Abstract: A radome system for fastening an aircraft radome, wherein the system includes a plurality of first fasteners each designed to put the radome into a position along two distinct axes contained in a plane approximately perpendicular to the longitudinal axis (L) of this fastener; and a plurality of second fasteners each designed to put the radome into a position along a single axis of a plane approximately perpendicular to the longitudinal axis (L) of this fastener.

Abstract: The invention relates to a device for fastening an aircraft radome (2) which comprises: a plurality of first fasteners (10) each designed to put said radome into a position along two distinct axes contained in a plane approximately perpendicular to the longitudinal axis (L) of this fastener; and a plurality of second fasteners (12) each designed to put said radome into a position along a single axis of a plane approximately perpendicular to the longitudinal axis (L) of this fastener. The invention also relates to an aircraft comprising a nose radome fixed to the aircraft using such a device, and an assembly method for assembling a radome (2) on an aircraft fuselage (1).