| CPC B60L 58/26 (2019.02) [B60L 50/64 (2019.02); B64D 27/24 (2013.01); B60L 2200/10 (2013.01); B60L 2240/36 (2013.01)] | 20 Claims |

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1. An apparatus for a ground-based battery management for an electric aircraft, the apparatus comprising:
a battery pack mechanically coupled to the electric aircraft, wherein the battery pack comprises at least a battery module, wherein each battery module of the at least a battery module comprises:
at least a battery unit, wherein the at least a battery unit comprises:
battery cells; and
a thermal conduit configured to transfer heat between the battery cells and the thermal conduit; and
a thermal circuit mechanically coupled to the thermal conduit, wherein the thermal circuit is configured to facilitate the heat transfer using thermal media; and
a media channel, communicatively connected to a computing device, that encompasses the battery pack, wherein the media channel is configured to:
connect to a ground cooling component, wherein the ground cooling component is configured to provide the flow of the thermal media into the battery pack using the thermal circuit; and
evacuate the thermal media out of the battery pack using the thermal circuit; and
the computing device comprising a battery management system, wherein the battery management system is configured to receive a condition parameter and to control the flow of the thermal media as a function of the condition parameter.
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