BATTERY ARRANGEMENT FOR INTEGRATION IN A VEHICLE

A battery arrangement for integration in a vehicle, in particular an aircraft or spacecraft, comprises two cover plates having battery sockets; a plurality of batteries, which are held on both sides between the cover plates by the battery sockets, wherein the batteries are arranged in battery rows along the cover plates; and a microchannel tube arrangement having a plurality of thermally conducting tubes configured to dissipate heat from the batteries, wherein a lateral surface of each battery is wrapped in a thermally conductive sheet, which is thermally connected to the microchannel tube arrangement. (Fig. 6)