An aircraft with an aircraft structure, comprising: a radome cover shell that is adapted to enclose equipment in a nose region of the aircraft in a closed position; and a radome cover opening kinematic that enables a first movement of the radome cover shell from the closed position to an opened position and a second movement of the radome cover shell from the opened position to the closed position, wherein the radome cover opening kinematic comprises: a guiding rail that is attached to the radome cover shell, and at least three rollers that are attached to the aircraft structure, wherein a first and a second roller (230a, 230b) of the at least three rollers are arranged on opposing sides of the guiding rail, and wherein the second and a third roller (230b, 230c) of the at least three rollers are arranged on the same side of the guiding rail; wherein the first movement of the radome cover shell from the closed position to the opened position comprises a longitudinal movement from the closed position to a first partially opened position, a first rotational movement from the first partially opened position to a second partially opened position, and a second rotational movement from the second partially opened position to a completely opened position, and wherein the guiding rail further comprises: a curved end that engages with the first roller to form a guiding rail rear stopper that stops the longitudinal movement of the radome cover shell at the first partially opened position; wherein the first and second rollers (230a, 230b) are opposing each other on opposing sides of the guiding rail; and wherein the curved end is rotated around an axis defined by the first roller during the first and second rotational movements. a radome cover shell that is adapted to enclose equipment in a nose region of the aircraft in a closed position; and a radome cover opening kinematic that enables a first movement of the radome cover shell from the closed position to an opened position and a second movement of the radome cover shell from the opened position to the closed position, wherein the radome cover opening kinematic comprises: a guiding rail that is attached to the radome cover shell, and at least three rollers that are attached to the aircraft structure, wherein a first and a second roller (230a, 230b) of the at least three rollers are arranged on opposing sides of the guiding rail, and wherein the second and a third roller (230b, 230c) of the at least three rollers are arranged on the same side of the guiding rail; wherein the first movement of the radome cover shell from the closed position to the opened position comprises a longitudinal movement from the closed position to a first partially opened position, a first rotational movement from the first partially opened position to a second partially opened position, and a second rotational movement from the second partially opened position to a completely opened position, and wherein the guiding rail further comprises: a curved end that engages with the first roller to form a guiding rail rear stopper that stops the longitudinal movement of the radome cover shell at the first partially opened position; wherein the first and second rollers (230a, 230b) are opposing each other on opposing sides of the guiding rail; and wherein the curved end is rotated around an axis defined by the first roller during the first and second rotational movements. a guiding rail that is attached to the radome cover shell, and at least three rollers that are attached to the aircraft structure, wherein a first and a second roller (230a, 230b) of the at least three rollers are arranged on opposing sides of the guiding rail, and wherein the second and a third roller (230b, 230c) of the at least three rollers are arranged on the same side of the guiding rail; wherein the first movement of the radome cover shell from the closed position to the opened position comprises a longitudinal movement from the closed position to a first partially opened position, a first rotational movement from the first partially opened position to a second partially opened position, and a second rotational movement from the second partially opened position to a completely opened position, and wherein the guiding rail further comprises: a curved end that engages with the first roller to form a guiding rail rear stopper that stops the longitudinal movement of the radome cover shell at the first partially opened position; wherein the first and second rollers (230a, 230b) are opposing each other on opposing sides of the guiding rail; and wherein the curved end is rotated around an axis defined by the first roller during the first and second rotational movements.