AIRCRAFT HAVING A FUEL-CELL PROPULSION SYSTEM

The invention is directed to an aircraft having a fuel-cell propulsion system that includes a fuel cell for supplying electricity to an electric propulsion apparatus of the aircraft, a fuel store for storing fuel for the fuel cell, and a cooling apparatus for cooling the fuel cell. A main heat exchanger of the cooling apparatus and the fuel store are arranged on a top side of a fuselage of the aircraft, and the main heat exchanger is arranged in front of the fuel store toward the aircraft nose.