FUSELAGE OF AN AIRCRAFT OR SPACECRAFT AND CORRESPONDING AIRCRAFT OR SPACECRAFT

摘要

The invention relates to a fuselage of an air- or spacecraft. The fuselage comprises at least one shell element and one insulation element. The insulation element is configured as a passive, watertight insulation element and can be mounted on an inner side of the at least one shell element in a completely air- and watertight manner. The invention furthermore relates to a respective aircraft or spacecraft.