger should be engineered together to balance charging time, temperature rise and battery service life.
Yes. Depending on the battery architecture, LithoTop can evaluate smart monitoring and communication functions such as CAN, UART, SMBus or customized protocols. Voltage, current, temperature, remaining capacity, cycle information and protection status can be integrated with the aircraft or fleet-management system.
Yes. Swappable battery packs can be developed with customized pack dimensions, handles, mounting structures, anti-spark connectors, power terminals and communication interfaces. For fleet applications, the mechanical interface and electrical connection should be designed for fast replacement, repeatable positioning and reliable high-current connection.
Yes. LithoTop can evaluate low-temperature LiPo and high-rate battery solutions for winter logistics, mountain delivery and cold-region UAV operations. Low-temperature design should consider cold-soak duration, takeoff current, voltage sag, usable capacity and minimum operating voltage.
Please provide the required battery voltage, target capacity, maximum battery dimensions and weight, aircraft takeoff weight, payload, motor and ESC specifications, hover current, continuous current, peak takeoff current and duration, required flight time or range, connector, charging requirement, operating temperature and estimated quantity. Aircraft drawings, existing battery specifications and certification requirements are also helpful for engineering evaluation.
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