
INR-21700-P50B cylindrical rechargeable battery cell
- Energy
- 18 Wh
- Nominal voltage
- 3.6 V
- Specific energy
- 265 Wh/kg
High energy density cells, modules and packs with battery management systems (BMS) for electric and hybrid propulsion.
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Updated November 3, 2026
In an electric aircraft the battery sets the range, a large share of the take-off mass and much of the safety case. The figures that matter are not only the energy density of the cell, but what remains after packaging, cooling and protection are added to make a flight-worthy pack.
Higher-energy cells usually give less power and fewer cycles. A drone flying long missions at low power and an eVTOL that must deliver high power for landing at the end of a flight need different cells, even at the same capacity.
Examples include H55, EaglePicher, Amprius and Molicel. See also power management units and hydrogen fuel cells.
Because a pack adds structure, wiring, cooling, the BMS and thermal-runaway protection, none of which store energy. Comparing cells is useful, but aircraft performance depends on the pack figure.
The discharge or charge current relative to capacity: 1C empties the battery in about one hour, 5C in about twelve minutes. Lift phases of eVTOL flights demand high C-rates.
It monitors cell voltages and temperatures, balances the cells, estimates state of charge and health, and isolates the pack if a limit is exceeded. In aircraft it also reports the battery status to the flight controller.
A self-sustaining overheating of a lithium cell that can spread to neighbouring cells. Aircraft packs are designed to contain it or stop it propagating, and are tested for it.
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