ah so these don't have the ability to discharge as much energy as Li-ion batteries, but for the volume and half the weigh have the same total energy
I wonder why then this would be more applicable to a drone or aerospace application - perhaps something that is not particularly heavy hence the reference to drones and high altitude flights, but won't these still need a decent amount of energy to launch?
Without cars it would seem to reduce the TAM, but yes there may be other applications where weigh is a significant issue (boats perhaps)
ah so these don't have the ability to discharge as much energy...
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