A hover-capable airship, comprising an electric propulsion system comprising: - a plurality of electric power generators (G1, G2, G3, G4), - a plurality of electrical buses (Bus 1, Bus 2, Bus 3, Bus 4) and - a plurality of electric propulsion points (PXt, PXb, PY, PZbt, PZbb, PZst, PZsb), characterized in that said plurality of propulsion points comprising at least one propellant bundle formed of a plurality of electric-driven propeller-based thrusters dedicated to exert a longitudinal thrust, at least one propellant bundle formed of a plurality of dedicated electric-driven propeller-based thrusters to exert a vertical thrust and at least one of said longitudinal or vertical propellant bundles being arranged so that each thruster within said propellant bundle is electrically connected by means of an electrical bus (Bus 1, Bus 2, Bus 3, Bus 4) among said plurality of electrical buses to a generator within said plurality of electric power generators and each other thruster within said propellant bundle is electrically connected by means of another electrical bus among said plurality of electrical buses to another generator within said plurality of electric power generators, and in that the plurality of propulsion points further comprises at least one propellant bundle (PY) dedicated to producing a lateral thrust, said propellant bundle (PY) being arranged so that one of its thrusters is electrically connected by means of an electrical bus (Bus 1, Bus 2, Bus 3, Bus 4) among said plurality of electrical buses to a generator within said plurality of electric power generators and each at least one other thruster within said propellant bundle is electrically connected by means of another electrical bus among said plurality of electrical buses to another generator within said plurality of electric power generators. - a plurality of electric power generators (G1, G2, G3, G4), - a plurality of electrical buses (Bus 1, Bus 2, Bus 3, Bus 4) and - a plurality of electric propulsion points (PXt, PXb, PY, PZbt, PZbb, PZst, PZsb), characterized in that said plurality of propulsion points comprising at least one propellant bundle formed of a plurality of electric-driven propeller-based thrusters dedicated to exert a longitudinal thrust, at least one propellant bundle formed of a plurality of dedicated electric-driven propeller-based thrusters to exert a vertical thrust and at least one of said longitudinal or vertical propellant bundles being arranged so that each thruster within said propellant bundle is electrically connected by means of an electrical bus (Bus 1, Bus 2, Bus 3, Bus 4) among said plurality of electrical buses to a generator within said plurality of electric power generators and each other thruster within said propellant bundle is electrically connected by means of another electrical bus among said plurality of electrical buses to another generator within said plurality of electric power generators, and in that the plurality of propulsion points further comprises at least one propellant bundle (PY) dedicated to producing a lateral thrust, said propellant bundle (PY) being arranged so that one of its thrusters is electrically connected by means of an electrical bus (Bus 1, Bus 2, Bus 3, Bus 4) among said plurality of electrical buses to a generator within said plurality of electric power generators and each at least one other thruster within said propellant bundle is electrically connected by means of another electrical bus among said plurality of electrical buses to another generator within said plurality of electric power generators. <EOS>