Abstract: A three-dimensional biomaterial including particles encapsulating at least one complement active fragment dispersed therein. Also, a process of manufacturing of the three-dimensional biomaterial with at least one biocompatible and/or resorbable polymer and the particles. The three-dimensional biomaterial is useful for tissue regeneration, especially with regards to dental pulp, dentin, periodontal and gingival tissues, as well as bones tissues.

Abstract: A lightning protection system for a radome, the system comprising at least one lightning protection strip positioned on an inner wall of the radome, wherein the lightning protection strip defines, on the inner wall of the radome, a curve that is substantially perpendicular, at all points thereof, to the polarization direction of the electrical field vector radiated by an antenna across from the inner wall of the radome.

Abstract: A lightning protection system for a radome, the system comprising at least one lightning protection strip positioned on an inner wall of the radome, wherein the lightning protection strip defines, on the inner wall of the radome, a curve that is substantially perpendicular, at all points thereof, to the polarization direction of the electrical field vector radiated by an antenna across from the inner wall of the radome.

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).